# SDR

REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES, RBL 11 BS 312 TO BS 328 INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 60 INCHES IN SEVERAL AREAS, BS 302 TO BS 362 LEFT SIDE Z-ANGLE.  REMOVED CORRODED Z-ANGLE, REPLACED AND COMPLETED INSTALLATION.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES LBL 11 BS 328 TO BS 344 INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 30 PERCENT CORRODED Z-ANGLE FORWARD GALLEY ENTRANCE, STATION 277 AND STATION 344.  REMOVED AND REPLACED NR ME-32 REQUIRED.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02.  CORROSIONLEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 74 INCHES BY .5 INCH CORRODED AREA BS 344 LBL 55 THROUGH RBL 21 BEAM.  FABRICATED T-CAP AND REPAIR ANGLE AND INSTALLED.  REPAIRED PER TR 53-10-3.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ONE .5 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 947 LBL 4 ANDRBL 4 FLOOR BEAM.  INSTALLED T-CAP, REPAIR ANGLES AND STRAPS.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 25 INCHES BY .5 INCH CORRODED AREA LBL 22 BS 344-369 SEAT TRACKS.  FABRICATED SEAT TRACKS AND INSTALLED.  REPAIRED PER SRM 53-00-52.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1.5 INCH BY 1 INCH, BY STATION 947 TO STATION 967, RBL 45 INTERCOSTAL.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 SQUARE INCHES OF CORROSION AT T-CAP FLOOR BEAM STATION 947 RBL 9.  REMOVED CORRODED SECTION OF T-CAP.  SPLICED IN NEW SECTION OF T-CAP.  REPAIRED PER SRM 53-10-9.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH CORRODED AREA ON STRINGER S-27L AT STATION 947.5.  REMOVED CORRODED SECTION OF STRINGER AND REPLACED.  REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 3 INCH AT ATTACH ANGLE STATION 947.5 BETWEEN STRINGER 26L AND 27L.  REPLACED ANGLE WITH NEW ONE FROM STOCK.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-202-01.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK RBL 25 LONGITUDINAL FLOOR BEAM AT AILERON QUADRANT STATION 676, WL 206.5.  INSTALLED DOUBLER, REPAIRED PER EA 40395 AND EO 5791G632.  (M)


REMARKS:
INT - DURING Q-2 VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 616 LEFT FRAME INBOARD CHORD FIRST FASTENER ABOVE CENTERWING.  INSTALLED DOUBLER, REPAIRED PER EO 40390.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 616 RIGHT FRAME INBOARD CHORD AT FIRST FASTENER ABOVE CENTER WING.  INSTALLED DOUBLER, REPAIRED EPR EA 40390.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK 1.5 INCHES LONG STATION 597 ABOVE WING CENTER SECTION LEFT FRAME. REPLACED FRAME SECTION.  REPAIRED PER SRM 51-10-01.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK 1.25 INCH LONG STATION 597 ABOVE WING CENTER FRAME SECTION RIGHT SIDE.  REPLACED FRAME SECTION.  REPAIRED PER SRM 51-10-01.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK LBL 25 SEAT TRACK SUPPORT CHANNEL STATION 520, WL 207.5. REPLACED SUPPORT CHANNEL, REPAIRED PER SRM 51-10-1.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FouND .75 INCH CRACK LBL 45 SEAT TRACK SUPPORT CHANNEL STATION 520, WL 207.5. REPLACED SUPPORT CHANNEL, REPAIRED PER SRM 51-10-01.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TWO CRACKS (LIGHTNING STRIKE) ON SKIN S-19R FS 328.  INSTALLED DOUBLER AND FILLER.  REPAIRED PER EO 40393 EA 40393.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1.5 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 328 LBL 13 TO RIGHT END OF FLOOR BEAM.  REPLACED T-CAP.  REPAIRED PER TR 53-10-03 SRM 51-70-12 SRM 51-70-11.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK SHEET METAL AT LOWER CORNER MED.  INSTALLED INTERIM REPAIR PER EA 31854 AND TBC.  REPAIRED PER EA 31854SB 737-53-1083.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION RIGHT STUB WING TO FUSELAGE AT STATION 24011-26011.  INSTALLED DOUBLER REPAIR PER USAIR EA NR 29492B AND EA NR 31703.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND CORROSION ON FLOOR BEAM BLO AT STATION 3845 T-CAP.  REMOVED SECTION OF CORRODED T-CAP FROM STATION 3845 TO 5315 AND SPLICED IN NEW SECTION PER SRM 53-21-10.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND LIGHTNING STRIKE DAMAGE ABOVE CO-PILOTS SLIDING WINDOW IN FUSELAGE SKIN PITTED.  INSTALLED FLUSH REPAIR PER USIAR EA NR 31049.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION LEFT STUB WING TO FUSELAGE AT STATION 24011 TO 26011.  INSTALLED DOUBLER REPAIR PER USAIR EA NR 29492B AND EA NR 31703.  (M)


REMARKS:
PIT - DURING Q-1 INSPECTION, FOUND CORROSION .005 INCH TO .053 INCH ON FLOOR BEAM AT STATION 1127R FWD OF FRAME 4850.  REPLACED SECTION OF BEAM FROM STATION 4850 TO 5305 PER SRM 53-21-10.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER INBOARD PYLON SKIN IN AREA OF HEAT SHIELD NR 1 PYLON.  REPLACED SKIN IN NR 1 PYLON INBOARD SIDE AS PER EA NR 40605.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER OUTBOARD PYLON SKIN IN AREA OF HEAT SHIELD NR 1 PYLON.  REPLACED SKIN NR 1 PYLON OUTBOARD SIDE PER USAIR EA NR 40605.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND A .0531 INCH DEEP DENT WITH .0065 GOUGE LOCATED AT FUSELAGE SKIN AT STRINGER 52R-55R, BETWEEN STATION 480-500.  INSTALLED EXTERNAL DOUBLER AS PER USAIR EA NR 40595.  (M)


REMARKS:
CLT - INSPECTION VISUALLY AND BY HFEC FOUND AT FUSELAGE SKIN A DENT 5.5 INCH BY 3.75 INCH, .130 DEEP LOCATED AT BS 231.5, OUTBOARD CHORD ABOVE VANE.  REPLACED CHORD ANGLES AND REPAIRED SKIN WITH FILLER AND DOUBLER AS PER USAIR EA NR 40596. (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND A DENT 8 INCHES BY 4 INCHES IMPACT DAMAGE LOCATED AT BS 480 BETWEEN STRINGER 25R AND STRINGER 26R OF FUSELAGE SKIN.  INSTALLED DOUBLER PER USA EA NR 40585.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 597 RIGHT FRAME OUTBOARD FLANGE RADIUS JUST ABOVE CENTER WING.  REMOVED AND REPLACED FRAME PER DRAWING 65-46538.  NO WEIGHT CHANGE.  (M)


REMARKS:
INT - DURING Q-5 CHECK, EDDY CURRENT FOUND .5 INCH CRACK AT BS 400 STRINGER 25L TO STRINGER 26L.  INSTALLED DOUBLER, REPAIRED PER EA 40544.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER CLIP, AT BS 639 STRINGER 6R.  REPLACED CLIP,REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 616, STRINGER 2L TIE CLIP.  INSTALLED NEW TIE CLIP.  REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SPOTS OF CORROSION AT FLOOR BOARD BEAM ATTACH HOLES BS 986.5 LBL 18 TO RIGHT END.  INSTALLED REPLACEMENT T-CAP.  REPAIRED PER TR 53-10-05C.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 1.(M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 38 INCHES IN LENGTH UPPER FLANGE CABIN FLOOR BEAM BS 967 LBL 10-RBL 28.  INSTALLED T-CAP REPAIR.  REPAIRED PER TR 53-10-05C.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 21 INCHES CORRODED AREA AT FLOOR BEAM BS 947 RBL 10 TO LBL 11.  REPAIRED T-CAP.  REPAIRED PER SRM 53-10-9.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 1.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND THREE CORRODED AREA ON INTERCOSTAL .5 INCH BY .25 INCH AT BS 986 TO BS 1006 APPROXIMATELY LBL 18 INCHES.  REPLACED WITH IDENTICAL PART NR 1121963.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
PHL - FL 194 - AFTER TAKEOFF FROM BWI, AIRCRAFT ENCOUNTERED LIGHT WAKE TURBULENCE.  CREW RECEIVED BULK CARGO DOOR WARNING LIGHT AND REPORTED THAT THE AIRCRAFT WOULD NOT HOLD PRESSURIZATION.  FLIGHT DIVERTED TO PHL AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE PRESSURIZED THE AIRCRAFT AND COULD NOT DUPLICATE THE CONDITION.  UPON OPENING THE REAR BULK BINDOOR, THEY FOUND THAT A BAG HAD FALLEN AGAINST THE DOOR BENDING THE DOOR SENSOR (S211).  SENSOR WAS SUBSEQUENTLY REPLACED.  (M)


REMARKS:
LAX - FL 7 - EN ROUTE PIT-LAX - PASSENGER SMELLED AND SAW SMOKE IN THE CABIN.  CREW DESCENDED FROM FL390 TO FL310 AND SHUT DOWN THE RIGHT PACK.  SMOKE ABATED, FLIGHT CONTINUED TO LAX AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT RECIRCULATION FAN AND FILTER.  (M)


REMARKS:
CLT - FL 551 - AFTER TAKEOFF, CREW HAD GEAR DOOR OPEN INDICATION.  FLIGHT RETURNED TO CLT AND LANDED WITH BOTH MAIN LANDING GEAR DOORS OPEN.  THE LEFT GEAR DOOR WAS DAMAGED.  MAINTENANCE REPLACED THE LEFT LANDING GEAR DOOR SWITCH AND THE LEFT MAIN LANDING GEAR DOOR.  (M)


REMARKS:
FLT NR 328 - CLT - UPON TAKEOFF AT CLT, THE NR 3 MAIN TIRE LOST THE RECAP.  GEAR WAS NOT RETRACTED.  FLIGHT RETURNED TOFIELD AT CLT AND LANDED WITHOUT INCIDENT.  (M)


REMARKS:
FLT NR 1281 - SYR - ON TAKEOFF CLIMB FROM SYR CAPTAIN REPORTED A GEAR INDICATION PROBLEM AND RETURNED TO THE FIELD AT SYR.  THE NOSE AND LEFT MAIN GEAR WOULD NOT RETRACT.  (M)


REMARKS:
SYR - FL 1146 - ON APPROACH, CREW SELECTED GEAR DOWN AND THE LEFT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE.  CREW RECYCLED GEAR WITH SAME RESULT.  NO WARNING HORN SOUNDED AND NO RED LIGHT ILLUMINATED.  GEAR WAS VERIFIED DOWN AND LOCKED THROUGH VIEW PORT.  FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOWNLOCK SWITCH AND PROGRAMMED THE GEAR HARNESS FOR REPLACEMENT.  (M)


REMARKS:
FLT NR 689 - PIT - WHILE AT FL 350 THE AIRCRAFT PRESSURIZATION STARTED TO CLIMB TO 10K FEET.  THE CAPTAIN REQUESTED DESCENT TO FL 100 AND RECEIVED SAME FROM ATC.  THE FLT WAS DIVERTED TO PIT.  NO EMERGENCY WAS DECLARED.  THE FLT LANDED IN AT PIT WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THAT THE RIGHT AIRCO PACK WAS AT FAULT AND REPLACED SAME.  (M)


REMARKS:
CRW - FL 551 - EN ROUTE CLE-CLT, CREW EXPERIENCED VIBRATION FROM RIGHT ENGINE.  UPON POWER REDUCTION, THE VIBRATION BECAME SEVERE.  CREW SHUT DOWN ENGINE (SET 12 MINUTES), DECLARED AN EMERGENCY DIVERTED TO CRW.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT ENGINE.  (M)


REMARKS:
PIT - FL 317 - AFTER TAKEOFF AND UPON GEAR RETRACTION, CREW RECEIVED 'GND/FLT' MESSAGE ON MFDU, FOLLOWED BY SEVERAL AURAL AND VISUAL WARNINGS.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE PROXIMITYSWITCH ELECTRONICS UNIT.  (M)


REMARKS:
PIT - FL 1095, DURING TAKEOFF AT PIT, THE LEFT OUTBOARD MAIN WHEEL DEPARTED THE AIRCRAFT.  CREW WAS ADVISED BY THE PIT TOWER.  FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE WHEEL.  INVESTIGATION PROCEEDING, REVEALED THE POSSIBILITY EXISTS OF A FALSE TORQUE ON THE WHEEL NUT.  (M)


REMARKS:
FLT NR 1007 - CLT - THE FLIGHT RETURNED TO FIELD DUE TO A GROUND SENSE PROBLEM.  (M)


REMARKS:
CRW - FL 7007 - EN ROUTE TYS-PIT - CABIN ALTITUDE BEGAN CLIMBING AND WAS UNCONTROLLABLE.  CREW DESCENDED AND DIVERTED TO CRW.  BOTH PACKS WERE REPORTED AS OPERATING SATISFACTORILY.  MAINTENANCE FOUND A HOLE IN THE AFT PRESSURE BULKHEAD DUETO AN UNCONTAINED APU FAILURE.  THE APU HAD FAILED ON THE GROUND IN TYS.  THE FACT THAT THE FAILURE WAS UNCONTAINED WASNOT RECOGNIZED PRIOR TO FLIGHT.  THIS IS THE FIRST REPORTED UNCONTAINED FAILURE OF THIS MODEL APU.  (M)


REMARKS:
GRR - FL 400 - CREW REPORTED, THAT THE LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION.  CREW PERFORMED A TOWER FLY-BY AND DECLARED AN EMERGENCY.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED A BURNED OUT LIGHT BULB.  (M)


REMARKS:
CLT - FL 1295 - EN ROUTE PIT - LGA, CREW RECEIVED TAIL ANTI-ICING FAULT SHORTLY AFTER SELECTING TAIL ANTI-ICE.  FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE TAIL ANTI-ICE SHUTOFF VALVE.  (M)


REMARKS:
PIT - COCKPIT EMERGENCY LIGHT DID NOT ILLUMINATE WITH THE EMERGENCY SWITCH IN THE ON POSITION.  MAINTENANCE REPLACED THE DOME LIGHT ASSEMBLY.  (M)


REMARKS:
SJU - FL 7010 - ON CLIMB-OUT, FLIGHT ATTENDANT NOTIFIED CAPTAIN OF BURNING SMELL IN CABIN.  PUT PRESSURIZATION SYSTEM INTO STANDBY AND RETURNED TO SJU.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR ONE TRANSFORMER RECTIFIER.  (M)


REMARKS:
FLT 818 - PIT - FLIGHT DIVERTED TO PIT DUE TO NR 1 ENGINE HIGH EGT.  (M)


REMARKS:
FLT NR 1244 - CLT - LEFT WING BODY OVERHEAT ILLUMINATED IN FLT.  ISOLATED LEFT BLEED AIR DUCT BUT OVERHEAT LIGHT REMAINED ON.  MAINTENANCE FOUND OVERHEAT ELEMENT SHORTED.  REPLACED ELEMENT.  OPS CHECKS SAT.  (M)


REMARKS:
FLT NR 1440 - MCO - ON TAKEOFF FROM PBI, AIRCRAFT WOULD NOT PRESSURIZE.  SELECTED STANDBY THEN MANUAL, NO HELP, OUTFLOWVALVE FULL CLOSED.  MAINTENANCE REPLACED PRESSURIZATION SELECTOR PANEL.  PRESSURIZED AIRCRAFT ON GROUND AT MCO.  OPS CHECKS OK.  (M)


REMARKS:
FLT NR 2339 - FLL - ON APPROACH TO FLL, COULD NOT GET FLAPS TO EXTEND BEYOND 18 DEGREES INDICATED.  INITIATED GO AROUND, RESET BREAKERS, FLAPS EXTENDED NORMALLY SECOND TIME, NO ASYMMETRY.  MAINTENANCE LUBRICATED BALL NUT RESERVOIR AND JACKSCREWS.  (M)


REMARKS:
FLT NR 1530 - PHL - GREEN 'NOSE GREEN' REMAINED ON ENTIRE LIGHT.  RED 'NOSE GEAR' LIGHT NEVER CAME ON IN FLIGHT.  FLEW BY TOWER.  MAINTENANCE REPLACED THE LANDING GEAR ACCY UNIT.  ALL INDICATIONS NORMAL.  (M)


REMARKS:
FLT NR 1635 - PHL - UNSCHEDULED MAINTENANCE FOR CEILING EMERGENCY LIGHTS INOP.  MAINTENANCE REPAIRED WIRE ON CENTER OVERHEAD CEILING LIGHT.  EMERGENCY LIGHTS OPS CHECK NORMAL.  (M)


REMARKS:
STL - FLT 401 - DURING INSPECTION, FOUND ROW 2 AND ROW 3 EGRESS LIGHTS NOT OPERATING.  REPLACE BULBS TW NR 93-2832, MFG7732.  OPERATIONAL CHECK OF EGRESS LIGHTS, CHECK NORMAL.  NEW AIRCRAFT 8-25-95.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR BEAM CAP, STA 1518, RBL 18.  REMOVED CORROSION AND REPAIRED PER SRM 53-00-51.  AIRCRAFT TOTAL TIME:  38,181 HOURS; 13,720 CYCLES.


REMARKS:
LAX - FLT 39 - ON APPROACH DURING GEAR EXTENSION, LEFT MAIN RED GEAR LIGHT CAME ON.  THE ALTERNATE GEAR EXTENSION METHOD WAS USED AND ALL LIGHTS FUNCTIONED PROPERLY.  REMOVED AND REPLACED PROXIMITY BOX, MFG PN 3260-0014-83.  OPERATIONAL CHECK NORMAL.  CHECK C-2D  7-19-95 - MCI.


REMARKS:
STL - FLT 39 - AFTER TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT ON LANDING GEAR RETRACTION.  CYCLED LANDING GEAR.  FOUND NLG AIR CHARGE DEPLETED.  SERVICED NLG WITH OIL AND NITROGEN.  NLG LEAK CHECKED AND OPERATION CHECKED NORMAL.  CHECK C-2D - 12-4-95 - JFK.


REMARKS:
FSD - FLT 0663 - DURING DESCENT, AUTO GROUND SPOILER ACTUATOR FAILED.  MFG PN 1040T100-5.  PULLED CIRCUIT BREAKER AND PLACARDED.  CHECKS MADE TO ASSURE NORMAL PERFORMANCE.  POWERED AIRCRAFT, NO FURTHER.  ELECTRICAL PROBLEM EXISTS.  CHECK C1-12-95 - STL.


REMARKS:
STL - FLT 255 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR DID NOT RETRACT.  CYCLED LANDING GEAR. FOUND NLG STRUT LOW ON AIR PRESSURE.  REPLACED SCHRADER VALVE, MFG PN A00314.  SERVICED NLG STRUT.  LANDING GEAR OPERATION CHECKED NORMAL.  CHECK C-1D - 7-28-95 - MCI.


REMARKS:
MCI - FLT 1435 - DURING CLIMB, SHUT DOWN RIGHT ENGINE, SN 1716, DUE TO NO THRUST LEVER RESPONSE.  FOUND BOLT MISSING FROM CROSS-SHAFT TO THRUST LEVER CABLE.  INSTALLED NEW BOLT, NUT, AND COTTER PIN.  ENGINE THRUST LEVER RESPONSE AND ENGINEOPERATION CHECKED NORMAL.  CHECK C-12 - 12-27-95 - STL.


REMARKS:
CID - FLT 64 - DURING CRUISE, FIRST CLASS COFFEEMAKER EMITTED SMOKE.  TURNED OFF COFFEEMAKER AND OPENED CIRCUIT BREAKER.  FOUND INTERNAL MALFUNCTION IN COFFEEMAKER.  REPLACED COFFEEMAKER, MFG PN 50198A, AND OPERATION CHECKED NORMAL.  CHECKC - 2-17-95 - MCI.


REMARKS:
IAD/MCO - FLT 467 - AFT AIRSTAIR LIGHT CAME ON AND CREW COULD NOT HOLD CABIN ALTITUDE.  CABIN ROSE TO 8,000 FEET, DESCENDED AND RETURNED TO IAD.  LANDED 3,000 POUNDS OVERWEIGHT.  INSPECTED ALL AIRCRAFT DOORS AND SEALS.  FOUND FOD ON RT FORWARD EMERGECY EXIT DOOR SEAL.  REMOVED FOD.  NO OTHER DEFECTS.  PERFORMED PRESSURIZATION FUNCTIONAL CHECK IAW MM 21-30.PERFORMED OVERWEIGHT LANDING CHECK.


REMARKS:
FLT 591 - AIR RETURN, ALTIMETER OFF 200 FEET AT ALTITUDE AND 120 FEET OFF ON ALTERNATE STATIC SOURCE.  REMOVED AND REPLACED CAPTAIN'S AND FIRST OFFICER'S ALTIMETER.  ACCOMPLISHED LEAK AND OPS CHECK GOOD.


REMARKS:
CLT - INSPECTION VISUALLY FOUND A DENT 5 INCHES BY 4 INCHES, .280 INCH DEEP AT EXTERIOR SKIN STA 278, 2 INCHES BELOW STR 17L FUSELAGE SKIN.  INSTALLED DOUBLER PER BOEING SRM 53-00-01, FIG 203, WITH BLIND RIVETS.  (X)


REMARKS:
TPA/ATL -  FLT 72 - WHILE PARKING AT GATE, ELECTRICAL SMOKE STARTED TO COME FROM GLARE SHIELD AND INSTRUMENT PANEL.  SHUT DOWN ENGINES AND APU.  FOUND MASTER DIM AND TEST MODULE M833 BURNED.  REMOVED AND REPLACED MASTER TEST AND DIM MODULE.  OPS CHECK PER MM 33-15-01.  (X)


REMARKS:
TPA/ATL - FLT 12 - LOW OIL FILTER BYPASS LIGHT CAME ON IN-FLIGHT.  IN-FLIGHT SHUT DOWN NR 3 ENGINE PRECAUTIONARY.  REMOVED AND REPLACED NR 3 ENGINE OIL SCREEN, NO CLOGGING FOUND.  FOUND CHAFED WIRE 6 INCHES FROM BYPASS PRESSURE SWITCH, D1402, PIN NR 1.  WIRE REPAIRED, OPS CHECK OK PER MM 79-34-01.  (X)


REMARKS:
FLT NR 559 - BNA-ATL - ON TAKEOFF THE LANDING GEAR WOULD NOT RETRACT.  AIR RETURN TO BNA.  LUBED RELEASES SWITCH AND CYCLED GEAR LEVER WITH PINS INSTALLED.  NO DEFECTS NOTED, AIRCRAFT OK FOR SERVICE.  (M)


REMARKS:
ON FLT NR 530 - ATL- AIR RETURN, NR 2 ENGINE OIL FILTER CLOG LIGHT CAME ON IN FLIGHT.  REPLACED NR 2 ENGINE OIL FILTER. INSPECTED FILTER FOR METAL AND OTHER DEBRIS, NO DEFECTS NOTED, FOUND DIFFERENTIAL PRESSURE SWITCH STUCK CLOSED.  REMOVED AND REPLACED SWITCH, RAN NR 2 ENGINE.  OPS CHECK NORMAL, LEAK CHECK OK.  (M)


REMARKS:
ON FLT NR 283 - IAD-FLL - AT FL 350 PRESSURIZATION FAILED.  CABIN CLIMBED TO 11,000 FEET.  THE CREW COULD NOT CONTROL MANUALLY.  CREW PERFORMED EMERGENCY DESCENT AS PER VJ EMERGENCY PROCEDURES.  MANUAL PRESSURE REGAINED AT 12,000 FEET.  FLIGHT DIVERTED TO ATL FOR MAINTENANCE.  UPON INSPECTION OF TAIL COMPARTMENT MX FOUND LEFT PACK DUCT BLOWN OFF THE WATER SEPARATOR.  RESECURED DUCT AND TIGHTENED CLAMPS.  RAN LEFT PACK.  NO LEAKS NOTED.  SYSTEM CHECKS GOOD PER MM 21-30.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 616 LEFT FRAME INBOARD INNER CHORD ANGLE FIRST FASTENER ABOVE CENTER WING.  INSTALLED FILLER AND ANGLE.  REPAIRED PER EA 40570.  (M)


REMARKS:
INT -DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BL 0 LONGITUDINAL FLOOR BEAM LOWER WEB STATION 707 WL 203AT FASTENER HOLE.  INSTALLED DOUBLER, REPAIRED PER BOEING REF DRAWING 65C34537.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS RBL 25 LONGITUDINAL FLOOR BEAM LOWER WEB STATION 707-708, WL 203 AT FASTENER HOLES.  INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 616 RIGHT FRAME INBOARD INNER CHORD ANGLE FIRST FASTENER ABOVE CENTER WING.  INSTALLED FILLER AND REPAIR ANGLE.  REPAIRED PER EA 40570.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION, 3 INCHES BY 3 INCHES ON WEB, LOCATED AT BS 1016 THROUGH BL0.  INSTALLED DOUBLERS, FILLERS AND STIFFENERS AS PER USAIR SRM 53-80-08, 51-70-11 AND 53-80-01.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND A LEVEL 2 CORROSION, 3 INCHES BY 6 INCHES, LOCATED ON INTERCOSTAL AT S21L, BS 986.5 THROUGH BS 1006.  FABRICATED AND INSTALLED NEW PARTS AS PER USAIR SRM 53-60-15, FIG 1 SHEET 4 DETAIL II-A.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND AN LEVEL 2 CORRODED AREA 3 INCHES ON FRAME, LOCATED FS 967 AT S-27L.  FABRICATED NEW PARTS AND INSTALLED FAIL/SAFE CHORD AS PER BOEING 51-70-11, 51-30-01 FIG 2, PG 14 AND BOEING DRAWING 65-46563-7.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORRODED AREA, 6 INCHES BY 6 INCHES, ON DOUBLER LOCATED AT BS 986.5 THROUGH 527L, 527R.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION, 6 INCHES LOCATED ON STRINGER 27L AT FS 967.  INSTALLED REPAIR CHANNEL AND ANGLES AS PER BOEING SRM 53-00-03 FIGURE 201, DETAIL VII.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND A LEVEL 2 CORRODED AREA, 10 INCHES BY 6 INCHES, LOCATED ON SKIN AT BS 967 THROUGH BS 987, BL 0.  CUT OUT CORRODED SKIN AND INSTALLED DOUBLER AS PER BOEING SRM 53-00-01 AND USAIR EO 40687.  (M)


REMARKS:
INT - DURING CX-6 CHECK VISUAL INSPECTION, FOUND TWO LOCATIONS 2 INCHES BY 4 INCHES CORRODED AND 2 INCHES BY 8 INCHES CORRODED AT STRINGER 27L, BS 927 TO 967.  INSTALLED STRINGER AND DOUBLERS.  REPAIRED PER SRM 53-10-3, FIG 1.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND A .25 INCH IMPACT DAMAGE TO COMPOSITE SKIN THROUGH COMPOSITE LAYERS LOCATED RIGHT ELEVATOR SKIN 15 INCHES OUTBOARD FROM INBOARD END, MIDDLE OF ELEVATOR.  ACCOMPLISHED WET LAYUP COMPOSITE REPAIR AS PER BOEINGSRM 51-70-17 AND USAIR EA NR 40618.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND AN 8 INCH BY 8 INCH EXTERNAL DOUBLER WITH BLIND FASTENERS, LOCATED AT FS 1006 TO 1016 BETWEEN STRINGER 23R THROUGH STRINGER 25R.  REINSTALLED WITH SOLID RIVETS AS USAIR EA NR 40533.  (M)


REMARKS:
CLT - INSPECTION BY HFEC, FOUND A CRACK APPROXIMATELY 1 INCH, LOCATED AT THE FLOOR BEAM, STATION 520, LBL 25.  INSTALLED DOUBLER AND RADIUS BLOCK AS PER USA EO NR 40604.  (M)


REMARKS:
CLT - INSPECTION BY HFEC, FOUND A CRACK APPROXIMATELY 1 INCH LOCATED AT THE FLOOR BEAM, STATION 520, RBL 45.  FABRICATED AND INSTALLED DOUBLERS AND FILLERS AS PER USAIR 40604.  (M)


REMARKS:
CLT - INSPECTION FOUND BY HFEC, A CRACK APPROXIMATELY 1 INCH LOCATED AT FLOOR BEAM STATION 520, LBL 45.  FABRICATED ANDINSTALLED DOUBLERS AND FILLERS AS PER USAIR EA NR 40604.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND 2 INCHES OF TORN SKIN AT EDGE OF CUTOUT, GND AIR/COND LOCATED APPROXIMATELY FS 530 BL0. INSTALLED REPAIR STRAP AS PER USAIR EO NR 40532.  (M)


REMARKS:
FLT NR 1080 - PIT - DIVERTED TO PIT, FLIGHT OFFICERS WINDSHIELD CRACKED IN FLIGHT.  MAINTENANCE REPLACED FLIGHT OFFICERS COCKPIT WINDSHIELD.  (M)


REMARKS:
FLT NR 1111 - PIT - RAPID DEPRESSURIZATION AT FL 370.  CABIN CLIMBED AT 2000 FT/MINUTE.  PRESS CONTROLLER WOULD NOT CONTROL CABIN IN STANDBY, MANUAL AC, OR MANUAL DC.  MAINTENANCE REPLACED RIGHT SAFETY RELIEF VALVE.  (M)


REMARKS:
FLT NR 1551 - MCO - RIGHT GEAR INDICATED UNSAFE (NOT LOCKED) AFTER GEAR RETRACTION.  GEAR WAS RECYCLED WITH SAME RESULT.  MAINTENANCE CHECKED LANDING GEAR SENSORS AND INDICATIONS IAW MM.  ALL CHECKED NORMAL.  PERFORMED RETRACTION CHECK IAWMM.  ALL SYSTEMS AND INDICATIONS CHECKED NORMAL.  CLEANED AND LUBED RT GEAR UPLOCK.  (M)


REMARKS:
FLT NR 1974 - CLT - AFT WATER FIRE EXTINGUISHER SEAL MISSING AND IS LEAKING.  MAINTENANCE REPLACED EXTINGUISHER.  (M)


REMARKS:
FLT NR 1951 - BOS - START VALVE OPEN LIGHT CAME ON IN FLIGHT.  RETURNED TO FIELD.  (M)


REMARKS:
FLT NR 388 - JAX - DIVERTED TO JAX, DUE TO START VALVE OPEN LIGHT ILLUMINATED AND NR 2 ENGINE OVERHEAT.  (M)


REMARKS:
FLT NR 1191 - PHL - MAINTENANCE FOUND L2 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP.  MAINTENANCE REPLACED THE BATTERY PACK.  (M)


REMARKS:
DURING SCHEDULED CHECK, FOUND AFT SERVICE DOORWAY SKIN AT LOWER HINGE CUTOUT CRACKED UNDER REINFORCEMENT TAB. REPAIRED PER BOEING DRAWING 65C27269 AND SWA ACO 649-53.


REMARKS:
DURING SCHEDULED CHECK, FOUND A 3 INCH CRACK AT S18R AT BS 747.  REPAIRED PER BOEING SRM.


REMARKS:
PASSENGER COMPLAINED OF STRONG OIL ODOR IN CABIN.  ALSO, FLIGHT CREW EXPERIENCED SAME IN COCKPIT, SEEM TO BE STONGER ATOVERWING EXIT AREA.  REPLACED AIR MACHINE, WATER SEPARATOR BAG AND OPS CHECKED PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT FWD UPPER RADIUS OF DOOR TORQUE TUBE CUTOUT, AT AFT SERVICE DOOR CUTOUT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND NUMBER 2 ENGINE PYLON, UPPER FWD BULKHEAD WEB TO SKIN ATTACH ANGLE CRACKED AT FWD FASTENER STA 222.7.  REPAIRED PER SWA RA 1-257-030.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND LOWER SKIN OF RIGHT HORZI STAB CRACKED BETWEEN STA 120 AND 129.  REPAIRED PER SWA RA 1-355-0215.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD CRACKED AT BS 727 BBL 0.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD SUPPORT ANGLE CRUSHED AND DENTED AT BS 727, BBL 0.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED IN RADIUS AT BS 526 LBL 44 WL 160.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME HAT SECTION ATTACH BRACKET AT BS 887 S9R, BS 847 S9R, BS 827 S9R, BS 787S9R, BS 787 S9R, BS 767 S9R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD GALLEY DOORWAY LOWER AFT CORNER SKIN CRACKED 1 INCH AT BS 327 WL 206 RBL 65.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED 2 PLACES WL 219, LBL 5 TO 12.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED 2 PLACES WL 210 TO 213, RBL 5.7.  REPAIRED PER BOEING SRM.


REMARKS:
FLT NR 818 - PIT - FLIGHT DIVERTED DUE TO LOSS OF PRESSURIZATION.  (M)


REMARKS:
JFK - FLT 880 - AFTER TAKEOF, LEFT ENGINE, SN 4703, SURGED WITH ACCOMPANYING COMPRESSOR STALL AND HIGH EGT.  REDUCED POWER TO IDLE.  FOUND HIGH PRESSURE COMPRESSOR DETERIORATION.  ENGINE TOTAL TIME:  10,716 HOURS; 2,083 CYCLES.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND LEFT FUSELAGE SKIN CRACKED AT BS 740, S17L.  REPAIRED PER BOEING SRM.


REMARKS:
EMERGENCY EXIT LIGHTS WILL NOT TURN OFF AFTER AIRCRAFT SHUTDOWN.  REWIRED REAR SWITCH, REPLACED AFT ENTRY DOOR LIGHT ASSEMBLY AND SECURED AFT FLOOR TRACK LIGHTING BATTERY PACK PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 727, LBL 35 TO 44, WL 180.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND ANGLE CRACKED AT BS 725, LBL 17 WL 230.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, S2R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S25R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 24R CORRODED AT BS 757.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR INNER SKIN CRACKED AT OUTER EDGE CORNER LWR CONTROL BOX CAVITY.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEBS CRACKED AT BS 695 LBL 61 WL 206 AND AT BS 709 RBL 25 WL 205.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACKED UPPER ANGLE ON SHEAR WEB AT BS 384 BL 0 WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACKED LOWER CHORDS AT S5L AND S5R, BS 1138 AND AT BS 1156, LBL 23 AND RBL 23.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIES CRACKED AT BS 1121 BETWEEN S12 AND 13L AND AT BS 360, S13L AND S15L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS CORRODED AT BS 986 LBL 30 TO RBL 51, BS 328 RBL 14 AND 15 WL 208 AND BS 986 WL 208 RBL 5, 24, 32, 43 AND LBL 43.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORTS CORRODED AT BS 957.5 WL 208 RBL 49, BS 1006 TO 1016 WL 208 LBL 6 TO 8 AND AT BS 540 LBL 2 WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907 S4L AND S4R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787 S11L, BS 947 S25R AND S21L AND AT BS 663 S10R AND S10L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT BS 296 RBL 40 WL 274.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492 RBL 37 WL 161.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 663 RBL 65 WL 208.  REPLACED CREASE BEAM CHORD PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 987, S20R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND 3 CRACKS ON BS 178 BULKHEAD ADJACENT TO 2 FASTENERS AT WL 234 RBL 10.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND AFT GALLEY DOOR UPPER HINGE CUTOUT TOP FWD CORNER CRACKED.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND BELT FRAME CRACKED AT BS 807 BL 0.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND FWD CARGO DOOR CRACKED ON FWD LOWER CORNER ADJACENT TO UPLOCK HOOK.  REPAIRED PER SWA TYPICAL REPAIR T1-A25-005.


REMARKS:
INITIATED AIR TURNBACK DUE TO NUMBER 2 ENGINE COMPRESSOR STALL.  AIRCRAFT LANDED AT LAS WITHOUT INCIDENT.  INSPECTED, ENGINE CHANGE UNDERWAY PER BOEING M/M.


REMARKS:
STL - DURING OP-15, FOUND .25 INCH CRACK IN AFT RIGHT LAVATORY FORWARD BULKHEAD, AT OUTBOARD CORNER AT FLOOR LINE.  REPAIRED LAVATORY BULKHEAD PER SRM 53-03, FIGURE 31.


REMARKS:
STL - DURING DESCENT, NR 2 ENGINE, S/N 3231, WAS SHUT DOWN DUE TO FIRE INDICATION LIGHT ILLUMINATION AND FIRE BELL SOUNDED.  BOTH FIRE EXTINGUISHER BOTTLES WERE DISCHARGED.  REMOVED AND REPLACED NR 2 ENGINE FIRE DETECTION CONTROL UNIT, MFGP/N 892809-0400-02.  OPERATIONAL CHECK NORMAL.


REMARKS:
MCI - DURING C-CHECK, FOUND RIGHT WING TANK RIB CRACKED, LOWER STRINGER, 2ND STRINGER, STATION 629, FROM REAR.  STOP DRILLED AND INSTALLED REPAIR PER SRM 57-10-5.


REMARKS:
MCI - DURING C-CHECK, FOUND A .5 INCH CRACK IN LEFT WHEELWELL PRESSURE DECK, LBL 55, STATION 938, AND A .25 INCH CRACK,STATION 948.  STOP DRILLED AND REPAIRED BY INSTALLING DOUBLER PER BOEING DWG 6589360.  (M)


REMARKS:
MCI - DURING C-CHECK, FOUND BOTTOM LEG OF RIB CRACKED ABOVE STRINGER 6, STATION 601.5.  STOP DRILLED PER SRM 51-10-1 AND REPAIRED PER SRM 57-10-5.


REMARKS:
MCI - DURING C-CHECK, FOUND BOTTOM FLANGE OF RIB CRACKED ABOVE STRINGER 5, STATION 6865.  STOPPED DRILLED CRACKS PER SRM 51-10-01 AND REPAIRED PER SRM 57-10-15, FIGURE 2 SHEET, 1 AND FIGURE 1, SHEET 3.  (M)


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND 1.25 INCH CRACK IN FUSELAGE SKIN AT STRINGER 1, STRINGER BOX 1090, INSIDE CENTER ENGINE INLET HOUSING THROUGH BOTH SIDES OF RIVET HOLE, EXTENDING UNDER FAIRING HOUSING HATCH ANGLE.  REPAIRED PER SERVICE BULLETIN 727-53A-0204.  (M)


REMARKS:
MCI - DURING OP-16, FOUND CORROION LOWER FUSELAGE SKIN BETWEEN LONGERONS 27R AND 28R, STATION 740 TO STATION 750.  REMOVED CORROSION PER SRM 51-10-3, INSTALLED REPAIR PER SRM 53-04, FIGURE 53.  (M)


REMARKS:
STL - DURING SPECIAL CHECK, FOUND ONE AND TWO INCH CRACKS IN FUSELAGE SKIN BETWEEN RIVETS AT STATION 817, LONGERON R9, AND A 1 INCH FUSELAGE SKIN CRACK AT STATION 817, LONGERONS R7-R8.  REPAIRED PER SERVICE BULLETIN A53-147, AND DRAWING J060143.  (M)


REMARKS:
MCI - DURING C-CHECK, FOUND A 1.5 INCH CRACK IN CABIN FORWARD DOOR FRAME RIGHT SIDE.  REPAIRED PER SRM 51-40-3, FIGURE 1 AND TWA STANDARD PRACTICES.  (M)


REMARKS:
STL - DURING OP-15, FOUND A TWO INCH CRACK IN FUSELAGE SKIN, FORWARD OF FIRST OFFICERS WIPER BLADE POST.  REPAIRED PER ARA 10023.  (M)


REMARKS:
MCI - DURING C-CHECK, FOUND CRACK ON LOWER CHORD ATTACH BOLT HEAD FLANGE ABOVE EXCESS HOLE, RIGHT WING, W.5738.5.  REPAIRED PER SRM 57-10-05, PAGE 3-5, AND TWA STANDARD PRACTICES.  (M)


REMARKS:
MCI - DURING C-CHECK, FOUND A CRACK AT WS 629 RIB LOWER HOLE, STRINGER 2.  STOP DRILLED PER SRM 57-10-5 AND REPAIRED PER SRM 57-10-5, FIGURE 2 AND TWA STANDARD PRACTICES.  (M)


REMARKS:
STL - DURING OP-15, FOUND CORROSION AT TOP OF SCREW HOLE ON FLOOR BEAM OUTBOARD WALL OF RIGHT LAV, STATION 980.  REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER ARA 10024.


REMARKS:
MCI - DURING OP-16, FOUND RIGHT FRAME BROKEN AT STRINGER 24A, STATION 380.  REPAIRED PER ARA 8913 AND TWA STANDARD PRACTICES.  (M)


REMARKS:
TPA - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR WOULD NOT RETRACT.  FOUND NOSE LANDING GEAR INFLATION LOW DUE TO CRACKED SCHRADER VALVE.  REPLACED SCHRADER VALVE, MFG P/N A00314, AND SERVICED NOSE LANDING GEAR, OPERATION THEN CHECKED NORMAL.


REMARKS:
DURING OP-15, FOUND THREE CRACKS, 1.5 INCH EACH, IN RIGHT FORWARD OVERWING EXIT DOOR PAN, UPPER AFT AND BOTH TOP CLIPS. INSTALLED DOUBLERS AND REPAIRED PER SRM 52-05, FIGURE 51 AND ARA 8897.  (M)


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON INNER SKIN AND DOUBLER, BETWEEN STRINGERS 45R AND 46R, STATION 1830 TO 1840.  CUT OUT CORROSION AND REPAIRED PER ARA 9822.


REMARKS:
JFK - DURING CLIMB, THE FLAPS WOULD NOT FULLY RETRACT.  REMOVED AND REPLACED THE FLAP/SLAT ELECTRONICS UNIT (FSEU), MFGP/N 285T0049-53.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
MCI - DURING OP-16, FOUND CORROSION BETWEEN UPPER SKIN AND REAR SPAR CAP, WS 398.  REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER ARA 8915 AND SRM 57-30-03, FIGURE 9.  (M)


REMARKS:
MCI - DURING OP-16, FOUND POPPED RIVETS AND BULGING SKIN IN FORWARD CARGO BIN CUTOUT FOR E/E DOOR, BETWEEN FS 800 AND FS 820, INBOARD OF STRINGER 46L.  INSTALLED NEW SKIN SECTION PER ARA 9807.  (M)


REMARKS:
DURING OP-16, FOUND CORROSION ON FORWARD FUSELAGE SKIN PANEL FS 740 TO FS 850, STRINGER 44L TO 44R.  INSTALLED NEW SKINPANEL PER ARA 9807.  (M)


REMARKS:
MCI - DURING OP-16, FOUND DOUBLER DISBONDED BETWEEN FS 780 AND FS 800, INBOARD OF STRINGER 45R.  INSTALLED NEW SKIN PANEL PER TWA ARA 9807.  (M)


REMARKS:
MCI - DURING OP-16, FOUND LEFT STRINGER 13A FRAME WEB CRACKED, FS 240.  REPAIRED WEB PER ARA 9626 AND ARA 9629A.


REMARKS:
MCI - DURING OP-16, FOUND 1.5 INCH CRACK IN 1-L DOOR INBOARD SUPPORT ANGLE FOR THRESHOLD PLATE, STATION 467, LBL 90.  CUT UPPER FLANGE OFF 'U' CHANNEL AND REPLACED WITH REPAIR PER ARA 9627.  (M)


REMARKS:
JFK - DURING CRUISE, NR 2 AFT GALLEY SERVING CART EMITTED SMOKE WHEN TURNED ON.  REMOVED AND REPLACED SERVING CART.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED.  REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNALFAILURE, MFG P/N 2589445-933.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING LANDING THE LEADING EDGE SLATS WERE FROZEN AND WOULD NOT DEPLOY.  LEADING EDGE SLAT ACTUATORS AND JACKSCREWS WERE THAWED, LUBRICATED AND SERVICED.  LEADING EDGE SLATS WERE CYCLED NUMEROUS TIMES, OPERATION NORMAL.


REMARKS:
MCI - DURING CLIMB RIGHT ENGINE 'B' FIRE WARNING LOOP FLICKERED ON, SWITCHED TO 'A' LOOP.  AFTER LEVEL OFF AT CRUISE.  'A' LOOP WARNING CAME ON AND WENT OFF.  FOUND LOWER APRON 'A' AND 'B' LOOPS CHAFED.  REPLACED 'A' AND 'B' APRON LOOPS, MFG P/N 5938323-505 AND 5938323-506, AND FIRE WARNING SYSTEM OPERATION CHECKED NORMAL.


REMARKS:
MCI - DURING OP-16, FOUND CRACK AT AFT LATCH AREA OF MID CARGO DOOR SEAL RETAINER AND DOOR FRAME.  REPAIRED PER SRM 52-05, PAGE 110A, FIGURE 26A.


REMARKS:
MCI - DURING C-CHECK, FOUND CRACK IN LEFT FUSELAGE FRAME AT 5TH HOLE FROME BOTTOM OF FUSELAGE FRAME.  REPAIRED PER DWG NR 65C36280, SHEET 1.


REMARKS:
STL - EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 12A.  REMOVED AND REPLACED POWER WIRE, MFG P/N 5853-1.  OPERATIONAL CHECK NORMAL.


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND .375 INCH CRACK AT STATION 408 LONGERON 17R BELTFRAME.  SPLICED IN NEW SECTIONOF BELTFRAME PER SRM 53-03 FIG 32.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON UPPER AND LOWER HORIZONTAL FLANGE AND FWD FACE OF WEB AT STATION 1322 RIGHT SIDE FLOOR BEAM.  CORROSION TASK C5853300.  CLEANED OUT CORRODED AREA AND REPAIRED PER SRM 53-05 FIG 73A AND 79 AND USAIR EA 31736.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT STATION 1338 RIGHT AFT LAV FLOOR BEAMCAP.  CORROSION TASK REF C58-53300.  CUT OUT CORRODED AREA AND ACCOMPLISHED SPLICE REPAIR OF BEAM SECTION PER SRM 53-10-14.  (M)


REMARKS:
PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED FROM LONGERON 28R-29R AT STATION 1338 T-CAP ANGLES AND WEB.  CORROSION TASK REF C50-53300.  REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-10.  (M)


REMARKS:
ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND ONE .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM AT BS 727.  INSTALLEDDOUBLER.  REPAIRED PER EO 5393G256 REV 'A' 11/01/95.  (M)


REMARKS:
ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM WEB AT BS 706.  INSTALLEDDOUBLER.  REPAIRED PER EO 5393G259 REV 'A' 11/01/95.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 CRACKS IN UPPER RADIUS OF FLOOR BEAM AND .5 INCH LONGITUDINAL CRACK BS 520 2 INCH CRACK AT LBL 24 AND RBL 24, AND .5 INCH CRACK AT LBL 45.  INSTALLED REPAIRS AND PREVENTIVE MODIFICATION ON BS 520 FLOOR BEAM PER SB 727-53-1120 REV 1.  REPAIRED PER EA 40569.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CORROSION NUT PLATE HOLE BEAM BS 297 LBL 10 INCH.  REMOVED CORROSION AND INSTALLED STRAP.  REPAIRED PER TR 53-10-01A.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 12 CORRODED AREAS APPROX 1 INCH BY 1 INCH EACH AT FLOOR BEAM, BS 328 RBL 48 AND LBL 48.  SPLICED IN NEW T-CAP.  REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER CLIP, BS 597 S-9 R.  REPLACED CLIP, REPAIREDPER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK IN INTERCOSTAL BS 328 TO 344 LBL 17 INCHES.  INSTALLED NEWINTERCOSTAL.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND DAMAGE ON UNKNOWN DOUBLER 12 INCHES BY 18 INCHES STATION 500B BETWEEN STRINGER 27R AND 26R.  PREVIOUS INSTALLED EXT DOUBLER.  REPAIRED PER SRM 53-30-3.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT STRINGER 27R STATION 1006, 2 INCH BY 1 INCH.  REPAIRED ANDREPLACED SHORT STRINGER SECTION WITH NEW COMPLETE STRINGER.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 1 INCH AT FLOOR SUPPORT 10 PERCENT DEEP AT STRINGER28L STATION 947.  REPAIRED AND REPLACED STR SECTION AND REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 10R.  REPLACED CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED STRINGER TIE CLIP BS 767 STRINGER 10R.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED STRINGER TIE CLIP BS 787 STRINGER 4R.  REPLACED CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED TIE CLIP, BS 807, STRINGER 10R.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED TIE CLIP, BS 827 STRINGER 10R.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER 3L TIE CLIP, AT BS 685.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 5L TIE CIP, BS 685.  REPLACED TIE CLIP.  REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, .1250 INCH CRACK IN STRINGER 2R TIE CLIP, AT BS 685.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK STRINGER 3R TIE CLIP, AT BS 685.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 4R TIE CLIP BS 685.  REPLACED TIE CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 4R TIE CLIP, BS 727 B.  REPLACED TIE CLIP,REPAIRED PER EO NR 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER 3R TIE CLIP AT BS 706.  REPLACED CLIP, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 5L TIE CLIP AT BS 727A.  REPLACED CLIP, REPAIRED PER EO NR 5394G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER 6L TIE CLIP, BS 727B.  REPLACED CLIP, REPAIRED PER EO NR 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 7R TIE CLIP, BS 727B.  REPLACED CLIP, REPAIRED PER EO NR 5393G227.  (M)


REMARKS:
DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 3L, BS 747 AT STRINGER TIE CLIP.  REPLACED CLIP,REPAIRED PER EO NR 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 10R TIE CLIP AT BS 747.  REPLACED CLIP, REPAIRED PER EO NR 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 5R TIE CLIP, BS 727 B.  REPLACED CLIP, REPAIRED PER EO NR 5393G227.  (M)


REMARKS:
PIT - DURING Q-6 INSPECTION, FOUND A .5 INCH CRACK STATION 101 RIGHT SIDE LEADING EDGE OF STROBE IN SKIN.  REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-11.  (M)


REMARKS:
PIT - DURING Q-6 INSPECTION, FOUND TWO CHAFFED 4 INCH RADIUS AREAS FROM LEFT ENGINE THRUST REVERSER CABLE DRUM SHAFT BOLT HEADS IN STATION 1338 AFT PRESSURE BULKHEAD AFT SIDE.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 78-30-14.  (M)


REMARKS:
PIT - DURING Q-6 INSPECTION, FOUND TWO CHAFFED 4 INCH RADIUS AREAS FROM RIGHT ENGINE THRUST REVERSER CABLE DRUM SHAFT BOLT HEADS IN STATION 1338 AFT PRESSURE BULKHEAD AFT SIDE.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 78-30-14.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK FORWARD SERVICE DOOR, FORWARD CUTOUT FRAME AT STATION 295,WL 209.  CUTOUT DAMAGE AND INSTALLED A FLUSH REPAIR.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREA OF CORROSION STATION 947 FLOOR BEAM UPPER FLANGE RBL 4, WL 208.  CUTOUT DAMAGED FLOOR BEAM AND INSTALLED FILLER AND REPAIR ANGLES.  REPAIRED PER SRM 53-60-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.   (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH AREA OF CORROSION INTERCOSTAL UPPER FLANGE STATION 947TO 967, LBL 25, WL 208.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 53 INCHES CORROSION FLOOR BEAM, BS 344 LBL 37 TO RBL 16.  INSTALLED T-CAP AND REPAIR ANGLE AND STRAPS.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.(M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 5 INCHES BY 40 INCHES CORRODED BEAM, BS 312 LBL 18 TO RBL 22.  FABRICATED AND INSTALLED T-CAP AND REPAIR ANGLES.  REPAIRED PER TR 53-10-3.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED INTERCOSTAL BETWEEN BS 294 THROUGH 312 RBL 11.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 50 INCHES CORRODED FLOOR BEAM BS 294.5 RBL 6, RBL 56.  INSTALLED T-CAP AND REPAIR ANGLES AND FILLER, REPAIRED PER SRM 53-10-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND UNKNOWN 4 INCH DIAMETER PREVIOUSLY INSTALLED SKIN DOUBLER, NO SDA ON FILE BS 475 BETWEEN STRINGER 15R AND STRINGER 16R.  DOUBLER INSTALLED PER SRM 53-00-01 FIG 208. (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH AREA OF CORROSION INTERCOSTAL UPPER FLANGE STATION 947TO 967, LBL 51 WL 208.  REPLACED WITH IDENTICAL PART NR 65C333671.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL AREAS .75 INCH BY .75 INCH CORROSION ON FLOOR BEAM STATION 328 RBL 11 TO RBL 57.  SPLICED IN NEW UPPER CHORD SECTION.  REPAIRED PER SRM 53-10-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS LEFT Z-ANGLE BS 947 TO BS 1006. REPLACED WITH IDENTICAL PART NR 65C80735-116.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA AT INTERCOSTAL BS 967 TO BS 986 LBL 16.REPLACED WITH IDENTICAL PART NR 65-46812-169.  REMOVED DEFECTIVE PART COMPLETED INSTALLATION OF INTERCOSTAL.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA INTERCOSTAL BS 967 TO BS 986 RBL 16 INCHES.  REPLACED WITH IDENTICAL PART NR 65-46812-169.  REMOVED DAMAGED PART COMPLETED INSTALLATION OF INTERCOSTAL.  REPAIRED PER SRM 51-10-02.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION IN SEVERAL AREAS (NUTPLATES HOLES) BS 285 TOBS 355 RIGHT SIDE Z-ANGLE.  REMOVED DAMAGED ANGLE COMPLETED INSTALLATION OF Z-ANGLE AND REPAIR PARTS.  REPAIRED PER SRM51-10-2.  CORROSION TASK NR C52-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH DIAMETER SPOTS OF CORROSION (APPROX 25 PERCENT METAL LOSS), RBL 54.5 SEAT TRACK AT BS 336 AT SCREW HOLES.  REMOVED SEAT TRACK, REPLACED SEAT TRACK COMPLETED REPAIR.  REPAIRED PER SRM 53-00-52 FIG 202.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORROSION AT INTERCOSTAL RBL 11 BETWEEN BS 328 THROUGH 344. REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY.5 INCH CORROSION AT INTERCOSTAL LBL 11 BETWEEN BS 312-328.  REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORROSION AT INTERCOSTAL LBL 11 BETWEEN BS 328-344.REPLACED INTERCOSTAL.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH AREA OF CORROSION AT INTERCOSTAL UPPER FLANGE STATION 947 TO 967 LBL 16, WL 208.  REPLACED WITH IDENTICAL P/N BAC1506-43.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL 2 INCH BY 2 INCH CORRODED AREAS AT BS 947 TO BS 1006 RIGHT SIDEZ-ANGLE.  REMOVED RIGHT SIDE Z-ANGLE, COMPLETED INSTALLATION OF RIGHT SIDE Z-ANGLE.  REPAIRED PER SRM 51-10-02, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED NUT PLATE HOLES FLOOR BEAM, BS 986 LBL 45 INCHES TO RBL 45 INCHES.  MODIFIED PART NR INSTALLED, EXT BAC1505-100703, 7075-T65, BAC1490-2887 AND 2886.  REMOVEDDAMAGED T-CAP.  COMPLETED INSTALLATION OF T-CAP ON FLOOR SEAL AT BS 986.5.  REPAIRED PER EA 40627.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH AREA SURFACE CORROSION AT INTERCOSTAL, BS 336, RBL 59,WL 208.  REPLACED CORRODED INTERCOSTAL WITH NEW PART.  REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORRODED AREA AT FLOOR STRINGER, BS 787 TO BS 847 RBL 14 INCHES.  REMOVED DAMAGED FLOOR STRINGER, COMPLETED INSTALLATION AND REPAIR OF FLOOR STRINGER.  REPAIRED PER SRM 53-00-53 FIG 202 ALSO, SRM 51-10-2.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA BL 0 BS 360, FLOOR BEAM.  FABRICATED AND INSTALLED REPAIR ANGLE.  REPAIRED PER SRM 53-30-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK UPPER T-CAP IN RADIUS BS 520 RBL 45.5, BEAM.  CONTAINED CRACK INSTALLED U-CHANNEL AND RADIUS BLOCKS AND COMPLETED REPAIR, EA 40649.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH GROOVE WORN INTO CHANNEL ON CABIN FLOOR BEAM AT BS 520 AT BBL 0.  INSTALLED REPAIR PER SB AND EA.  REPAIRED PER SB 737-53-1120 REV 1 AND REV 2 AND EA 40548.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1875 GROOVE WORN IN CHANNEL ON CABIN FLOOR BEAM, BS 520 AT LBL 24.75.INSTALLED REPAIR PER SB AND EA, REPAIRED PER SB 737-53-1120 REV 1 AND EA 40649. (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1875 INCH GROOVE WORN INTO CHANNEL ON CABIN FLOOR BEAM, BS 520 AT RBL 24.75.  INSTALLED REPAIR PER SB AND EA.  REPAIRED PER SB 737-53-1120 REV 1 AND EA 40649.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND A 12 INCH LONG BY 2 INCH WIDE BY .250 INCH DEEP DENT IN THE FUSELAGE SKIN LOCATED AT STATION 390 BETWEEN STRINGER 28R AND STRINGER 24R.  INSTALLED DOUBLER (TIME LIMITED REPAIR) AS PER USAIR EA NR 40719.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORROSION AT CABIN FLOOR SUPPORT ANGLE, STATION 292 TOSTATION 300 LBL 12.  REPLACED ANGLE, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH CORROSION ON BEAM AT BS 277-294.5 LBBL 12.  REPLACED ANGLE, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER TIE CLIP, STATION 1064 STRINGER 17L.  INSTALLED NEW TIE CLIP MFG PER BOEING DRAWING 69-40276.  REPAIRED PER BOEING ASSEMBLY DRAWING 69-40276.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION INTERCOSTAL STATION 927 TO STATION 947 RBL 8INCH.  INSTALLED NEW INTERCOSTAL.  REPAIRED PER DRAWING 65-67316.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 747 STRINGER 6R.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 47.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35353-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 520 LBL 25 WL 207.75 UPPER CHORD FLOOR BEAM.  STOP DRILLED CRACK .25 INCH.  INSTALLED REPAIR DOUBLER AND FLOOR BEAM MOD.  REPAIRED PER EA 40741.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .1875 INCH BY 3 INCH AND .1875 INCH BY 2 INCH CORROSION AT CABIN FLOOR SUPPORT ANGLE, BS 292 THROUGH BS 300.  REPLACED SUPPORT ANGLE, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION PIT, TOP CAP FLOOR BEAM, STATION 328 AT RBL 20.  REMOVED TOP 'T' OF FLOOR BEAM AND INSTALLED NEW T-CAP.  REPAIRED PER TYPICAL REPAIR 53-10-13.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT TIE CLIP, STATION 1064 STR 9 L.  REPLACED CRACKED TIECLIP WITH ONE FABRICATED PER ORIG DRAWING.  REPAIRED PER BOEING DRAWING 69-40276.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT FRAME BS 616, 5 INCHES BELOW FLOOR LEVEL LEFT SIDE.  CUT OUT DAMAGE, INSTALLED ANGLE AND FILLER.  REPAIRED PER EA 40740.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION FLOOR BEAM FS 328 RBL 20 1/2.  REMOVED DAMAGED 'T' CHORD FROM LBL 29 TO RBL 65.  REPAIRED PER TYPICAL REPAIR NR 53-10-13 AND SRM CHAPTER 51-40-2 FIG 1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH CORROSION STATION 308 LBL 24 TO LBL 30 ANGLE AT BULKHEAD.  REPLACED ANGLE, REPAIRED PER SRM 51-10-01.  (M)


REMARKS:
INT -DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 616, 5 INCHES FLOOR LEVEL RIGHT SIDE FRAME.  CUT OUT DAMAGE INSTALLED ANGLE AND FILLER.  REPAIRED PER EA 40740.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 17 INCHES BY 2 INCHES CHAFFED AND FRETTING LEFT CHORD BS 710 TO BS 727. FABRICATED WASHERS AND STRAP AND INSTALLED.  REPAIRED PER EA 40745.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH STATION 307 LBL 11 TO LBL 42 AT CHANNEL.  REPLACED CHANNEL.  REPAIRED PER SRM 51-10-01.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACK IN WEB 4 INCHES AT FLOOR BEAM, BL O, STATION 706-710.  CUTOUT CRACKED WEB AND INSTALLED FILLER AND DOUBLER.  REPAIRED PER BOEING REPAIR DRAWING NR 65C34537.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BLEND OUT AFT CARGO FORWARD FRAME BS 794 STRINGER 19R THROUGH STRINGER 20R.  INSTALLED DOUBLER.  REPAIRED PER SRM 51-40-3.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORROSION FLOOR BEAM STATION 312, LBL 11 TO RBL 11.  REPLACED T-CAP.  REPAIRED PER TR 53-10-13.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACK IN WEB CUT OUT FOR LEFT AILERON BELLCRANK (1 INCH CRACK), BS 680 LBL 24 AND RBL 24 WEB OF FLOOR BEAM AT AILERON CUTOUT.  INSTALLED REINFORCEMENT.  REPAIRED PER EA 40739 AND SB 737-53-1130, R 4 FIG 5.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 706 STRINGER 4L TIE CLIP.  INSTALLED NEW TIE CLIP.  REPAIRED PER EA 5393G227.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP, STRINGER 4R, BS 685.  INSTALLED NEW TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35852-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 PLACES 3 INCHES BY 8 INCHES AND 3 INCHES BY 20 INCHES FLOORBEAM T-CAP, BS 344 LBL 55 AND RBL 8 TO LBL 14.  REPLACED 4 FEET OF T-CAP.  REPAIRED PER TR 53-10-13.  (M)


REMARKS:
INT - DURING Q-4 CHECK HIGH FREQUENCY EDDY CURRENT, FOUND .0625 INCH CRACK BS 520 LBBL 45.50 FLOOR BEAM.  INSTALLED DOUBLER.  REPAIRED PER EA 40741 SB 737-53-1120.  (M)


REMARKS:
INT - DURING Q-4 EDDY CURRENT INSPECTION, FOUND .5 INCH CRACK BS 520 RBBL 45.50 FLOOR BEAM.  INSTALLED DOUBLER.  REPAIRED PER EA 40741 SB 737-53-1120.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 520 RBBL 25 FLOOR BEAM.  INSTALLED DOUBLER.  REPAIRED PER EA 40741 SB 737-53-1120.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 6 RT.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 693535214.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 727 A STRINGER 7A.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 6R.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STRINGER 7R BS 747.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 787, STRINGER 5R.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT TIE CLIP BS 767, STRINGER 7L.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 727 RBL 6.5 KEEL BEAM VERTICAL STIFFENER FITTING.  REPLACED FITTING, REPAIRED PER BOEING DRAWING 65-46547.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT TIE CLIP BS 787, STRINGER 8L.  REPLACED TIE CLIP.  REPAIRED PER EO 5393G227.  MODIFIED PART NR INSTALLED 6935352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT TIE CLIP, BS 616 STRINGER 2L.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER 2R BS 727A, AT STRINGER TIE CLIP.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STRINGER 2R, BS 616.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 6935352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 3R BS 616 STRINGER TIE CLIP.  REMOVED AND REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 653535214.  (M)


REMARKS:
INT -DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 807 STRINGER 4L AT TIE CLIP.  INSTALLED NEW CLIP.  REPAIRED PER EA 5393G227.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER 5R BS 727B AT STRINGER TIE CLIP.  INSTALLED NEW MODIFIED TIE CLIP PER EO 5393G227.  REPAIRED PER EO 5393G227.  MODIFIED PART NR INSTALLED 6935352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STRINGER 4R, BS 727B.  INSTALLED NEW TIE CLIP PER EO 5393G227, REPAIRED PER EO 5393G227.  MODIFIED PART NR INSTALLED 69-3532-14. (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 807 STRINGER 5L TIE CLIP.  INSTALLED NEW CLIP.  REPAIRED PER EA 5393G227. (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER 6R BS 727B AT STRINGER TIE CLIP.  INSTALLED NEW CLIP.  REPAIRED PER EA 5393G227.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STRINGER 4R BS 727A.  REMOVED DAMAGEDTIE CLIP, REPLACED AND COMPLETED INSTALLATION OF TIE CLIP.  REPAIRED PER EA 53936227.  DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT STRINGER TIE CLIP STRINGER 4R BS 616.  REPLACED TIE CLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35-352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK TIE CLIP BS 727B S-1 L.  REPLACED TIE CLIP.  REPAIRED PEREO 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK TIE CLIP BS 727B STRINGER 8L.  REPLACED TIE CLIP.  REPAIRED PER EO 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT STRINGER TIE CLIP STRINGER 6R BS 727A.  REPLACED TIECLIP.  REPAIRED PER EA 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 24 INCH CORROSION AT CABIN FLOOR BEAM STATION 947 LBL 12 INCHES TO RBL 12 INCHES.  INSTALLED T-CAP AND REPAIRED DOUBLERS.  REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA INTERCOSTAL STATION 947 TO 967 LBL 17 INCHES.  REMOVED AND REPLACED WITH NEW INTERCOSTAL.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 17 INCH STR 27L CORRODED AT STATION 947 STRINGER 27L.  REPAIRED STRINGER STR SPLICE, REPAIRED PER SRM 53-10-3, PG 3.  (M)


REMARKS:
ROA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND HINGE CUTOUT AFT ENTRY DOOR SKIN.  INSTALLED DOUBLER,REPAIRED PER SRM 53-30-03 FIG 34.  (M)


REMARKS:
INT - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK AT SHEAR BEAM STRINGER 18A, STATION 706.  INSTALLED REPAIR ANGLES AND DOUBLERS.  REPAIRED PER EO 5393G256 PART 3 SECTION IV.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND AN 8 INCH BY 8 INCH CORROSION EXTERNAL DOUBLER NOT PER SRM LOCATED AT FS 1681.8 THROUGH1701 BETWEEN STRINGER 17 AND STRINGER 19L.  FABRICATED AND INSTALLED EXTERIOR DOUBLER AS PER USAIR EA 40578 AND BOEING SRM 53-60-10.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION APPROXIMATELY 1 INCH, LOCATED TOP AND LOWER SURFACE OF FLOOR BEAM UPPER CHORD.  SPLICED UPPER CHORD OF FLOOR BEAM AS PER BOEING SRM 53-00-01.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT CLIP NUTHOLES, TOP SURFACE 58 INCHES AT BS 1640 BETWEEN LBL 58 TO BL 0.  REPAIRED ENTIRE LENGTH OF UPPER CHORD FLOOR BEAM AT BS 1640.  REPLACEMENT OF UPPER CHORD INSTALLED AS PER USAIR EA 40609.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER, 2 INCHES LOCATED INBOARD PYLON IN AREA OF HEAT SHIELD NR 2 PYLON.  REPLACED PYLON SKIN INBOARD AS PER USAIR 40605 AND USAIR EO 5492R274.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND AN EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER 4 INCHES OUTBOARD PYLON SKIN IN AREA OF HEAT SHIELD NR 2 PYLON.  REPLACED PYLON SKIN OUTBOARD AS PER USAIR EA 40605, EA 40669 AND USAIR EO 05492R274. (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND A SHARP DENT 1 INCH DIAMETER .145 INCH DEEP, 3 INCHES FORWARD BS 1280 BETWEEN STRINGER 1280 BETWEEN STRINGER 24L AND STRINGER 25L.  INSTALLED FLUSH PATCH REPAIR AS PER BOEING SRM 53-00-01.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND A DENT 1 INCH DIAMETER BY .50 INCH DEEP (APPROXIMATELY 1.25 INCH BY .75 INCH) LOCATED AT BS 1738, S27L.  INSTALLED DOUBLER AS PER USAIR EA 58015 AND BOEING SRM 53-00-01.  (M)


REMARKS:
CLT - INSPECTION VISUALLY AND BY HFEC, FOUND A DENT 5.5 INCH BY 3.75 INCH BY .130 INCH DEEP IN THE FUSELAGE SKIN LOCATED AT BS 231.5, OUTBOARD CHORD ABOVE AOA VANE.  REPLACED CHORD ANGLES AND REPAIRED W/SKIN FILLER AND DOUBLER AS PER EA 40596.  (M)


REMARKS:
PIT - DURING SIP INSPECTION, FOUND .25 INCH CRACK IN THE LOWER AFT APERTURE FRAME CORNER SIP REF 53-10-20 EDDY CURRENT. REMOVED DAMAGED AREA AND INSTALLED FILLER PLUG AND 2 DOUBLERS PER SRM 53-02-16.  (M)


REMARKS:
PIT - DURING SIP INSPECTION, FOUND 2 CRACKS, .25 INCH FWD AND .25 INCH AFT SED UPPER APERTURE FRAME CORNERS, SIP REF 53-10-20 EDDY CURRENT.  REMOVED DAMAGED AREAS AND INSTALLED DOUBLER REPAIR AND FILLER PLUGS PER USAIR TYPICAL REPAIR 53-10-04.  (M)


REMARKS:
PIT - DURING SIP INSPECTION, FOUND 2 CRACKS, 3 INCHES AND 1.5 INCHES A REPAIR DOUBLER AT THE FORWARD PRESSURE BULKHEAD FS 1550 AFT SIDE OF LOWER CONNECTION ANGLE SIP REF 53-10-06 VISUAL/EDDY CURRENT.  REMOVED DOUBLERS, STOP DRILLED CRACKS AND INSTALLED NEW DOUBLERS PER SRM 53-02-18.  (M)


REMARKS:
CLT - FLIGHT NR 328 - UPON TAKEOFF AT CLT, THE NR 3 MAIN TIRE LOST THE RECAP.  GEAR WAS NOT RETRACTED.  FLIGHT RETURNEDTO FIELD AT CLT AND LANDED WITHOUT INCIDENT.  MAINTENANCE REPLACED THE NR 3 AND NR 4 (P/N 3910063507) WHEELS, A MAIN LANDING GEAR SENSOR (DAMAGED), A RIGHT INBOARD TRAILING EDGE FLAP PANEL (DAMAGED), AND THE C1 FAN ASSEMBLY ON THE RIGHT ENGINE (DAMAGE).  (M)


REMARKS:
SYR - UPON TAKEOFF FROM SYR, CREW RECEIVED NOSE AND LEFT MAIN GEARS UNSAFE LIGHTS.  NEITHER GEARED RETRACTED.  FLIGHT RETURNED TO SYR AND LANDED WITH NO FURTHER INCIDENT.  THE AIRCRAFT WAS FERRIED TO PHL, WHERE IT WAS JACKED AND THE GEAR SWUNG.  NO DEFECTS WERE NOTED.  MAINTENANCE LUBED THE GEAR AND RELEASED THE AIRCRAFT FOR SERVICE.  (M)


REMARKS:
MCO - AFTER TAKEOFF FROM MCO, NOSE GEAR WOULD NOT RETRACT.  FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT. (M)


REMARKS:
MCO - AFTER TAKEOFF FROM MCO, NOSE GEAR WOULD NOT RETRACT.  CREW TRIED TO CYCLE THE GEAR TO NO AVAIL.  FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED BOLTS IN THE NOSE GEAR SPRAY DEFLECTOR AND LUBED THE GEAR.  (M)


REMARKS:
PIT - FLIGHT WAS HOLDING FOR LANDING AT PHL WHEN BOTH AUTO PRESSURE CONTROLLERS FAILED AND CABIN ALTITUDE BEGAN TO CLIMB.  CREW DECLARED AN EMERGENCY.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT PACK CONTROL VALVE DUE TO LOW FLOW.  (M)


REMARKS:
ALB - AFTER TAKEOFF, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION.  EXTENDED GEAR, NORMAL INDICATIONS WERE RECEIVED.  ATTEMPTED SECOND RETRACTION AND GEAR LEVER WOULD NOT MOVE.  FLIGHT RETURNED TO ALB AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE INSPECTED THE GEAR AND FOUND THE NITROGEN CHARGE IN THE NOSE GEAR LOW.  GEAR WAS SERVICED AND RELEASED FOR SERVICE.  (M)


REMARKS:
BHM - ON MAINTENANCE FERRY FLIGHT, AFTER TAKEOFF, CREW NOTED RANCID BURNING SMELL.  CREW DECLARED AND EMERGENCY AND THEFLIGHT RETURNED TO BHM.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THAT A BIRD HAD BEEN INJESTED CAUSING THE SMELL.  ALL APPROPRIATE INSPECTIONS WERE COMPLETED AND THE WATER SEPARATOR BAG CHANGED.  (M)


REMARKS:
PIT - EMERGENCY LIGHT WERE ILLUMINATED WITH THE SWITCH IN THE OFF POSITION.  MAINTENANCE REPLACED TWO EMERGENCY LIGHT POWER SUPPLIES.  (M)


REMARKS:
PIT - ON GEAR EXTENSION CREW RECEIVED THREE UNSAFE GEAR INDICATIONS.  CREW CYCLED THE GEAR AND RECEIVED THREE SAFE INDICATIONS.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE R2-28 LANDING GEAR LEVER RELAY, AND SWUNG THE GEAR.  (M)


REMARKS:
CLT - CREW RECEIVED FAULT LIGHT ON LEFT ELECTRIC BUS.  RESET WOULD NOT CURE PROBLEM.  APU STARTED, BUT IT WOULD NOT POWER THE BUS.  FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT GENERATOR.  (M)


REMARKS:
PIT - DURING ANNUAL OPERATIONAL CHECK OF THE TAIL CONE EVACUATION SYSTEM, TAIL CONE WAS DROPPED BUT THE HARD COVER WHICH PROTECTS THE SLIDE WAS NOT RELEASED.  THIS PREVENTED THE SLIDE FROM BEING DEPLOYED.  MAINTENANCE WAS NOT ABLE TO DETERMINE WHY THE COVER REMOVAL WAS NOT INITATED.  THE TAILCONE WAS REINSTALLED AND RIGGED, AND REDEPLOYED.  THE SYSTEM PERFORMED CORRECTLY, RESULTING IN A GOOD SLIDE DEPLOYMENT.  PER USAIR STANDARD PRACTICES, TWO MORE OPERATIONAL CHECKS WILL BEPERFORMED ON THIS SYSTEM, AND AN INVESTIGATION INITIATED.  (M)


REMARKS:
ORD - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW RECEIVED THREE RED LIGHTS.  GEAR WAS CYCLED, CREW RECEIVED GREEN INDICATIONS FOR THE MAINS BUT A RED FOR THE NOSE GEAR.  FLIGHT RETURNED TO ORD AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANACE ACTION PENDING.  (M)


REMARKS:
ORD - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW COULD NOT RETRACT THE NOSE GEAR.  THIS IS THE SECOND RETURN TO FIELD OF THIS FLIGHT ON THIS DAY.  MAINTENANCE ACTION PENDING.  (M)


REMARKS:
FLT NR 1488 - RIC - SHORTLY AFTER GEAR RETRACTION THE FOLLOWING ALERTS, 'LD FAULT', 'STAB TRIM CONFIG' AND 'TCAS'.  WHEN GEAR EXTENDED, LOUD RELAY CLICKING FOLLOWED BY ALL MESSAGES CLEARING.  MAINTENANCE ADJUSTED THE LEFT MAIN GEAR NR 3 PROXIMITY SENSOR AND SWUNG THE GEAR.  (M)


REMARKS:
CLT - AFTER TAKEOFF, CREW RECEIVED GND/FLT FAULT, LIFT DUMPER FAULT, TCAS FAULT AND PROX SW SYS INOP.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR HARNESS AND THE SENSOR.  (M)


REMARKS:
PIT - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE IN AUTOMATIC OR MANUAL MODES.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REACTIVATED THE OUTFLOW VALVE WHICH WAS DEACTIVATED DUE TO PREVIOUS WORK.  (M)


REMARKS:
GSO - AFTER TAKEOFF, CREW RECEIVED THE RED WARNING LIGHT FOR THE RIGHT MAIN LANDING GEAR.  CREW COULD NOT GET THE LIGHTTO EXTINGUISH.  FLIGHT RETURNED FILED AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE ADJUSTED THE RIGHT GEAR UPLOCK BRACKET.  (M)


REMARKS:
PIT - AFTER TAKEOFF, CREW RECEIVED LEFT AND RIGHT MAIN LANDING GEAR WARNING ON THE MFDU.  THE GEAR WAS CYCLED WITH THE SAME RESULT.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE LANDING GEAR TEST VALVEIN THE TEST POSITION.  THE SWITCH WAS SAFETIED AND THE AIRCRAFT RELEASED FOR SERVICE. (M)


REMARKS:
CLT - CREW RECEIVED 'WING FLAP ASYMMETRY' WARNING LIGHT, AFTER TAKEOFF.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE SQUIRREL CAGE DRIVE COUPLING BROKEN AND REPLACED IT.  (M)


REMARKS:
CHS - AFTER TAKEOFF, CREW WOULD NOT GET THE MAIN GEAR TO RETRACT.  THE GEAR WAS CYCLED TWICE.  FLIGHT RETURNED TO CHS AND LANDED WITH NO FURTHER INCIDENT.  AIRCRAFT FERRIED TO CLT FOR REPAIR.  MAINTENANCE REPLACED THE RIGHT GEAR DOOR SEQUENCING 'A' VALVE.  GEAR SWING COMPLETED.  (M)


REMARKS:
CLT - AFTER TAKEOFF, THE CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE.  THE CREW DECLARED AN EMERGENCY.  THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.  THIS INCIDENT WAS SIMILAR TO A PREVIOUS INCIDENT OCCURING ON 1/25/96.  MAINTENANCE REPLACED BOTH PACK WATER SEPARATOR BAGS DUE TO OIL CONTAMINATION FROM THE APU.  THE APU WAS REPLACED.  (M)


REMARKS:
CAE - UPON TAKEOFF FROM CAE, CREW RECEIVED AURAL AND VISUAL FIRE WARNINGS ON THE NR 2 ENGINE AND THE START VALVE LIGHT. CREW SECURED THE ENGINE AND THE WARNINGS STOPPED.  FLIGHT RETURNED TO CAE AND LANDED WITH NO FURTHER INCIDENT.  SET 20MINUTES.  HEAT FROM THE STARTER CAUSED THE FIRE WARNING.  MAINTENANCE REPLACED THE STARTER AND THE RIGHT ENGINE OUTBOARD FIRE DETECTION LOOP.  (M)


REMARKS:
CHS - EN ROUTE MCO-IAD - CREW NOTED ELECTRICAL IN SMELL IN CABIN.  FLIGHT DIVERTED TO CHS AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE GASPER FAN.  (M)


REMARKS:
TPA/ATL - ON FLT 210 - THE CAPTAIN DECLARED AN EMERGENCY FOR THE LEFT GENERATOR FAILURE.  RIGHT GENERATOR DID NOT CROSS-TIE.  NO POWER TO LEFT BUS AND LOST RADIO COMMUNCATIONS.  REMOVED AND REPLACED LEFT GENERATOR, RESECURED CONNECTOR AT PYLON AND FOUND PHASE 'B' AT PYLON LOOSE.  RAN ENGINE AND X-TIED, ALL SYSTEMS OPS CHECKED OK.


REMARKS:
DURING SCHEDULED CHECK, FOUND AFT CARGO BELT FRAME AT BS 807 HAS CORRODED SHEAR TIE BETWEEN S27 AND 26R.  REPLACED PER BOEING SRM.


REMARKS:
LGW - FLT 721 - DURING CLIMB, SHUT DOWN NR 4 ENGINE, SN 4103, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATING.  FOUND OIL AND OIL FILTER HIGHLY CARBONATED.  REPLACED ENGINE, SN 4103.  ENGINE OPERATION CHECKED NORMAL.  CHECK C-1 - 11-14-94 - JFK.  SUPPLEMENTAL DATA - INVESTIGATION OF NR 4 ENGINE, SN 4103, OIL FILTER BYPASS LIGHT ILLUMINATION REVEALED NR 3 BEARING TUBE ASSY LEAKING AT THE JOINT ALLOWING CARBON THAT HAD BUILT UP IN THE NR 3 BEARING COMPARTMENT TO MIGRATE TO THE FILTER CAUSING THE BYPASS INDICATION.  ENGINE, SN 4103, REPAIRED AND RETURNED TO SERVICE.


REMARKS:
LAX - FLT 8595 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, SN 4626, DUE TO SURGING.  REMOVED AND REPLACED RT ENGINE BLEED CONTROL VALVE, MFG PN 773333-3.  PERFORMED BORESCOPE INSPECTION OF 5TH, 6TH, 8TH, AND 14TH COMPRESSOR STAGES AND 1ST, 2ND, AND 3RD TURBINE STAGES.  NO DISCREPANCIES FOUND.  OPERATIONAL CHECK NORMAL.  ENGINE TOTAL TIME:  34,097 HOURS; 8,432 CYCLES.  CHECK C-4C - 10-25-95 - LAX.


REMARKS:
ATL - FLT 605 - DURING LANDING TOUCHDOWN LEFT AND RIGHT ENGINES, 2164-L, 2146-R, SPOOLED DOWN.  COMPLETED LANDING PROCEDURES.  REPLACED LEFT ENGINE FUEL CONTROL, MFG PN 243602-4, AND RIGHT ENGINE FUEL CONTROL, MFG PN 243602-3.  ENGINE OPERATION AND PERFORMANCE CHECKED NORMAL.  LEFT ENGINE S/N 2164 - TOTAL TIME:  51,272 HOURS, CYCLES, 60,004.  RIGHT ENGINE S/N 2146 - TOTAL TIME:  56,299 HOURS, CYCLES, 66,976.  CHECK C-5-14-95 - STL.  REFERENCE OPERATOR CONTROL NR 96ZZZX224.


REMARKS:
ATL - FLT 605 - DURING LANDING TOUCHDOWN LEFT AND RIGHT ENGINES, 2164-L, 2146-R, SPOOLED DOWN.  COMPLETED LANDING PROCEDURES.  REPLACED LEFT ENGINE FUEL CONTROL, MFG PN 243602-4, AND RIGHT ENGINE FUEL CONTROL, MFG PN 243602-3.  ENGINE OPERATION AND PERFORMANCE CHECKED NORMAL.  LEFT ENGINE S/N 2164 - TOTAL TIME:  51,272 HOURS, CYCLES, 60,004.  RIGHT ENGINE S/N 2146 - TOTAL TIME:  56,299 HOURS, CYCLES, 66,976.  CHECK C-5-14-95 - STL.  REFERENCE OPERATOR CONTROL NR 96ZZZX223.


REMARKS:
MIA - FLT 149 - DURING CRUISE, LOST OIL RESULTING IN AN ENGINE SHUTDOWN AND DETERMINED HIGH SPEED.  MAIN GEAR BOX 29136, S/N 610200 FAILED.  REMOVED AND INSTALLED NEW GEAR BOX.  LEAK CHECK AND OPERATIONS NORMAL.


REMARKS:
MCI - DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED RIGHT SIDE WL 280.6, STATION 689.  INSTALLED REPAIR PER ARA 9471 ANDTWA STANDARD PRACTICES.


REMARKS:
STL - DURING C-CHECK, FOUND .5 INCH CRACK AT BOTH ATTACH POINTS TO BELTRING, LONGERON 6R, STATION 718.  REPAIRED PER SRM 53-02, FIGURE 2A.


REMARKS:
STL - DURING C-CHECK, FOUND ONE 2 INCH CRACK IN LONGERON 4L, LOWER LEG, STATION 737.  REPAIRED PER SRM 53-02, FIGURE 2A.


REMARKS:
MCI - DURING OP-16, FOUND A 3 INCH CRACK LEFT SIDE AT SIDEWALL UNDER FLOOR MEMBRANE, FS 1280.  REPAIRED PER SRM 53-05-96.


REMARKS:
STL - DURING C-CHECK, FOUND .5 INCH CRACK IN LOWER FLANGE OF LONGERON 7L, STATION 699.  REPAIRED PER SRM 53-02, FIGURE 2A.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON NR 2 CHAIR TRACK, FS 1130 AND FS 1142.  INSTALLED NEW TRACK PER SRM 51-01, PAGE 1.


REMARKS:
STL - DURING CRUISE, NR 12 FLIGHT SPOILER, MFG P/N 65-17347-81A, DELAMINATED CAUSING EXTREME AIRFRAME BUFFETING.  REMOVED AND REPLACED NR 12 FLIGHT SPOILER AND RIGGED.  OPERATIONAL CHECK NORMAL.


REMARKS:
MCI - DURING OP-16, FOUND FLOOR BEAM CORROSION, FS 1309, LBL 45. REMOVED CORROSION PER SRM 51-10-3, REPAIRED BEAM PER SRM 53-05, FIGURE 20A.


REMARKS:
MCI - DURING OP-16, FOUND LOWER FUSELAGE SKIN CORROSION, STATION 775 TO 827, RB 273.  REPAIRED EPR SRM 53-04, PAGE 321.


REMARKS:
MCI - DURING OP-16, FOUND FLOOR BEAM CORROSION BETWEEN FLOOR TRACKS, FS 1211.  REPAIRED PER SRM 51-01, PAGE 1 AND TWA STANDARDS PRACTICES.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FUSELAGE SKIN BELOW AFT CARGO BIN DOORWAY UNDER COVER PLATE, STATION 1155-1212.REMOVED CORROSION PER SRM 51-10-3.


REMARKS:
ON FLT NR 511 - ATL-ATL - AIR RETURN, THE RIGHT HYDRAULIC PRESSURE INDICATED ZERO IN FLIGHT.  THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP SHAFT WAS SHEARED.  THE PUMP WAS REPLACED.  (M)


REMARKS:
ON FLT 549 - ATL-ATL - AIR RETURN, ON TAKEOFF THE LEFT GEAR UNSAFE AND GEAR DOOR WARNING LIGHTS ON.  RECYCLED GEAR AND GOT THREE GREEN WITH GEAR DOORS CLOSED.  FOUND LEFT MLG DOOR SEQUENCE ARM BROKEN, REPLACED ARM AND PERFORMED MLG MECHANICAL CONTROL PUSH PULL CABLE RIG CHECK PER MM 52-31-0 PARA 3B.  SYSTEM OPS CHECK GOOD.  (M)


REMARKS:
ON FLT NR 116 - ATL-ATL - AIR RETURN, RIGHT PACK INOP AFTER TAKEOFF, NO PRESSURE INDICATION OR AIR FLOW.  FOUND CLAMP LOOSE ON RIGHT ACM AND BROKEN CLAMP ON RIGHT WATER SEPARATOR.  SECURED LOOSE CLAMP ON ACM AND INSTALLED CLAMP ON WATER SEPARATOR.  PRESSURIZATION AND AIR CONDITIONING OPS CHECK NORMAL.  (M)


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK FORWARD OF AFT END OF TRACK AT SCREWS, LBL 36, STATION 1136.  REMOVED CORROSION PER SRM 51-10-3, AND REPLACED TRACK PER SRM 51-10-1C.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON 'E' GALLEY AFT INBOARD HOLD DOWN TRACK, STATION 1302 TO STATION 1281.  REPLACED TRACK PER SRM 53-03, PAGE 10G.


REMARKS:
MCI - DURING OP-16, FOUND FORMER FRAME CORROSION BETWEEN LONGERONS 29L TO 29R, FS 1322.  REPAIRED PER SRM 53-03, PAGE 4E AND SSRM 51-40-501.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON BULKHEAD SUPPORT MEMBER, FS 1320, LBL 25L TO LBL 31L.  REPAIRED PER SRM 51-01, PAGE 1C AND TWA STANDARD PRACTICES.  (M)


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR PANEL SUPPORT BEAM BL, FS 1155.  INSTALLED NEW BEAM PER SRM 51-01, PAGE 1CAND TWA STANDARD PRACTICES.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON RIGHT FLOOR SUPPORT, FS 1155.  INSTALLED NEW FLOOR SUPPORT PER SRM 51-01, PAGE 1C AND TWA STANDARD PRACTICES.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION AT FLOOR BEAM, LEFT AFT LAVATORY FORWARD BULKHEAD LOWER END.  REPAIRED PER SRM 53-01, FIGURE 4, SHEET 3.


REMARKS:
MCI - DURING OP-16, FOUND CABIN FLOOR PANEL CORROSION, STATION 1305 TO STATION 1309.  REPLACED FLOOR PAN PER SRM 51-10-01.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON LEFT FLOOR CARGO TRACK, FS 1079 TO FS 1222.  INSTALLED NEW TRACK PER SRM 51-10, ITEM 1, FIGURE C AND INSTALLED SPLICE PER SRM 53-03, FIGURE 4G.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION BOTTOM SIDE IN FORMER ATTACH BRACKET, FS 1155, LBL 7.  REPAIRED PER SRM 51-01, PAGE1, ITEM C AND TWA STANDARD PRACTICES.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR BEAM CAP, FS 480, RIGHT SIDE.  REMOVED CORROSION PER SRM 51-10-01 AND REPAIRED PER ARA 9622.


REMARKS:
STL - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT, IT WAS DETERMINED THAT THE NOSE GEAR WAS DOWN AND LOCKED.  REMOVED AND REPLACED NOSE GEAR SEAL KIT, MFG P/N A03772REVH.  GEAR SWING CHECKED NORMAL.


REMARKS:
MCI - DURING CRUISE, CREW WAS UNABLE TO TRANSFER FUEL OUT OF THE CENTER TANK.  REMOVED AND REPLACED WORN CENTER BOOST PUMP ON-OFF SWITCH, MFG P/N 4TL62-3.  OPERATIONAL CHECK NORMAL.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION AT STRINGER WEB OF STRINGER 29L, FS 1155.  REPAIRED PER SRM 51-10-3 AND TWA STANDARD PRACTICES.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK, STATION 160 TO STATION 200, RBL 53.  REPLACED TRACK PER SSRM 51-10-01.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FORMER TO STRINGER ATTACH ANGLE OF STRINGER 29L, FS 1155.  REPAIRED PER SRM 51-01, PAGE 1, ITEM C AND TWA STANDARD PRACTICES.


REMARKS:
MCI - DURING OP-16, FOUND CORROSION IN LEFT TIEDOWN TRACK, STATION 1079 TO STATION 1109.  REPAIRED PER SRM 53-05, FIGURE 4G AND ARA 9859.


REMARKS:
BOS - DURING DESCENT SHUT DOWN NR 2 ENGINE, S/N 4422, DUE TO FIREWARNING.  FOUND LOWER ZONE 1 AFT DETECTOR LOOP, MFG P/N 898005, SHORTED.  REPLACED DETECTOR LOOP AND PERFORMED HIGH POWER ENGINE RUN AND OPERATION CHECKED NORMAL.


REMARKS:
SEA - FLT 740 - DURING CLIMB, NR 1 ENGINE, S/N 4603, SURGED.  POWER WAS REDUCED TO IDLE.  CHANGED NR 1 ENGINE.  ENGINE TOTAL TIME:  29,752 HOURS; 8,040 CYCLES.  CHECK C-4C - 10-25-95 - LAX.


REMARKS:
CLT - INSPECTION VISUALLY FOUND A LEVEL 2, .50 INCH BY 6 INCH, CORRODED AREA LOCATED AT STA 1010, STR 221.  REPAIR STRINGER SPLICED IN PER USAIR E.A. 40681 AND BOEING SRM 53-00-03.  (X)


REMARKS:
CLT - CLT INSPECTION FOUND BY EDDY CURRENT A 1.7 INCH FLOOR BEAM CRACK LOCATED AT STATION 520 EXTENDING 6 INCHES INBOARD OF RBL 24.75.  INSTALLED REPAIR DOUBLERS AS PER USAIR EA NR 40294.  (M)


REMARKS:
ATL- FLT 554 - DURING CRUISE, NR 1 ENGINE, SN 4026, SPUN DOWN.  SHUT DOWN ENGINE.  FOUND ACCESSORY GEARBOX HAD INTERNALMALFUNCTION.  REPLACED ENGINE AND ENGINE OPERATION CHECK NORMAL.  ENGINE TOTAL TIME:  49,589 HOURS, 33,419 CYCLES.  CHECK C-1 - 3-7-95 - MCI.  INVESTIGATION INTO ENGINE, SN 4026, GEARBOX FAILURE REVEALED A BUSHING, MFG PN 467572P3, ALLOWEDGEAR TO MIGRATE CAUSING RAPID TOOTH WEAR RESULTING IN GEARBOX FAILURE.  GEARBOX REPAIRED AND RETURNED TO SERVICE.


REMARKS:
FLT NR 1184 - BWI - ON FINAL APPROACH APU FIRE WARNING MOMENTARILY WENT OFF.  FIRED FIRE BOTTLE.  MAINTENANCE REPLACED THE APU.  (M)


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK NR 3, RBL 20, STATION 200-240.  REPLACED TRACK PER SRM 53-05, PAGE 10G AND SRM 51-01, ITEM C.


REMARKS:
ATL/ATL - FLT 509 - AIR RETURN, CABIN WOULD NOT PRESSURIZE IN MANUAL OR AUTO, ALL MASKS DEPLOYED.  FOUND LT DIVERTER VALVE ASSY BROKEN.  AFT INBOARD HEAT EXCHANGER FRAME SEAL REPLACED WITH HINGE REPLACEMENT.  RESTOWED MASKS.


REMARKS:
TPA - FLT 202 - NR 2 ENGINE REVERSER LIGHT ON OVERHEAD PANEL ILLUMINATED DURING FLIGHT, THROTTLE OPERATED NORMALLY AND REVERSER OPERATED NORMALLY ON GROUND.  MAINTENANCE REPLACED THRUST REVERSER CONTROL VALVE.  NO LEAKS NOTED.  OK FOR SERVICE.  (X)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACKED VERTICAL STIFFENER WEB AT BS 182 LBL 18 WL 184.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED 2 PLACES, ONE AT LBL 10 AND AT LBL 11, WL 219.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND APU COMPARTMENT UPPER BULKHEAD CRACKED AT LIGHTENING HOLE BETWEEN BS 1136 AND 1121 RIGHT SIDE AND BETWEEN BS 1121 AND 1104 LEFT SIDE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD SKIN CRACKED AT BS 178 WL 235 APPROX LBL 13.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 178 WL 195 LBL 24.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACK AT BS 178 WL 194 LBL 23.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 495, S23 AND 22R AND AT BS 1012, S7L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 747 S22R AT BS 727A S19R AND AT BS 520 S19L.  REPLACED PERBOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 CRACK ON LEFT SIDE AT WL 194 IN RADIUS OF SIDE CHORD.  REPAIRED PER SWAACO 96-0017.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND DOOR FRAME STRAP CRACKED AT BS 492 RBL 54 WL 180.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AND FAIL-SAFE CHORD CRACKED AT BS 179 LBL 55.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440 RBL 37 WL 160.  REPAIRED PER TRAMCO EWO 96-0041.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED 2 PLACES AT BS 440 LBL 55 AND 57 WL 177 AND 175.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGERS CORRODED BS 907 LBL 21 WL 168, BS 903 RBL 21 WL 168 AND BS 908 TO 906 RBL 19 WL 165.  REPLACED PER BOEING SRM.


REMARKS:
AT EWR - FLT NR 39 - NR 4 LEADING SLAT LIGHT CAME ON, AIRCRAFT RETURNED TO EWR.  FOUND NR 4 LEADING EDGE ACTUATOR REAR MOUNT BOLTS LOOSE, TIGHTENED LOOSE MOUNT BOLTS AND OPS CHECK FLAPS PER MM 27-80.  OPS OK.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 727 B S-1, STRINGER TIE CLIP.  REPAIRED PER EO 5393G227.  MODIFIED PART NR INSTALLED 69-35352-14. (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT STRINGER TIE CLIP BS 727A STRINGER 4 RIGHT.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 639 STRINGER 4 RIGHT.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 578 STRINGER 3 RIGHT.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 616 STRINGER 2 RIGHT.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 5 LEFT.  REPAIREDPER EO 5393G227.  MODIFIED PER NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 10L.  REPAIRED PER EO 5353G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 747 STRINGER 7L AND STRINGER 10L.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 727 A STRINGERS 3L, STRINGER 4L, STRINGER 5L.  REPAIRED PER EO 5393G227.  MODIFIED PER NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 706, STRINGER 10L.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 685, STRINGER 2L AND STRINGER 5L.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 639 STRINGERS 4L, 6L.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK IN 2 STRINGER TIE CLIPS BS 616 AT STRINGER 2L AND STRINGER 4L.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 578 AT STRINGER 3 LEFT STRINGER TIE CLIP.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 747 STRINGER 5 RIGHT, STRINGER TIE CLIP.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK BS 767 AT STRINGER 6 RIGHT STRINGER TIE CLIP.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK BS 767 AT STRINGER 10 RIGHT, STRINGER TIE CLIP.  REPAIREDPER EO 5393G227.  MODIFIED PART NR 69-3535214.  (M)


REMARKS:
INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK IN EACH OF 2 CLIPS, BS 727B AT STRINGER 2L AND STRINGER 7L, STRINGER TIE CLIPS.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 685 STRINGER 3 RIGHT STRINGER TIE CLIP.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK IN EACH OF 2 CLIPS BS 767 AT STRINGER 5L AND STRINGER 10L, STRINGER TIE CLIPS.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK TIE CLIP, STRINGER 3R, BS 727.  REPAIRED PER EO 5393G227.  MODIFIED PART NR 69-35352-14.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK SKIN BS 347 AT STRINGER 17L.  INSTALLED DOUBLERS.  REPAIRED PER EO 5391G-694.  (M)


REMARKS:
BOS - DURING INSPECTION OF PCI 1366 (FUSELAGE AREA BELOW MED) FOUND .125 INCH CRACK IN THE SKIN AT STATION 200 LONGERON22L.  FERRIED AIRCRAFT TO PIT FOR REPAIRS.  INSTALLED CLASS 3 DOUBLER PER SRM 53-04 FIG 12B.  (M)


REMARKS:
BOS - DURING INSPECTION OF PCI 949 (UPPER FUSELAGE CROWN INSPECTION) FOUND .5 INCH CRACK IN LONGERON 5R AT STATION 680. AIRCRAFT WAS FERRIED TO PIT FOR REPAIR.  REPAIRED LONGERON BY SPLICING PER SRM 53-02 FIG 2 IN PIT.  (M)


REMARKS:
BOS - DURING INSPECTION FOR PCI 959 A .125 INCH CRACK IN SKIN COMING FROM RIVET STATION 180 LONGERON 22L.  FERRIED AIRCRAFT TO PIT FOR REPAIRS.  ACCOMPLISHED EXTERNAL CLASS 3 REPAIR DOUBLER PER SRM 53-04 FIG 12B IN PIT.  (M)


REMARKS:
ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 27L, BS 786.5 TO BS 1016.  INSTALLED STRINGER SPLICES, REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
PIT - DURING C-6 INSPECTION, FOUND CORROSION AT LONGERON 22R STATION 140 TO STATION 160 BETWEEN SKIN AND LONGERON.  REMOVED DAMAGED AREA AND ACCOMPLISHED LONGERON SPLICE REPAIR AND SKIN DOUBLER REPAIR PER SRM 53-04-12B AND 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-4 INSPECTION, FOUND 1 INCH CRACK AT STATION 1437 LONGERON 3R IN FUSELAGE SKIN.  INSTALLED DOUBLER REPAIRPER SRM 53-04 FIG 27.  (M)


REMARKS:
PIT - DURING Q-4 INSPECTION, FOUND LEVEL 1 CORROSION ON LONGERON 30 FROM STATION 1285 TO STATION 1295.  CORROSION TASK NR C57-53300.  CUT OUT CORRODED SECTION OF LONGERON AND ACCOMPLISHED SPLICE REPAIR PER DACO DWG 5936667.  (M)


REMARKS:
PIT - DURING Q-4 INSPECTION, FOUND LEVEL 1 CORROSION AT LONGERON 29L STATION 1231-1250 AROUND AND AT RIVETS.  CORROSIONTASK NR C57-53300.  SPLICED IN NEW SECTION OF LONGERON PER USAIR EA 31905.  (M)


REMARKS:
PIT - DURING Q-4 INSPECTION, FOUND CORROSION 3 FEET BY 2 INCHES WIDE ON PREVIOUS REPAIR DOUBLER BETWEEN STATION 1154 - STATION 1211 AFT CARGO DOOR LOWER FRAME.  CORROSION LEVEL 1 TASK NR C57-53300.  MANUALLY INSTALLED REPAIR DOUBLERS PER USAIR EO NR 5390M251.  (M)


REMARKS:
PIT - DURING SCHEDULED CORROSION TRACK VISIT FOUND A CORRODED AREA 1 INCH BY 1.5 INCH AT BL 0 TOP T-EXTRUSION STATION 5305 FLOOR BEAM.  REMOVED T-EXTRUSION FROM FORWARD FACTORY SPLICE OF FLOOR BEAM.  INSTALLED NEW SECTION ANS SPLICED AFT END WITH 2 EACH DOUBLERS PER USAIR EA NR 32099.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCHES CORROSION STATION 967 BL 0 TO RBL 45 FLOOR BEAM.  CUTOFF TOP CAP, FABRICATED AND REPAIRED SPLICE AND INSTALLED PER SRM 53-10-9 FIG 2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION AT FLOOR BEAM SUPPORT ANGLE STATION 967 TO 947 LBL 12.  REPLACED WITH IDENTICAL PART NR 65-46812-170 AND ANGLE, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR BEAM STATION 1006, LBL 11 INCHES.  SPLICED IN NEW SECTION OF FLOOR BEAM, REPAIRED PER SRM 53-10-9.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION 8 INCH FLOOR SUPPORT INTERCOSTAL STATION 986.5 LNL 15 INCHES.  REPLACED WITH IDENTICAL PART NR 65-46812-191, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR SEAT TRACK BETWEEN STATION 1016 AND STATION 986.5.  INSTALLED NEW SEAT TRACK SECTION, REPAIRED PER SRM 51-10-3.  CORROSION TASK NR C53-107-02, CORROSION LEVEL2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM UPPER T-CAP BS 1016 LBL 3 INCHES.  INSTALLED T-CAP, REPAIR PLUS 2.6 LB WT CHANGE, REPAIRED PER SRM 53-10-9.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORRODED AREA ON SIDE OF STRINGER BS 351.2 - BS 380, STRINGER 28L.  REPLACED STRINGER SECTION REPAIRED PER SRM 51-10-1, PAGE 5, STEP 4.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND GOUGE APPROXIMATELY 22 INCHES FLOOR BEAM BS 312, LBL 12 INCHES TO RBL 10 INCHES.  CUT OUT DAMAGED AREA AND INSTALLED NEW SECTION WITH REPAIR ANGLES.  REPAIRED PER TR 53-10-13.  CORROSION TASKNR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE AT STATIO N967 TO 947 RBL 20.  REPAIRED PER SRM 51-10-1.  REPLACED WITH IDENTICAL PART NR 65-46812.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED NUT PLATE HOLES 3 FLOOR BEAM, STATION 986.5 RBL 36, LBL 5, RBL 5.  INSTALLED DOUBLERS, REPAIR PER SRM 53-10-9 FIG 7.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 24 INCH CORROSION Z-ANGLE AFT ENTRY DOOR.  REPLACED WITH IDENTICAL PART NR 65-52878-533, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 4 INCH CORRODED WEB AFT ENTRY DOOR Z-ANGLE THRESHOLD WEB.  FABRICATED NEW WEB, REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-52878.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A RIGHT.  INSTALLED PERMANENT ANGLE REPAIR, LESS THAN 1 POUND.  REPAIRED PER EA 40644.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND 3 INCH CRACK FRAME STATION 1491 BL 883L HIGH FREQUENCY EDDY CURRENT INSPECTION.  STOP DRILLED CRACK AND INSTALLED DOUBLERS PER USAIR EA NR 32077.  (M)


REMARKS:
GSO - DURING DE-ICING VISUALLY FROM DE-ICING BUCKET (DE-ICER DID NTO STRIKE A/C) FOUND 4 INCH CRACK IN SKIN, STATION 510 AT STRINGER 12L.  INSTALLED DOUBLER WITH BLIND FASTENERS, REPAIRED PER SRM 53-00-01, 51-40-00.  DEFERRED OM-7, NR 32811.  (M)


REMARKS:
TYS - FL 285 - EN ROUTE BNA-BWI, CREW RECEIVED RIGHT ENGINE 'B' LOOP FIRE WARNING.  CREW FOLLOWED PILOT HANDBOOK PROCEDURES.  SHORTLY THEREAFTER, THE CREW RECEIVED THE RIGHT AND LEFT 'A' LOOP AND LEFT 'B' LOOP WARNINGS.  FLIGHT DIVERTED TOTYS AND LANDED WITHOUT NO FURTHER INCIDENT.  MAINTENANCE REPLACED TWO GASKETS ON THE LEFT ENGINE ANTI-ICE DUCTS AND ONEON THE RIGHT ENGINE DUCT.  ALSO, FOUND POSSIBLE SHORT BETWEEN THE RIGHT 'A' AND 'B' LOOPS.  BOTH LOOPS WERE REPLACED ASA PRECAUTION.  (M)


REMARKS:
ORD - FL 904 - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW RECEIVED THREE RED LIGHTS.  GEAR WAS CYCLED, CREW RECEIVED GREEN INDICATIONS FOR THE MAINS BUT A RED FOR THE NOSE GEAR.  FLIGHT RETURNED TO ORD AND LANDED WITH NO FURTHER INCIDENT.MAINTENANCE ACCOMPLISHED A STRUT SERVICING PER THE MAINTENANCE MANUAL.  (M)


REMARKS:
ORD - FLT 904 - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW COULD NOT RETRACT THE NOSE GEAR.  THIS IS THE SECOND RETURN TO FIELD OF THIS FLIGHT ON THIS DAY.  MAINTENANCE SERVICED THE NOSE STRUT WHILE ON JACKS, AND THEN SWUNG THE GEAR.  AIRCRAFT RELEASED FOR SERVICE.  (M)


REMARKS:
ORD - FL 979 - FIRST OFFICERS WINDSHIELD CRACKED.  FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT.  (M)


REMARKS:
ORD FLI 979 - FIRST OFFICERS WINDSHIELD CRACKED.  FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE WINDOW HEAT CONTROLLER, P/N 9615059002, AND THE WINDOW.  (M)


REMARKS:
CLT - FLT 259 - EN ROUTE LGA-MCO - THE CENTER FUEL TANK BOOST PUMP CIRCUIT BREAKERS FWD 'A' AND 'B' POPPED AND COULD NOT BE RESET.  FLIGHT DIVERTED TO CLT DUE TO FUEL CONSIDERATIONS.  MAINTENANCE REPLACED THE CENTER FUEL BOOST PUMP.  (M)


REMARKS:
LGA - FLT 8002 - CREW REPORTED, THAT THE AIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FT.  FLIGHT DIVERTED TO LGA AND LANDED WITH NO FURTHER INCIDENT.  (M)


REMARKS:
DCA - FLT 2287 - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW COULD NOT RETRACT THE NOSE GEAR.  CREW CYCLED THE GEAR TWICE WITH THE SAME RESULT.  FLIGHT RETURNED TO DCA AND LANDED WITH NO FURTHER INCIDENT.  (M)


REMARKS:
STL - FL 1254 - AFTER TAKEOFF FROM STL AND GEAR RETRACTION, CREW RECEIVED MFDU MESSAGE THAT THE LEFT LANDING GEAR WAS NOT UP.  GEAR WAS CYCLED WITH THE SAME RESULT.  FLIGHT RETURNED TO STL AND LANDED WITH NO FURTHER INCIDENT.  AIRCRAFT WASFERRIED TO PIT.  MAINTENANCE CHECKED THE GEAR DOOR SWITCHES AND FOUND NO PROBLEMS.  AIRCRAFT WAS JACKED AND GEAR SWUNG TEN TIMES WITH NO FAULTS.  AIRCRAFT RELEASED FOR SERVICE.  (M)


REMARKS:
PIT - FL 1794, ON GEAR RETRACTION AFTER TAKEOFF, CREW RECEIVED LT MAIN GEAR AND RT MAIN GEAR MESSAGES.  AFTER CYCLING THE GEAR, CREW RECEIVED RIGHT MAIN LANDING GEAR DOOR MESSAGE.  CREW USED ALTERNATE PROCEDURE FOR THE LANDING GEAR AND RETURNED TO PIT.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE LANDING GEAR TEST VALVE IN THE TEST POSITION.  THE SWITCH WAS SAFTIED AND THE AIRCRAFT RETURNED TO SERVICE.  (M)


REMARKS:
CAE - FL 0854 - UPON TAKEOFF FROM CAE, CREW RECEIVED AURAL AND VISUAL FIRE WARNINGS ON THE NR 2 ENGINE.  CREW SECURED THE ENGINE AND THE WARNINGS STOPPED.  FLIGHT RETURNED TO CAE AND LANDED WITH NO FURTHER INCIDENT.  SET 20 MINUTES.  REMOVED AND REPLACED NR 2 OUTBOARD ENGINE DETECTION LOOP.  OPS CHECK NORMAL.  (M)


REMARKS:
MCO - FL 2226 - AFTER TAKEOFF FROM MCO, THE RIGHT MAIN LANDING GEAR RED LIGHT REMAINED ON.  FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT GEAR UPLOCK SENSOR AND MAIN GEAR RED GEAR CARD.  (M)


REMARKS:
FLT NR 1075 - PHL - UNABLE TO PRESSURIZE AIRCRAFT IN ANY MODE.  OUTFLOW VALVE WAS CONTROLLABLE IN FLIGHT.  BUT EVEN WITH OUTFLOW VALVE FULL CLOSED, AIRCRAFT WOULD NOT PRESSURIZE.  MAINTENANCE REPAIRED FORWARD CARGO DOOR SEAL PRESSURIZED AIRCRAFT TO 7.6 DIFF.  OPS NORMAL.  (M)


REMARKS:
TPA - FL 1798 - EN ROUTE CLT-SRQ - THE CAPTAINS OUTER WINDOW PANE SHATTERED.  THE FLIGHT DIVERTED TO TPA AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE WINDSHIELD.  (M)


REMARKS:
STL - DURING CLIMB, SHUT DOWN NR 1 ENGINE, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION.  FOUND METAL PARTICLES IN OIL FILTER.  REPLACED ENGINE.  GROUND OPERATION CHECKED NORMAL.  INVESTIGATION OF OIL FILTER BYPASS LIGHT ILLUMINATION AND METAL PARTICLES FOUND IN OIL FILTER OF NR 1 ENGINE REVEALED NR 3 BEARING FAILED.  REMOVED AND REPLACED NR 3 BEARING, AND ENGINE RETURNED TO SERVICE.  (M)


REMARKS:
ICT - DURING CRUISE, NR 1 ENGINE, S/N 3210, SPOOLED DOWN.  SHUT DOWN ENGINE.  FOUND INTERNAL MALFUNCTION IN N-2 ACCESSORY GEARBOX, MFG P/N 758300.  CHANGED ENGINE AND ENGINE OPERATION CHECKED NORMAL.  INVESTIGATION OF SPOOL DOWN OF NR 1 ENGINE, REVEALED A BUSHING, P/N 783310, ALLOWED THE INPUT GEAR TO SHIFT CAUSING RAPID TOOTH WEAR, RESULTING IN GEARBOX FAILURE.  GEARBOX REPAIRED AND RETURNED TO SERVICE.  (M)


REMARKS:
DURING CLIMBOUT, EXPERIENCED NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATING AND ASSOCIATED OIL PRESSURE DROP.  CREW PERFORMED ENGINE SHUT-DOWN CHECKLIST.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  REMOVED AND REPLACED NR 2ENGINE OIL PRESSURE PUMP, TRANSMITTER, AND MAIN OIL SCREEN PER BOEING M/M.


REMARKS:
CAPTAIN'S NR 1 WINDOW OUTER PANE SHATTERED ACROSS ENTIRE LENGTH.  DIVERTED TO TUL AND MADE AN UNEVENTFUL LANDING.  REMOVED AND REPLACED WINDOW ASSEMBLY PER BOEING M/M.


REMARKS:
STL - DURING TAKEOFF, NR 2 ENGINE SUFFERED A TURBINE FAILURE.  REMOVED AND REPLACED NR 2 ENGINE.  OPERATIONAL AND TRIM CHECKS NORMAL.


REMARKS:
SAN - DURING CLIMB SHUT DOWN LEFT ENGINE DUE TO COMPRESSOR STALL.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE AND ENGINE OPERATION CHECKED NORMAL.


REMARKS:
STL - DURING CLIMB SHUT DOWN LEFT ENGINE DUE TO COMPRESSOR STALL.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE AND ENGINE OPERATION CHECKED NORMAL.  INVESTIGATION OF ENGINE, S/N 3258, COMPRESSOR STALL REVEALED THE AIRFOIL OF ONE TURBINE BLADE FAILED DUE TO A FATIGUE CRACK CAUSING THE COMPRESSOR STALL, WHICH LEAD TO THE ENGINE SHUT DOWN.  THE ENGINE WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE, STATION 967 TO STATION947 RBL 45, REPAIRED PER SRM 51-10-1.  REPLACED WITH IDENTICAL PART NR 65C10592-4.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 2 INCH CORRODED FLOOR BEAM AREA AND AT ALL CLIPNUT HOLES BS 328 RBL 6 TO RBL 56.  INSTALLED NEW T-CAP AND DOUBLERS, REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL EDDY CURRENT INSPECTION, FOUND 1 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A LEFT.  INSTALLED PERMANENT ANGLE REPAIR, LESS THAN 1 LB, REPAIRED PER EA 40644.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 11 INCH BY 40 INCH CORROSION FLOOR SUPPORT ANGLE AT STATION 957 RBL 6 TO RBL 45.  REPAIRED PER SRM 51-10-1.  REPLACED WITH IDENTICAL PART NR 65-C10592-5 OR 6. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCH CORROSION FLOOR BEAM STATION 967 BL 0 TO LBL 45.  INSTALLED ONE DUOBLER AT LBL 42, REPAIRED PER TR 53-10-01A.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORRODED FLOOR SUPPORT ANGLE STATION 986.5 TO 967 LBL12.  REPLACED ANGLE, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR 53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK TOP FLANGE OF FRAME STATION 807 LEFT BETWEEN STRINGER 24 AND STRINGER 25.  CUT OUT CRACK, FABRICATED FILLER AND REPAIRED DOUBLER PER SRM 51-40-3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 727 BULKHEAD STIFFENER FITTING AT BL 0 WL 202.5.REMOVED CRACKED FITTING, INSTALLED NEW ONE, REPAIRED PER EO 5394G176.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND FOUR 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES BS 312 TO BS 328RBL 11 INTERCOSTAL.  REMOVED AND INSTALLED NEW INTERCOSTAL, REPAIRED PER SRM 51-10-1 PAGE 5.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 CORRODED AREAS AT CLIP NUT HOLES APPROXIMATELY 1 INCH BY 1 INCH BS 306 TO BS 345 LBL 48 'A' ANGLE LEFT ENTRANCE DOOR.  REMOVED AND INSTALLED NEW PART, REPAIRED PER SRM 51-10-1 PAGE 5.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES 'Z' ANGLE BS 294.5 TO BS 344 RBL 56.  REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-45875.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH ON INTERCOSTAL, RBL 10 INCHES BETWEEN BS 294.5 AND BS 312.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-45834.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA AT INTERCOSTAL BS 292 LBL 12 INCHES.  REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA 4 PLACES INTERCOSTAL, BS 344 TO BS 360 RBL 11.  REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 CORRODED AREAS APPROXIMATELY 2 INCHES BY 2 INCHES INTERCOSTAL, BS 297AND BS 303 LBL 12.  INSTALLED NEW INTERCOSTAL, REPAIRED PER SRM 51-10-1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM 'T' CAP CABIN BS 294.5 LBL 10INCHES, RBL 20.  CUT AND REPLACED T-CAP, LESS THAN 1 LB WEIGHT CHANGE, REPAIRED PER TR 53-10-04B.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND THREE CORRODED AREAS, APPROXIMATELY 1 INCH BY 1 INCH AT INTERCOSTAL, RBL 10 INCH BETWEEN BS 312 AND BS 328.  REPLACED WITH IDENTICAL PART NR 1137215, REPAIRED PER SRM 51-10-1.  CORROSION TASKNR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA INTERCOSTAL LBL 11 INCHES BETWEEN BS 312 AND BS 328.  REPLACED WITH IDENTICAL PART NR 65-45834-260, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHCK VISUAL INSPECTION, FOUND TWO CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH, INTERCOSTAL LBL 10 INCHES BETWEEN BS 328 AND BS 344.  REPLACED WITH IDENTICAL PART NR 65-45834-259, REPAIRED PER SRM 51-10-1.  CORROSION TASKNR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION INTERCOSTAL STATION 1006 - 986.5 '0' BL.  REPLACED WITH INDENTICAL PART NR 65-46812-170, REPAIRED PER SRM 51-10-1.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND 1 INCH CRACK, FRAME STATION 14911 BL 883 R (HFEC INSPECTION).  STOP DRILLED CRACK AND INSTALLED DOUBLERS PER USAIR EA NR 32077.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND FUSELAGE SKIN DELAMINATION RIGHT SIDE STUB WING LAY AREA AT FRAME STATION 23011.  INSTALLED DOUBLER REPAIR PER USAIR EA NR 31894.  (M)


REMARKS:
PIT - DURING Q-1 CHECK INSPECTION, FOUND FUSELAGE SKIN DELAMINATION LEFT SIDE STUB WING LAY AREA AT FRAME STATION 24011.  INSTALLED DOUBLER REPAIR PER USAIR EA NR 31894.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 2 INCH CRACKS AT NUT PLATE HOLES BS 500 G TO BS 520 BL 0 INTERCOSTAL.  REPAIRED PER S/B 737-53-1120 AND EA 40888.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND FIVE 1 INCH BY 1 INCH BY .050 INCH DENTS, RIGHT HORIZONTAL STABILIZER LOWER INTERSPAR SKIN STABILIZER STATION 184.7 TO 193.9 AT MID CHORD.  CUT OUT DAMAGE PLUS INSTALLED DOUBLER PER SRM 55-10-01 FIG 206.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 4 INCH CORRODED AREA AND SEVERAL 1 INCH BY 1 INCH AREAS AT BS794 RBL 14 INCHES CARGO FLOOR BEAM.  CUT OUT CORRODED SECTION (BS 779-877) FABRICATED AND INSTALLED NEW BEAM SECTION PER BOEING DRAWING 65-53844 AND SRM 53-00-53 FIG 202.  CORROSION TASK NR C53-108-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 5 INCHES OF SCRATCHES AND CORROSION ON FLOOR BEAM BS 312 LBL 15 TO 20.SPLICED 'T' SECTION PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH GOUGES LBL 45 SEAT TRACK SUPPORT CHANNEL FITTING STATION 521, WL 207.  REPAIRED PER EA 40888 STEP 3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY .5 INCH CORRODED FLOOR BEAM BS 947 LBL 5 AND RBL 6, LBL 16.  INSTALLED T-CAP PER EA 40816.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH GOUGES SEAT TRACK SUPPORT CHANNEL FITTING STATION 521, LBL25, WL 207.  REPAIRED PER EA 40888 STEP 3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH GOUGES SEAT TRACK SUPPORT CHANNEL FITTINGS STATION 521, BL0 WL 207.  REPAIRED PER EA 40888 STEP 3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH GOUGES SEAT TRACK SUPPORT CHANNEL FITTING STATION 521, RBL25, WL 207.  REPAIRED PER EA 40888 STEP 3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 BY 32 INCH CORROSION FLOOR BEAM BS 294 RBL 7 - RBL 60.  INSTALLED T-CAP AND REPAIRED ANGLES PER SRM 53-10-51.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN RADIUS BS 520 RBL 45 INCHES INBOARD SIDE OF SEAT TRACK FLOOR BEAM.  REPAIRED PER EA 40888 STEPS 1 AND 2.  (M)


REMARKS:
PIT - FL 862 - CREW RECEIVED HYDRAULIC STAB CHANNEL 2 FAULT.  AFTER PERFORMING APPLICABLE PROCEDURE, RECEIVED CHANNEL 1FAULT ALSO.  MAINTENANCE REPLACED THE HORIZONTAL STABILIZER ACTUATOR AND THE STABILIZER SERVOS.  (M)


REMARKS:
FLT NR 7015 - PIT - AFTER EXTENSION, RED NOSE GEAR LIGHT FAILED TO EXTINGUISH.  MAINTENANCE REPLACED THE NOSE GEAR LOCKSENSOR.  INDICATIONS NORMAL.  (M)


REMARKS:
FLT NR 592 - BWI - MAINTENANCE FOUND AISLE EMERGENCY LIGHT AT 7D INOP.  MAINTENANCE REPAIRED BROKEN WIRE AT 7D.  OPS CHECK SATISFACTORY.  (M)


REMARKS:
FLT 771 - PIT - DIVERTED TO PIT DUE TO RIGHT WING AND BODY OVERHEAT.  RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT.  WENT OUT SHORTLY AFTER RIGHT ENGINE BLEED VALVE WAS CLOSED ACCORDING TO FLIGHT MANUAL PROCEDURE.  MAINTENANCE CHECKED WIRING RESISTANCE PER MM, CHECKS OK.  PRESSURIZED, NO LEAKS FOUND.  REPLACED OVERHEAT DETECTOR PRECAUTIONARY, CHECKSOK.  (M)


REMARKS:
IND - FLT NR 275 - DURING CLIMB, SHUT DOWN NR 1 ENGINE.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE.  ENGINE OPERATION CHECKS NORMAL.  INVESTIGATION OF METAL PARTICLES IN TAILPIPE AFTER SHUTDOWN OF NR 1 ENGINE, REVEALED THAT A FIRST STAGE TURBINE BLADE FAILED DUE TO FATIGUE CRACKS AT INNER RADIUS.  REMOVED AND REPLACED FAILED TURBINE BLADE.  ALL SUBSEQUENT DAMAGE WAS ALSO REPAIRED.  ENGINE RETURNED TO SERVICE.  (M)


REMARKS:
JFK - DURING CHECK C-4D, FOUND A 1.25 INCH VERTICAL CRACK IN LT SIDE OF FUSELAGE FRAME GUSSET, STA 825.95.  REPAIRED PER SB 727-53-0197.  AIRCRAFT TT:  53,646 HRS; 35,058 CYCLES.


REMARKS:
STL - FLT 123 - DURING PREFLIGHT, FOUND FIRST CLASS EGRESS LIGHTS INOPERATIVE.  FOUND CAP STRIP, MFG PN 3350-0025-40, CAME LOOSE FROM LIGHT TRACK.  REINSTALLED CAP STRIP IN TRACK AND EGRESS LIGHTS.  OPERATION CHECKED NORMAL.  CHECK C-2 - 9-13-95 - MCI.


REMARKS:
MCI - FLT 1159 - DURING CLIMB, RT ENGINE 'B' FIREWARNING LOOP FLICKERED ON, SWITCHED TO 'A' LOOP.  AFTER LEVEL-OFF AT CRUISE, 'A' LOOP WARNING CAME ON AND WENT OFF.  FOUND LOWER APRON 'A' AND 'B' LOOPS CHAFED.  REPLACED 'A' AND 'B' APRON LOOPS, MFG PN 5938323-505 AND PN 5938323-506, AND FIREWARNING SYSTEM OPERATION CHECKED NORMAL.  CHECK C-2D - 11-15-95 - MCI.  REFERENCE: OPERATOR CONTROL NR 96ZZZX1194.


REMARKS:
MCI - FLT 1159 - DURING CLIMB, RT ENGINE 'B' FIREWARNING LOOP FLICKERED ON, SWITCHED TO 'A' LOOP.  AFTER LEVEL-OFF AT CRUISE, 'A' LOOP WARNING CAME ON AND WENT OFF.  FOUND LOWER APRON 'A' AND 'B' LOOPS CHAFED.  REPLACED 'A' AND 'B' APRON LOOPS, MFG PN 5938323-505 AND PN 5938323-506, AND FIREWARNING SYSTEM OPERATION CHECKED NORMAL.  CHECK C-2D - 11-15-95 - MCI.  REFERENCE: OPERATOR CONTROL NR 96ZZZX1193.


REMARKS:
LGA - FLT 460 - DURING APPROACH WHEN LANDING GEAR EXTENDED, NLG DID NOT EXTEND.  CYCLED LANDING GEAR.  FOUND NLG HYDRAULIC TRANSFER CYLINDER NOT OPERATING PROPERLY.  REPLACED NLG HYDRAULIC TRANSFER CYLINDER, MFG PN 69-14106-5.  NLG OPERATION THEN CHECKED NORMAL.  CHECK C-2 - 1-18-96.  MCI.


REMARKS:
DTW - FLT 220 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RT MLG AND DOOR LIGHTS REMAINED ILLUMINATED.  CYCLED LANDING GEAR.  FOUND RT MLG DOOR SWITCH AND TARGET DIRTY.  CLEANED DOOR SWITCH AND TARGET.  DOOR LIGHT INDICATION THEN CHECKED NORMAL.  CHECK C - 4-9-95 - MCI.


REMARKS:
LGA - FLT 300 - DURING APPROACH WHEN LANDING GEAR EXTENDED, NLG DID NOT EXTEND.  CYCLED LANDING GEAR.  LUBRICATED NLG TRUNNION, BEARINGS AND DRAG BRACE.  NLG OPERATION THEN CHECKED NORMAL.  CHECK C-2 - 1-18-96 - MCI.


REMARKS:
LGA - FLT 396 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NLG DID NOT EXTEND.  CYCLED LANDING GEAR.  FOUND NLG LOCK RELEASE ACTUATOR BYPASSING HYDRAULIC PRESSURE.  REPLACED NLG HYDRAULIC LOCK RELEASE ACTUATOR, MFG PN 65-40467-6.  NLGOPERATION THEN CHECKED NORMAL.  CHECK C-2 - 1-18-96 - MCI.


REMARKS:
JFK - FLT 148 - DURING CRUISE, SERVING CART, SN 1482, EMITTED AN ELECTRICAL ODOR.  DISCONNECTED SERVING CART.  FOUND BAD HEATING PADS.  REPLACED SERVING CART, MFG PN 958000-119.  NEW SERVING CART OPERATION CHECKED NORMAL.  CHECK C-11A - 11-29-95 - LAX.


REMARKS:
STL - FLT 385 - AFTER TAKEOFF WHEN LANDING GEAR RETRACTED, RT MLG AND DOOR LIGHTS REMAINED ILLUMINATED.  CYCLED LANDINGGEAR.  FOUND RT MLG HYDRAULIC ACTUATOR MALFUNCTION.  REPLACED RT MLG ACTUATOR, MFG PN 65-17830-13.  RT MLG OPERATION AND INDICATION THEN CHECKED NORMAL.  CHECK C - 4-9-95 - MCI.


REMARKS:
MXP - FLT 843 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RT MLG DID NOT INDICATE DOWN AND LOCKED.  CYCLED LANDING GEAR.  FOUND RT MLG GREEN INDICATOR LIGHT SOCKET, MFG PN 434-1033-2203, BROKEN.  REPLACED LIGHT SOCKET AND LANDING GEAR INDCATION CHECKED NORMAL.  CHECK C-5A - 1-24-96 - LAX.


REMARKS:
MCI - DURING OP-15, FOUND CORROSION ON AFT CARGO DOOR JAMB LOWER BEAM.  REPLACED BEAM PER SRM 51-01, PAGE 1, ITEM C.  AIRCRAFT TT:  39,822 HRS; 20,932 CYCLES.


REMARKS:
STL - FLT 414 - DURING CLIMB, LT ENGINE SURGED ACCOMPANIED WITH A DROP IN EPR.  SHUT DOWN LT ENGINE, SN 3201.  FOUND METAL PARTICLES IN TAILPIPE AND TURBINE BLADE DAMAGE.  CHANGED LT ENGINE AND ENGINE OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  31,874 HRS; 16,491 CYCLES.  CHECK C-1D - 8-21-95 - MCI.


REMARKS:
STL - DURING ROUTINE MAINTENANCE, FOUND EGRESS LIGHTS SEAT ROWS 21 TO 23 AND TAILCONE PATHWAY, INOPERATIVE.  FOUND EGRESS LIGHT CABLE CONNECTOR, MFG PN 5854-1, DIRTY.  CLEANED CABLE CONNECTOR AND LIGHT OPERATION CHECKED NORMAL.  CHECK C - 9-2-95 - STL.


REMARKS:
STL - DURING OP-15, FOUND .3750 INCH CRACK ON TOP LIP OF LONGERON 7L, STA 639.  REPLACED LONGERON SECTION PER SRM 53-02, PAGE 2A, FIGURE 2.  AIRCRAFT TT:  54,237 HRS; 59,836 CYCLES.


REMARKS:
JFK - FLT 903 - DURING CRUISE, NR 2 AFT GALLEY SERVING CART EMITTED SMOKE WHEN TURNED ON.  REMOVED AND REPLACED SERVINGCART.  OPERATIONAL CHECK NORMAL.  CHECK C-6A - 12-7-95 - LAX.


REMARKS:
STL - DURING LANDING, THE LEADING EDGE SLATS WERE FROZEN AND WOULD NOT DEPLOY.  LEADING EDGE SLAT ACTUATORS AND JACKSCREWS WERE THAWED, LUBRICATED AND SERVICED.  LEADING EDGE SLATS WERE CYCLED NUMEROUS TIMES, OPERATION NORMAL.


REMARKS:
STL - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT.  IT WAS DETERMINED THE NOSE GEAR WAS DOWN ALND LOCKED.  REMOVED AND REPLACED NOSE GEAR SEAL KIT, MFG PN A03772REVH.  GEAR SWING CHECKED NORMAL.  CHECK C-1D - 4-13-95 - MCI.


REMARKS:
STL - DURING CHECK 'C', FOUND SCRAPE ON FUSELAGE, STA 242, LONGERON 17L.  REPAIRED FUSELAGE DAMAGE PER SRM 53-04, FIGURE 38, SHEET 20 AND SRM 53-02, FIGURE 2.  AIRCRAFT TT:  24,501 HRS; 12,379 CYCLES.


REMARKS:
STL - FLT 86 - DURING CRUISE, LT FORWARD LAVATORY EMITTED AN ELECTRICAL ODOR.  CHECKED LIGHT BALLAST AND WIRING, FLUSH SYSTEM WIRING, SMOKE DETECTOR SYSTEM.  FOUND NO INDICATION OF OVERHEAT OR SOURCE OF ODOR.  ALL SYSTEMS CHECKED NORMAL.  CHECK C-7C - 1-14-96 - LAX.


REMARKS:
STL - FLT 585 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NLG UNSAFE RED LIGHT REMAINED ILLUMINATED WITH INTERMITTENT WARNING HORN.  CYCLED LANDING GEAR.  FOUND ICE IN NLG STRUT SCHRADER VALVE, MFG PN B05076-2.  REPLACED SCHRADER VALVE, SERVICED NOSE STRUT WITH OIL AND NITROGEN AND LANDING GEAR INDICATION CHECKED NORMAL.  CHECK C - 12-22-95 - STL.


REMARKS:
JFK - FLT 12 - DURING TAKEOFF ROLL, NR 3 ENGINE THROTTLE WOULD NOT ADVANCE.  REMOVED AND REPLACED THRUST REVERSER SEQUENCE ACTUATOR, MFG PN R1409M13-1.  OPERATIONAL CHECK NORMAL.  CHECK C-2 - 10-23-95 - JFK.


REMARKS:
PKX - FLT 205 - AFTER TAKEOFF, NLG DID NOT RETRACT.  FOUND NLG INFLATION LOW.  REPLACED SHRADER VALVE, MFG PN B05076-2,AND SERVICED NLG.  NLG INDICATION AND OPERATION THEN CHECKED NORMAL.  CHECK C-1D - 2-27-95 - MCI.


REMARKS:
MCI - FLT 475 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, SN 3921, DUE TO LOSS OF OIL QUANTITY.  FOUND OIL LEAK AT FUEL OILCOOLER LINE.  REPLACED OIL LINE SEAL, MFG PN 443330, AND RETAINER, MFG PN 354117; ENGINE LEAK CHECK AND OPERATION WAS NORMAL.  ENGINE TT:  57,657 HRS; 38,613 CYCLES.  CHECK C-3 - 4-8-95 - MCI.


REMARKS:
IND - FLT 160 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 3245, DUE TO VIBRATION AND COMPRESSOR STALLS.  DURING GROUND RUN, ENGINE HAD OFF IDLE STALLS.  REPLACED ENGINE AND OPERATONAL CHECKS WERE NORMAL.  ENGINE TT:  26,119 HOURS; 13,618 CYCLES.  CHECK C-1D - 7-28-95 - MCI.


REMARKS:
STL - FLT 296 - DURING APPROACH, NR 2 ENGINE, SN 3232, SPUN DOWN.  COMPLETED SHUTDOWN CHECKLIST.  FOUND INTERNAL MALFUNCTION IN FUEL CONTROL, MFG PN 769606-16.  REPLACED FUEL CONTROL AND ENGINE OPERATION CHECKED NORMAL.  ENGINE TT:  31,831HOURS; 16,687 CYCLES  CHECK C-1 - 10-12-95 - MCI.


REMARKS:
STL - DURING CHECK 'C', FOUND .50 INCH CRACK IN LOWER FLANGE OF LONGERON 7L, STA 699.  REPAIRED PER SRM 53-02, FIGURE 2A.  AIRCRAFT TT:  63,390 HOURS; 75,098 CYCLES.


REMARKS:
STL - DURING CHECK 'C', FOUND .50 INCH CRACK AT BOTH ATTACH POINTS TO BELT RING, LONGERON 6R, STA 718.  REPAIRED PER SRM 53-02, FIGURE 2A.  AIRCRAFT TT:  68,390 HRS; 75,098 CYCLES.


REMARKS:
STL - DURING CHECK 'C', FOUND .50 INCH CRACK IN LONGERON 4L, LOWER LEG, STA 737.  REPAIRED PER SRM 53-02, FIGURE 2A.  AIRCRAFT TT:  63,390 HOURS; 75,098 CYCLES.


REMARKS:
STL - FLT 503 - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED.  REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNAL FAILURE, MFG PN 2589445-933.  OPERATIONAL CHECK NORMAL.  CHECK C-12 - 1-11-95 - STL.


REMARKS:
STL - DURING LAYOVER MAINTENANCE, LT OVERWING EMERGENCY EXIT LIGHT FOUND INOPERATIVE.  REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, MFG PN 61-0478-3.  OPERATIONAL CHECK NORMAL.  CHECK C - 7-20-95 - MCI.


REMARKS:
JFK - FLT 884 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 4187, DUE TO COMPRESSOR STALL ACCOMPANIED BY INCREASING EGT ANDDECREASING RPM.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE AND ENGINE OPERATION CHECKED NORMAL.  ENGINE TT:  80,615 HRS; 14,493 CYCLES.  CHECK C-2 - 1-15-96 - JFK.


REMARKS:
MCI - FLT 117 - DURING APPROACH, LANDING GEAR WARNING HORN SOUNDED; CYCLED GEAR.  REMOVED AND REPLACED LANDING GEAR POSITION WARNING MODULE, MFG PN 65-60211-34.  OPERATION NORMAL.  CHECK C-3 - 3-24-95 - MCI.


REMARKS:
CMH - FLT 211 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NLG DID NOT RETRACT.  CYCLED LANDING GEAR.  FOUND NLG SCHRADER VALVE LEAKING.  REPLACED SCHRADER VALVE, MFG PN B05076-2, AND SERVICED LANDING GEAR.  NLG OPERATION CHECKED NORMAL.  CHECK C-2D - 4-10-95 - MCI.


REMARKS:
EWR/ATL - FLT 25 - AT EWR, AFT CARGO DOOR OPEN LIGHT CAME ON DURING TAKEOFF ROLL.  ABORTED TAKEOFF.  ADJUSTED CARGO DOOR SWITCH PER MM 52-70-01.  OPS CHECK OK.  (X)


REMARKS:
JFK - FLT 901 - DURING CRUISE, BOTH EICAS ANTI-SKID LIGHTS ILLUMINATED.  CLEANED AND RESEATED NR 2 TRANSDUCER CONNECTOR.  PERFORMED BITE CHECK, SYSTEM TESTED NORMAL, NO FAULTS NOTED.  CHECK C-C4A - 11-15-95 - LAX.  (IRELAND)


REMARKS:
TPA - FLT 427 - DURING CLIMB, NLG DOOR FAILED TO RETRACT.  SERVICED NLG STRUT.  OPERATIONAL CHECK NORMAL.  CHECK C-01 -6-27-95 - MCI.  (IRELAND)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787 S24R AND S20R, BS 727A S25L, BS 747 S20L AND S22L AND AT BS 947, S25R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CHORD CRACKED AT BS 726, RBL 9 WL 202.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 999 LBL 13 WL 208, BS 1002 LBL 12 WL 208 AND BS 1005 LBL 10 WL 208.  REPLACED CORRODED SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 987 LBL 3 TO 19 WL 208 AND BS 947 RBL 10 WL 208 AND LBL 4, 12, 22, WL 208.  REPLACED CORRODED SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344 LBL 45 WL 170.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S20R.  REPLACED WITH NEW PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER AND STRINGER SPLICE CORRODED AT BS 909 LBL171 WL 171.  REPLACED WITH NEW PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN S14 AND 15L.  REPLACED WITH NEW PER BOEING SRM.


REMARKS:
DURING SCHEDULED A1-CHECK, FOUND RT EMERGENCY EXIT LIGHTS INOP.  REPLACED LIGHT HOUSING PER BOEING MM.


REMARKS:
DURING SCHEDULED SV-CHECK, FOUND FUSE SKIN CRACKED AT BS 947.5, ABOVE S25L AND FWD 4 INCHES.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CRACKS AT BS 500B LT IN RADIUS OF UPPER FLANGE.  REPAIRED PER SWA ACO 595-53.


REMARKS:
BETWEEN 75 AND 100 MILES FROM OMA, NUMBER 2 ENGINE OIL PRESSURE DROPPED TO 20 PSI, ALL OTHER INDICATIONS READ NORMAL.  PERFORMED ENGINE SHUTDOWN CHECKLIST, AIRCRAFT MADE AN UNEVENTFUL LANDING AT OMA.  REMOVED AND REPLACED OIL PRESSURE TRANSMITTER PER BOEING MM.


REMARKS:
AFTER TAKEOFF, CREW WAS UNABLE TO RAISE GEAR WITHOUT USING OVERRIDE TRIGGER.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  CYCLED GEAR SEVERAL TIMES, NO DEFECTS NOTED.  RESET LANDING GEAR POSITION LIGHTS C/B.


REMARKS:
ON TAKEOFF ROLL AT 100 KTS, ON CROSS CHECK OF AIRSPEED INDICATORS, THE CAPTAINS WAS AT ZERO KTS AND THE FIRST OFFICERS WAS 100 KTS, TAKEOFF WAS ABORTED.  RESEATED CANNON PLUG AND PERFORMED INSTRUMENT PITOT STATIC LEAKAGE CHECK, OPS CHECK GOOD IAW MM 31-10.  (M)


REMARKS:
ON FLT NR 166, SAV-SAV - AIR RETURN, AIRCRAFT EXPERIENCED A RIGHT A/C TEMP SUPPLY HIGH LIGHT ON.  MAINTENANCE REPLACED THE RIGHT A/C SUPPLY TEMP HIGH SENSOR.  OPS CHECKS GOOD IAW 21-55.  (M)


REMARKS:
ON FLT NR 550, ATL-ATL, AIR RETURN, AFTER TAKEOFF THE TAKEOFF WARNING HORN SOUNDED DURING FLAP RETRACTION.  THE FLAP SLAT WERE RE-EXTENDED TO 5 DEGREES, DID NOT GET AIR MODE.  AUTO SPOILER ' DO NOT USE' LIGHT WAS ON FOR LANDING.  MAINTENANCE FOUND THE GROUND SHIFT MODE OUT OF RIG.  RIGGED NOSE GEAR GROUND SENSE MECHANISM, OPS CHECK GOOD.  SECURED TURNBARRELS MM 32-23-1.  (M)


REMARKS:
ON FLT NR 535, ATL-ATL, AIR RETURN, DURING THE CLIMB THE CAPTAIN NOTICED NR 2 ENGINE OIL PRESSURE AT 100 PSI.  THE AIRCRAFT LANDED UNDER THE MAXIMUM LANDING WEIGHT.  MAINTENANCE FOUND A BAD CANNON PLUG.  REMOVED AND REPLACED THE CANNON PLUG, OPS CHECKED GOOD IAW MM 79-31.  (M)


REMARKS:
ON FLT NR 517 - ATL-ATL - AIR RETURN, ON GEAR RETRACTION ALL LIGHTS WENT OUT, ON UPLATCH CHECK GREEN LIGHT ON, DOOR LIGHTS CLOSED.  GEAR CYCLED AND NOSE GEAR INDICATED UNSAFE.  RECYCLED AND ALL LIGHTS GREEN.  FOUND LEFT GEAR UPLOCK TARGET MISALIGNED WITH RETENTION SPRING.  REALIGNED RETENTION WITH TARGET AND ADJUSTED NOSE GEAR LOCK SENSOR TARGET.  REPLACED PROXIMITY BOX AND LANDING GEAR LEVER RELAYS AS PRECAUTIONARY.  OPS CHECK NORMAL.  (M)


REMARKS:
ON FLT NR 363 - BOS-RDU, CAPTAIN COULD NOT PRESSURIZE THE CABIN IN MANUAL OR AUTO.  MAINTENANCE FOUND THE OUTFLOW VALVECONTROL WHEEL STUCK IN FULL OPEN POSITION.  MAINTENANCE FREED WHEEL AND OPS CHECKED OK.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK IN CIRCUMFERENTIAL FRAME STATION 360 4 INCHES BELOW STRINGER 19 R.  INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK ON CIRCUMFERENTIAL FRAME WEB STATION 328 4 INCHES BELOW STRINGER 20R.  INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STATION 639 STUB BEAM WEB LBL 48 WL 206.5.  INSTALLED WEB,REPAIRED PER BOEING DRAWING 65C25211.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK ON SKIN BS 380 BETWEEN STRINGER 28 L AND BL 0.  INSTALLED DOUBLER, REPAIRED PER TR 53-30-04 AND EA 25454.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN FUSELAGE SKIN 1156 BULKHEAD STRINGER 2 L AND STRINGER 3L.  INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION INTERCOSTAL, STATION 270 TO STATION 294 LBL 10 INCHES.  INSTALLED NEW PREFAB INTERCOSTAL, REPAIRED PER BOEING DRAWING 65-45634.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA AT STRINGER TIE CLIP BS 540 STRINGER 26 L.  REPLACED STRINGER TIE CLIP, REPAIRED PER SRM 53-10-1.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK NR 4 STOP CUTOUT (AFT FRAME) AT FORWARD CABIN SERVICE DOOR.  STOP DRILLED CRACK, REPAIRED AND INSTALLED.  REPAIRED PER SRM 52-00-2 PAGE 4 FIG 1 AND SRM 51-40-3 PAGE 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED NUT PLATE HOLES AT FLOOR BEAM STATION 460-500 ABOVE STRINGER 27 R.  REPLACED ANGLE, REPAIRED PER SRM 53-10-5 FIG 6.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LEFT WING AT WS 537.8 LOWER FLANGE OF AILERON HINGE FITTING.  FABRICATED AND INSTALLED FLANGE REPAIR PER EA 40893.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH LONG CRACK FUSELAGE BULKHEAD STATION 178, WL 200, RBL 6 INCHES.INSTALLED REPAIRED DOUBLER, REPAIRED PER TR 53-10-11.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 20 INCH CORRODED AREA RIGHT Z-ANGLE AT AFT SERVICE DOOR STATION 940 TO STATION 1010.  REMOVED CORROSION ON ALODINE AND PRIMED.  COMPLETED REPAIR PER SRM 51-10-6.  LEVEL 1 CORROSION. (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK NR 3 STOP CUT OUT (AFT FRAME) AT FORWARD CABIN SERVICE DOOR.  STOP DRILLED CRACK, REPAIRED PER SRM 52-00-2 PAGE 4, FIG 1 AND SRM 51-40-3 PAGE 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 727 B 2 INCH AND STRINGER 17.INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6.  (M)


REMARKS:
PIT - DURING SIP VISIT INSPECTION, ACCOMPLISHED SIP 53-10-06 AND FOUND 4 INCH AND 3.5 INCH CRACK IN FRONT PRESSURE BULKHEAD FISHPLATE BETWEEN STRINGER 72 AND 73.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-02-18 PG 28.  (M)


REMARKS:
CLT - INSPECTION VISUAL FOUND DAMAGED INNER, OUTER CHORD, WEGB AND FORMED ANGLES APPROX 8 INCHES BY 2 INCHES LOCATED ATTHE FUSELAGE FRAME LOCATED AT BS 188 FROM 7 INCHES RIGHT OF BL 0 TO 23 INCHES RIGHT OF BL 0.  INSTALLED REPAIR CHORD AND WEB AS PER BOEING SRM 51-70-11, 51-70-12 AND 51-70-13.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 328 AT NR 3 STOP FOR FORWARD CABIN SERVICE DOOR FRAME.  STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3 PAGE 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION Z-ANGLE STATION 270 AT BL 0.  REMOVED CORROSION AND INSTALLED DOUBLER, REPAIRED PER TR 53-20-04.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH HOLE STATION 400-420 STRINGER 27 R SKIN AND STRINGER.  INSTALLED DOUBLER ON SKIN, SPLICED IN STRINGER SECTION, REPAIRED PER SRM 53-00-03 AND SRM 53-00-01.  (M)


REMARKS:
LGA- FLT 301 - UPON GEAR EXTENSION, THE CABIN STANDBY LIGHTS AND EXIT IDENTIFIERS DID NOT ILLUMINATE.  MAINTENANCE REPLACED THE K2618A RELAY.  (M)


REMARKS:
FLT NR 1017 - PIT - EMERGENCY SLIDE AT MAIN ENTRY DOOR IS COMING OUT OF ITS PACK.  REPLACED MED EMERGENCY SLIDE PER MM. OPS CHECK GOOD.  (M)


REMARKS:
FLT NR 275 - RDU - OUTER PANE OF CAPTIANS WINDSHIELD SHATTERED IN FLIGHT AT 29,000 FEET PRECAUTIONARY LANDING MADE AT RDU.  REPLACED L1 WINDOW.  (M)


REMARKS:
FLT 578 - CLT - RIGHT MAIN GEAR FAILED TO INDICATE DOWN AND GREEN.  RECYCLED GEAR, CHANGED BULBS WITH NO CHANGE.  LANDED NORMALLY, TAXIED WITH GEAR PINNED.  PERFORMED BITE USING THE PSEU WITH NO DEFECTIVE SWITCHES OR TARGETS.  INSPECTED INDICATION PACK ON FORWARD PANEL AND FOUND ONE BROKEN BULB AND ONE BURNED OUT BULB.  REMOVED AND REPLACED ALL BULBS AND GEAR WARNING SYSTEM OP'D NORMAL.  AIRCRAFT OK FOR CONTINUED SERVICE.  (M)


REMARKS:
PHL-MCI - FLT 439 - THE NR 1 BOOST PUMP WARNING LIGHT ILLUMINATED.  SHORTLY THEREAFTER, THE NR 2 BOOST PUMP WARNING LIGHT ILLUMINATED.  FLIGHT DIVERTED TO IND AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE OPERATED BOTH PUMPS ON THE GROUND AND FOUND THEM BOTH WORKING PROPERLY.  PERFORMED BITE AND COULD NOT DUPLICATE PROBLEM.  AIRCRAFT RELEASED FOR SERVICE.  (M)


REMARKS:
FLT NR 1201 - BWI - ON CLIMB-OUT FROM EWR AT 34.5 CABIN ALT.  WARNING HORN CABIN AT 13,000 UNABLE TO CONTROL PRESSURE DESCENT TO 10,000.  MAINTENANCE REPLACED AUTO CONTROLLER, OPS CHECK NORMAL.  PERFORMED OPERATIONAL TEST OF PRESS CONTROL SYSTEM IAW MM CH 21-31-00 PAGE 201.  (M)


REMARKS:
FLT NR 800 - MCI - DURING CLIMB AT APPROXIMATELY 10,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON.  THE CAPTAIN REDUCED POWER AND THE LIGHT WENT OUT.  PULLED NR 2 ENGINE BACK TO IDLE AND RETURNED TO MCI.  (M)


REMARKS:
FLT NR 1129 - CRW - AFTER DEPARTING PIT AND CLIMBING TO FLT LEVEL 350, THE FIRST OFFICERS WINDSHIELD BEGAN TO BUBBLE/DELAMINATE.  CAPTAIN DECIDED TO DIVERT TO CRW BECAUSE HE COULD NOT TELL IF ONLY THE OUTER PANE WAS INVOLVED.  MAINTENANCE REPLACED FIRST OFFICERS WINDSHIELD PER MAINTENANCE MANUAL.  OPS CHECKED GOOD.  (M)


REMARKS:
FLT NR 1759 - DCA - EMERGENCY EXIT LIGHT AT SEAT 12C IS BROKEN OFF.  MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECKS SATISFACTORY.  (M)                                                                                                                     P


REMARKS:
FLT NR 885 - GSO - ON INITIAL CLB FLIGHT ATTENDANT NOTICED A VIBRATION THROUGH THE CABIN.  AT CRUISE VIBRATION CONTINUES WIHT CAPTAIN ISOLATING PROBLEM TO NR 1 ENGINE.  ALL ENGINE READINGS CONTINUED TO BE NORMAL.  AIRCRAFT DIVERTED TO GSO. (M)


REMARKS:
FLT NR 2201 - CLT - AUTOPRESSURIZATION FAILED AT FL 370.  EMERGENCY DESCENT MADE, WAS ABLE TO REGAIN CONTROL OF CABIN IN MANUAL.  NEVER GOT THE 10,000 FEET ALT HORN AND FIRST INDICATION PAX OXYGEN LIGHT AND OVERHEAD ON RECALL.  MAINTENANCEREMOVED AND REPLACED RIGHT PRESSURE RELIEF VALVE.  CHECKS SATISFACTORY.  REPLACED LEFT PRESSURE RELIEF VALVE PRECAUTIONARY.  CHECKS SATISFACTORY.  (M)


REMARKS:
FLT NR 797 - MCO - FIVE MINUTES AFTER TAKEOFF, 'OIL FILTER BYPASS' LIGHT FOR NR 1 ENGINE CAME ON.  RETARDED THROTTLES, NO HELP.  SHUT DOWN ENGINE AND RETURNED TO MCO.  MAINTENANCE REPLACED THE FILTER BYPASS SWITCH.  (M)


REMARKS:
SEA - FLT 740 - DURING CLIMB, NR 1 ENGINE, SN 4609, SURGED.  POWER WAS REDUCED TO IDLE.  CHANGED NR 1 ENGINE.  ENGINE TOTAL TIME:  29,752 HOURS; 8,040 CYCLES.  CHECK C-4C - 10-25-95.  LAX.


REMARKS:
FLT NR 1215 - PIT - RED NOSE GEAR LIGHT ON TAKEOFF WHEN HANDLE IN UP AND OFF POSITION.  RECYCLED GEAR THREE GREEN LIGHTS, RED REMAINED ON.  MAINTENANCE REPLACED NOSE GEAR LOCK SENSOR.  SWUNG GEAR, OPS CHECK OK.  (M)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294, RBL 36 AND RBL 46, WL 208.  ALSO, AT BS 328, RBL 15 AND 25, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 PRESSURE WEB CRACKED AT RBL 9.7, WL 219.  ALSO, AT LBL 11.3, WL 219.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 726, STRINGER 18A, RBL 61, WL 188.25.  ALSO, AT BS 530, RBL 43, WL 161.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND INBOARD CREASE BEAM  CRACKED AT BS 616, RBL 65, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, BL 0 TO LBL 25, WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 663, RBL 24 AND LBL 24.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, RBL 55, BETWEEN S20R AND 21R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT AFT BAY AT BS 907, S25L, LBL 21, WL 168.  REPLACED SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED B2-CHECK, FOUND FWD SERVICE DOOR CRACKED AT LOWER HINGE UPPER RADIUS AT PREVIOUS REPAIR.  REPAIRED PERBOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED SEVERAL PLACES, AT LBL 5.7, WL 192 TO 198.5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED 6 INCHES TO 7 INCHES AT WL 219 AND BL 15.5, O/B RTOF RADAR UNIT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERM CHECK, FOUND NOSE WHEEL WELL CEILING CRACKED NEAR ATTACH BRACKET FOR NLG MANUAL EXTENSION EXT SPRING.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS AT RT WING STRINGER 13R, WRL 91 TO WBL 94 LOWER RADIUS.  REPAIRED PERBOEING SRM AND DRAWING 65C34533.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, WL 209, BL 64 LEFT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B/C2 CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED .25 INCHES AT UPPER CORNER.  REPAIRED PER SWA RA 1-352-242.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND 3 INCHES FUSELAGE SKIN CRACK AT BS 310 AT S25L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHTS AT OVERWING EXIT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND 2 FUSELAGE SKIN CRACK 10 INCHES FWD OF WATER SERVICE DOOR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM NUTPLATE HOLE CORRODED AT BS 986.5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM NUTPLATE HOLE CORRODED AT BS 986.5 RBL 30.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND 3.3 INCH CRACK IN RADIUS OF RT CREASE BEAM I/B CHORD ANGLE AT BS 294, RBL 54.  REPAIRED PER BOEING SRM AND TYPICAL REPAIR T1-A53-023.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM AFT FLANGE CORRODED AT BS 312 LBL 15.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800 WL 205.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C-CHECK, FOUND FUSELAGE SKIN CRACK AT BS 972 AT S25L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND FWD SERVICE DOOR CRACKED AT LOWER HINGE UPPER RADIUS ON DOOR SKIN.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED ON DOOR AT RADIUS.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND 2 INCH CRACK AT BS 178  BULKHEAD PRESSURE WEB, RBL 9.7 WL 219.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND 1.8 INCH CRACK AT BS 178  BULKHEAD PRESSURE WEB, LBL 11.3 WL 219.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 530, RBL 43 WL 161.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 663 RBL 24 AND LBL 24 WL 201.  REPAIRED PER BOEING SRM AND BOEING DRAWING 691A0032.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK INDICATION AROUND FASTENER HEAD AT BS 178 WL 234 RBL 10.  REPAIRED PER BOEING SRM.


REMARKS:
PIT - FL 1193 - ON CLIMB-OUT FROM PHL, CREW RECEIVED TCAS FAULT AND GROUND/FLIGHT CONTROL FAULT.  EN ROUTE TO MCI, CREWRECEIVED THE TAKEOFF CONFIGURATION STAB TRIM FAULT.  FLIGHT DIVERTED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE PSEU COMPUTER.  (M)


REMARKS:
FLT NR 8945 - CLT - RETURNED TO FIELD, LOUD AIR DRAFT DOOR L-1, UNABLE TO MAINTAIN PRESSURIZATION.  MAINTENANCE FOUND LOWER HINGE ARM FLAP BENT.  REPOSITIONED FLAP.  PRESSURIZED AIRCRAFT ON GROUND, NO LEAKS OR LOUD NOISE NOTED.  OK FOR SERVICE.  (M)


REMARKS:
FLT NR 1204 - PHL - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF.  NO COCKPIT INDICATIONS.  OUTFLOW VALVE WAS CLOSED.  MAINTENANCE REPLACED RIGHT PACK TURBINE INLET SWITCH FOR PRECAUTIONARY MEASURES.  (M)


REMARKS:
SJU - FLT 1041 - RIGHT PACK TRIPPED, COULD NOT RESET.  LEFT PACK RESET THEN TRIPPED AGAIN.  LEFT PACK CONTINUALLY TRIPS.  MAINTENANCE REPLACED RIGHT PRIMARY HEAT EXCHANGER.  OPS CHECKS SATISFACTORY.  (X)


REMARKS:
MIA - FLT 17 - DURING DESCENT, SHUT DOWN NR 2 ENGINE, SN 3979, DUE TO FIREWARNING.  FOUND MOISTURE IN LOOP CONNECTOR, MFG PN 894232.  CLEANED CONNECTOR AND INSTALLED NEW GASKET WASHERS.   GROUND OPERATION OF WARNING SYSTEM CHECKED NORMAL.ENGINE TT:  58,407 HRS; 38,756 CYCLES,  CHECK C-4 - 10-5-95 - MCI.


REMARKS:
STL - FIRST CLASS OVERHEAD EMERGENCY LIGHT INOPERATIVE.  REMOVED AND REPLACED TWO EACH BULBS, MFG PN 1315, AND ONE EACHBATTERY PACK, MFG PN 5822-2.  OPERATIONAL CHECK NORMAL.  CHECK C - 9-17-95 - STL.


REMARKS:
BOS/RDU - FLT 361 -  NO GREEN LIGHT ON LEFT MAIN GEAR WHEN LOWERED IN RDU.  APPROPRIATE PROCEDURES WERE FOLLOWED AND EVENTUALLY LIGHT CAME ON STEADY.  GEAR PINNED FOR TAXI.  INSPECTED AND PINNED GEAR DOWN AND LOCKED FOR MAINTENANCE FERRY TO 31J.  REPAIRED LEFT MLG DOWN AND LOCKED SWITCH AND CANNON PLUG, OPS CHECK GOOD IAW DC-9 MM 20-50-1 AND MM 32-30-1.


REMARKS:
BOS/PBI - FLT 395 - UPON GEAR EXTENSION, NEITHER RED UNSAFE NOR GREEN SAFE LIGHT ILLUMINATED FOR NOSE GEAR.  FOUND A NOSE GEAR POSITION SWITCH CONNECTOR LOOSE.  CANNON PLUG WOULD NOT LOCK.  INSTALLED NEW PLUG PER MM 32-60-1, PAGES 20-23A.OPS CHECK GOOD.


REMARKS:
ATL/ATL - FLT 166 - AIR RETURN, BOTH VHF NAVS INOP ON ALL FREQUENCIES.  FOUND BOTH ANTENNA CONNECTIONS LOOSE.  RECONNECTED, CHECKED BOTH NAV SYSTEMS WITH TIC 30, OPS CHECK GOOD.


REMARKS:
AFTER TAKEOFF WITH LANDING GEAR LEVER IN THE UP POSITION, RIGHT MAIN GEAR RED LIGHT ILLUMINATED.  WHEN GEAR LEVER MOVEDTO OFF, RIGHT MAIN GEAR EXTENDED AND WENT TO GREEN POSITION.  GEAR LEVER WAS THEN POSITIONED TO UP AND GEAR RETRACTED.INSPECTED AND REPLACED RIGHT MAIN GEAR UPLOCK ACTUATOR AND CYCLED GEAR SEVERAL TIMES PER BOEING M/M.


REMARKS:
UNABLE TO LOWER OR RETRACT T/E FLAPS PAST 5 DEGREES USING HYDRAULICS.  ALTERNATE/ELECTRICAL EXTENSION USED TO MOVE THEMTO 15 DEGREES.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT LAX.  INSPECTED AND REPLACED FLAP POSITION INDICATOR PER BOEING M/M.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR SKIN CRACKED AT TOP AFT CORNER AT UPPER RIVET.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FWD LEFT FUSELAGE SKIN CRACKED 2 INCHES AT BS 380 S24L.  REPAIRED PER BOEING SRM.


REMARKS:
AFTER LANDING, EXPERIENCED POOR BRAKING ACTION.  ALSO, BRAKES WOULD NOT SET AT GATE.  INSPECTED AND FOUND AN ADEL CLAMPUNDER F/O BRAKE PEDAL PANEL.  REMOVED AND BRAKES OPERATED NORMALLY.


REMARKS:
RDU/RDU - FLT 790 - AIR RETURN, AFTER TAKEOFF, RIGHT GENERATOR FAIL/CROSS TIE LOCK-OUT WARNING.  C/W QRH PROCEDURES, DISCONNECTED RIGHT GENERATOR/CSD.  ASSIGNED MEL 24-01-01 CONTROL NR DM7319.


REMARKS:
MIA - FLT 538 - LEFT EMERGENCY DOOR (L3) WARNING LIGHT CAME ON DURING CLIMB OUT FROM MIA.  AIRCRAFT RETURNED TO FIELD.CORRECTIVE ACTION:  PENDING.  (X)


REMARKS:
CLT - FLT 1543 - ON TAKEOFF FROM RDU RWY 23R, CAPT HAD GEAR FAULT MESSAGE, RDU TOWER TOLD HIM IT LOOKED LIKE SOMETHING FELL OFF THE AIRCRAFT.  WHILE THE FLT HELD IN THE AIR OVER RDU, THEY FOUND THE NR 2 MAIN WHEEL ASSY.  FLT PROCEEDED TO CLT.  CORRECTIVE ACTION:  PENDING.  (X)


REMARKS:
PIT - FLT 946 - TAIL ANTI-ICE FAILED REPEATEDLY ON CLIMB-OUT.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE TAIL ANTI-ICE VALVE.  (X)


REMARKS:
PIT - FLT 421 - RIGHT ENGINE COWLING LATCH CAME OPEN IN-FLIGHT, ACFT RETURNED.  MAINTENANCE SECURED RIGHT ENGINE UPPER COWLING LATCH, CHECKS NORMAL.  CHECKED ALL OTHER COWLING LATCHES, CHECK GOOD.  (X)


REMARKS:
CLT - FLT 0035 - FORWARD SECTION OF FLOOR LEVEL EMERGENCY LIGHTING INOP.  MAINTENANCE ADDED A GROUND WIRE TO TERMINAL BLOCK PIN 1 FOR SECTION 1 LIGHTS.  WDM 33-51-41 SHEET 1 OF 2, PER EA 80599.  EMERGENCY LIGHTS OPS CHECKS NORMAL.  (X)


REMARKS:
BNA - DURING DESCENT NR 2 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED.  REMOVED AND REPLACED OIL FILTER.  PLACARDED FILTERCLOG INDICATOR LIGHT.  (M)


REMARKS:
MCI - AFTER TAKEOFF THE ELFT MAIN GEAR WOULD NOT RETRACT.  REMOVED AND REPLACED LEFT MAIN GEAR DOOR SEQUENCE VALVE, MFGP/N 1U1084.  ACCOMPLISHED GEAR SWING, OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING CRUISE LEADING EDGE AMBER LIGHTS ON FORWARD PANEL ILLUMINATED.  REMOVED AND REPLACED NR 5 LEADING EDGE SLAT SWITCH, MFG P/N 1U11032.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND MULTIPLE CRACKS IN BULKHEAD AND STIFFENER WEBS, FS 1363, RBL 42.5, WL 102 TO WL 143.REPAIRED PER SRM 51-10-02 AND 53-11-00.  (M)


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND AFT BULKHEAD WEB CRACKED AT INBOARD SIDE OF WHEEL WELL STATION 1363, WL 102.  REPAIRED PER SRM 53-11-00 AND 51-10-02.  (M)


REMARKS:
STL - DURING ROUTINE MAINTENANCE, EMERGENCY EGRESS LIGHTS REMAINED ON.  REMOVED AND REPLACED LOW BATTERY PACK, MFG P/N 5822-3.  OPERATIONAL CHECK NORMAL.


REMARKS:
LNK - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR DID NOT RETRACT.  CYCLES LANDING GEAR.  FOUND NOSE LANDING GEAR STRUT LOW.  SERVICED NOSE LANDING GEAR STRUT WITH NITROGEN.  NOSE LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL.  (M)


REMARKS:
MCO - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, LEFT MAIN LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED.  CYCLED LANDING GEAR.  FOUND LEFT MAIN LANDING GEAR DOOR PROXIMITY SENSOR OUT OF ADJUSTMENT.  ADJUSTED PROXIMITY SENSOR TO MAINTENANCE MANUAL LIMITS.  LANDING GEAR DOOR OPERATION AND INDICATION CHECKED NORMAL.


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH FLOOR SUPPORT ANGLE CORROSION STATION 967 TO 947 RBL 6.  REPAIRED PER SRM 51-10-1.  REPLACED WITH IDENTICAL PART NR 65C10592-2.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND TWO DELAMINATION DENTS MEASURING 2 INCH BY 1 INCH BY .050 INCH AND 1 INCH BY .5 INCH .030 INCH LOCATED AT TRAILING EDGE WEDGE ASSEMBLY, OUTBOARD TRAILING EDGE FLAP STATION 260, 6 INCHES FORWARD OF TRAILING EDGE (LOWER SKIN).  REMOVED DAMAGED SKIN AND INSTALLED COMPOSITE REPAIR PLIES AS PER SRM 51-70-17.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND GOUGES, SEAT TRACK SUPPORT CHANNEL FITTING STATION 521, RBL 25, WL 207. REPAIRED PER EA 40888 STEP 3.  (M)


REMARKS:
INT - DURNG Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH AND .75 INCH GOUGE IN SKIN AT BS 800 BETWEEN STRINGER 22R AND STRINGER 24R.  INSTALLED DOUBLER PER SRM 53-00-01.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FUOND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES TOP OF FLOOR BEAM BS 328 LBL 9 TO RBL 21.  CUT OUT SECTION OF UPPER CHORD AND REPAIRED EPR SRM 53-10-51 FIG 205.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES TOP OF FLOOR BEAM BS 344 LBL 50 TO RBL 8.  CUT OUT SECTION OF UPPER CHORD AND SPLICED IN NEW SECTION OF T-CAP PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH OF CORROSION STATION 986.5 FLOOR BEAM UPPER FLANGE AT SCREW HOLES LBL 52 TO RBL 52.  REMOVED UPPER CHORD AND SPLICED IN NEW CHORD PER EA 40883.  CORROSION TASK NR C53-107-02,CORROSION LEVEL 2.  (M)


REMARKS:
PIT - DUIRNG Q6-C3 INSPECTION, FOUND LEVEL 1 CORROSION JUST AFT OF STATIN 1211 ABOVE LONGERON 26R IN WEB MEMBRANE.  CORROSION TASK NR C57-5330 PREVIOUSLY REWORKED.  CUT OUT CORRODED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 3 ANDSRM 53-14-3 FIG 3.  (M)


REMARKS:
ROA - DURNG CX-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION, STRINGER 27 LEFT BETWEEN BS 986 TO 1006. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
PIT - FL 1767 - PRIOR TO DEPARTURE, EMERGENCY EXIT LIGHTS AT ROWS 22, 23 AND 25 AND R-3 AND R-4 DOORS WERE INOPERATIVE. MAINTENANCE REPLACED THE APPROPRIATE BATTERY PACKS.  (M)


REMARKS:
FLT NR 88 - PIT - EMERGENCY TRACK LIGHT AT SEAT 33D INO.  ALL OTHER LIGHTS NORMAL.  REPLACED EMERGENCY LGIHT AT 33D.  OPERATES NORMALLY.  (M)


REMARKS:
CMH - FLOOR PATH EMERGENCY LIGHTING WAS INOPERATIVE.  MAINTENANCE REPAIRED WIRING AT THE FORWARD POWER SUPPLY, SECTIONS1 AND 2 OF THE FLOOR PATH LIGHTING AND THE FORWARD ENTRY DOOR.  (M)


REMARKS:
FLT NR 1543 - CLT - ON TAKEOFF FROM RDU RWY 23R, CAPTAIN HAD GEAR FAULT MESSAGE, RDU TOWER TOLD HIM IT LOOKED LIKE SOMETHING FELL OFF THE AIRCRAFT.  WHILE THE FLIGHT HELD IN THE AIR OVER RDU, THEY FOUND THE NR 2 MAIN WHEEL ASSEMBLY.  FLIGHT PROCEEDED TO CLT.  WHEEL DEPARTED AIRCRAFT DUE TO CIRCUMFERENTIAL WHEEL FAILURE DUE TO A BENT BRAKE HEAT SHIELD.  MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR.  (M)


REMARKS:
FLT NR 770 - ROA - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF.  OUTFLOW VALVE INDICATED CLOSED IN AUTO, STANDBY, AND MANUAL.  RETURNED TO FIELD.  MAINTENANCE FOUND AC AND DC CANNON PLUGS DISCONNECTED FROM THE OUTFLOW VALVE.  SECURED PLUGS, OPS CHECK NORMAL.


REMARKS:
ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK SKIN, STRINGER 19 LEFT BS 807.  INSTALLED DOUBLER, REPAIRED EPR SRM 53-30-3.  (M)


REMARKS:
MIA - FLT 538 - LEFT EMERGENCY DOOR (L3) WARNING LIGHT CAME ON DURING CLIMB-OUT FROM MIA.  AIRCRAFT RETURNED TO FIELD.MAINTENANCE PERFORMED DOOR FIM PROCEDURE.  NO PROBLEMS WERE FOUND.  DOOR WAS CHECKED OPERATIONALLY AND NO PROBLEMS WERENOTED.  AIRCRAFT WAS RELEASED FOR SERVICE.  REFERENCE:  OPERATOR CONTROL NR USAABB96006A.


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 4 AREAS 1 INCH BY 1 INCH CORRODED AREAS FLOOR BEAM BS 947, LBL 4 - RBL 11.  INSTALLED T-CAP AND REPAIR ANGLES.  REPAIRED PER SRM 53-00-051 AND EA 40947.  (X)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND .75 INCH CORROSION FLOOR BEAM BS 967, RBL 42.  CUT OUT CORRODED AREA,FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER.  REPAIRED PER SRM 53-60-51, FIGURE 203.  (X)


REMARKS:
INT - DURING 'Q-1' CHECK, VISUAL INSPECTION FOUND 10 AREAS 1 - 2 INCH SQUARES OF CORROSION FLOOR BEAM (FLOOR BOARD HOLES) BS 986.5, RBL 46 - LBL 46.  CUT OUT CORRODED UPPER T-CAP AND REPLACED T-CAP, PLACING A SPLICE AT LBL 7, REPAIRED PER EA 40946.  (X)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA BS 344 FLOOR BEAM LBL 9 INCH AND LBL 21 INCH.  INSTALLED T-CAP FROM RBL 17 TO LBL 36, REPAIRED PER T.R. 53-10-03.  CORROSION LEVEL 2.  CORROSION TASK NR C53-107-02.  (X)


REMARKS:
INT - DURING 'Q-1 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS BS 328 FLOOR BEAM, RBL 14 INCHTO RBL 56 INCH.  SPLICED SECTION AND REPAIRED PER SRM 53-10-01.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA, BS 312, FLOOR BEAM BL ZERO.  CUT OUT CORRODED SECTION OF UPPER CHORD FROM LBL 38 TO RBL 25 AND SPLICED IN NEW CHORD SECTION.  REPAIRED PER T.R. 53-10-03.  CORROSION TASK NR C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
CLT - INSPECTION VISUALLY FOUND SURFACE LEVEL 1 CORROSION .50 INCH IN DIAMETER AROUND NUT CLIP HOLES LOCATED AT FS 328 - RBL 12 TO RBL 56.  CUT CORRODED T-CAP OFF AND REINSTALLED SAME PER BOEING SRM 53-10-03.  (X)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 1 CORROSION AROUND SCREW HOLES 30 INCH LENGTH ON TOP OF BEAM LOCATED AT STA 344 -181 BL TO 12 RBL.  CUT CORRODED BEAM T-CAP OFF AND REPLACED PER BOEING SRM 53-10-51.  (X)


REMARKS:
CLT - INSPECTION VISUALLY FOUND A LEVEL 1 SURFACE CORROSION MEASURING 3 INCH BY 85 INCH LOCATED AT BEAM STA 986.5 - LBL29.0 TO RT AFT SERVICE DOOR.  REPAIRED UPPER FLANGE (INSTALLED REPAIR FLANGE) PER USAIR TYPICAL REPAIR 53-10-05.  (X)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION MEASURING 3 INCH BY 60 INCH LOCATED AT LT ENTRY AFT DOOR THRESHOLD LOCATED AT STA 947 THROUGH STA 1006.  INSTALLED REPLACEMENT ANGLE PER BOEING SRM 51-10-02.  (X)


REMARKS:
ROA - DURING 'CX-4' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN SKIN AND BEAR STRAP FORWARD SERVICE DOOR CUT OUT (LOWER AFT CORNER) STA 328.  REPAIRED DOUBLER, PN 65C27287-13, REPAIR DOCUMENT T.R. 53-10-19, REV A.  (X)


REMARKS:
SMF - FLT 68 - AFTER TAKEOFF FROM SFO, CREW NOTED LOSS OF OIL FROM LT ENGINE.  CREW SHUT DOWN ENGINE.  FLIGHT DIVERTED TO SMF AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE TOWER SHAFT SEALS.  (X)


REMARKS:
BNA - FLT 1426 - UPON GEAR RETRACTION, CREW GOT TWO GREEN LIGHTS ON THE MAIN GEAR AND RED LIGHT ON THE NOSE GEAR.  CREWALSO HEARD A LOUD NOISE FROM THE NOSE GEAR AREA.  RETURNED TO FIELD.  (X)


REMARKS:
DAY - FLT 282 - ON DESCENT INTO IND, CAPTAIN'S ALTIMETER AND AIR DATA COMPUTER WERE ERRATIC.  DUE TO WEATHER AT IND, FLIGHT DIVERTED TO DAY AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR 1 AIR DATA COMPUTER.  (X)


REMARKS:
CLT - FLT 729 - DURING CLIMB-OUT WITH ONE CSD ON MEL AND THE APU RUNNING, APU EXPERIENCED AN OVERSPEED AND SHUTDOWN.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE MULTI-SPEED ELECTRONIC SWITCH.  (X)


REMARKS:
CLT - FLT 1850 - AFTER TAKEOFF FROM CLT, CREW RECEIVED NR 1 FUEL HEAT LIGHT AND NR 1 OIL TEMPERATURE ROSE INTO THE YELLOW ARC.  CREW REDUCED POWER TO ENGINE.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND PIN IN FUEL HEAT VALVE CONNECTOR D1004 PUSHED BACK.  CONNECTOR WAS REPAIRED.  (X)


REMARKS:
CLT - FLOOR TRACK LIGHTING SEGMENT FOUND INOPERATIVE.  REPAIRED EXPOSED WIRING.  (X)


REMARKS:
JFK - AFTER TAKEOFF THE NOSE GEAR DID NOT FULLY RETRACT.  REMOVED AND REPLACED NOSE GEAR STRUTS SEALS, MFG P/N A03772REVH.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
ON FLT NR 183 - ATL-MSY - DIVERTED TO MGM, EN ROUTE TO MSY NR 2 ENGINE OIL QUANTITY WENT TO ZERO THEN OIL PRESSURE DROPPED TO 35 PSI, SHUT DOWN NR 2 ENGINE AND LANDED IN MGM.  MAINTENANCE FOUND OIL LEAKING FROM THE STARTER OIL SEAL ON GEARBOX.  REMOVED STARTER AND REPLACED STARTER SEAL AND REINSTALLED STARTER IAW MM 72-60.  PERFORMED LEAK CHECK AND PART POWER ENGINE RUN.  NO DEFECTS NOTED.


REMARKS:
PBI - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT MAIN GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED.  CYCLED LANDING GEAR.  REPLACED LANDING GEAR ACCESSORY BOX, MFG P/N 65-37568-19, AND LANDING GEAR INDICATION CHECKED NORMAL.


REMARKS:
STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR.  FOUND BROKEN WIRE TO PIN 7 OF UPLIMIT SWITCH, MFG P/N H14-6.  REPAIRED WIRE TO PIN 7 AND NOSE LANDING GEAR INDICATION CHECKED NORMAL.  (M)


REMARKS:
STL - DURING APPROACH AIRCRAFT REQUIRED EXCESSIVE AILERON TRIM CHANGE WHEN POWER AND SPEED CHANGED, AND MORE POWER THANNORMAL TO MAINTAIN PROPER SINK RATE.  FOUND LEFT AILERON INBOARD HINGE EYEBOLT BEARING, MFG P/N DMD6-7E1-501, WORN.  REPLACED HINGE EYEBOLT AND AILERON SYSTEM OPERATION CHECKED NORMAL.  (M)


REMARKS:
STL - DURING CRUISE, EGRESS LIGHTS AT SEAT ROW 15 THROUGH 19 ILLUMINATED.  FOUND LIGHTING SYSTEM BATTERIES, MFG P/N 3350-0026-21, WEAK.  REPLACED BATTERIES AND EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL.  (M)


REMARKS:
MCI - DURING CRUISE, SHUT DOWN NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY.  FOUND OIL LINE, MFG PN A02923-1, FROM SNUBBER 'T' TO OIL PRESSURE TRANSMITTER, FRACTURED.  REPLACED OIL LINE AND SERVICED OIL.  ENGINE OPERATION AND LEAK CHECKS NORMAL.  (M)


REMARKS:
STL - DURING APPROACH, LEADING EDGE SLATS WOULD NOT EXTEND.  RESET RIGHT SLAT ASYMMETRY LOCKOUT.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING ROUTINE MAINTENACNE CHECK, EXTERIOR EMERGENCY LIGHTS DID NOT ILLUMINATE.  FOUND BATTERIES, MFG P/N 41B030CF00101, WEAK.  REPLACED BATTERIES AND EXTERIOR LIGHT OPERATION CHECKED NORMAL.  (M)


REMARKS:
PHL - FLT NR 304 - DURING CRUISE SHUT DOWN NR 3 ENGINE, S/N 1539, DUE TO FILTER BYPASS LIGHT ILLUMINATING.  FOUND OIL FILTER BYPASS SWITCH AT FAULT.  REPLACED OIL FILTER BYPASS SWITCH, MFG P/N A00803-2 AND ENGINE OPERATION AND INDICATION CHECKED NORMAL.  (M)


REMARKS:
LAX - FLT NR 15 - DURING CRUISE LEFT AISLE EGRESS LIGHT AT SEAT ROWS 30 TO 35 AND L3 DOOR, ILLUMINATED.  CYCLED SWITCH AND BACK TO ARMED.  FOUND POWER SUPPLY, MFG P/N 5822-43, FAULTY.  REPLACED POWER SUPPLY AND EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL.  (M)


REMARKS:
STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED.  CYCLED LANDING GEAR.  FOUND INTERNAL MALUNCTION IN LANDING GEAR ACCESSORY BOX AND NOSE LANDING GEAR INDICATION CHECKED NORMAL.(M)


REMARKS:
STL - AFTER TAKEOFF SHUT DOWN NR 2 ENGINE, S/N 2153, DUE TO FIRE WARNING.  FOUND 13TH STAGE ANTI-ICE DUCT TO NOSE COWL RUPTURED, MFG P/N 5005253.  REPLACED ANTI-ICE DUCT.  ENGINE OPERATION AND INDICATION SYSTEMS CHECKED NORMAL.  (M)


REMARKS:
MSY - ON LANDING, NOSE LANDING GEAR DOOR LIGHT ILLUMINATED.  FOUND NOSE GEAR DOOR MECHANISM 'A' ROD, MFG P/N 69-67889-7, FRACTURED.  REPLACED NOSE GEAR DOOR MECHANISM 'A' ROD AND RIGGED NOSE GEAR DOOR SYSTEM.  NOSE GEAR AND DOOR OPERATION CHECKED NORMAL.  (M)


REMARKS:
ON FLT NR 444 - ATL-ATL - AIR RETURN, STRONG ACRID ODOR IN COCKPIT IN CLIMB-OUT SIMILAR TO ELECTRICAL SMOKE.  INSPECTEDELECTRICAL SYSTEM IN AND AROUND FLIGHT DECK AREA AND GALLEY.  RAN BOTH ENGINES, FOUND AN OVERHEATED COFFEE MAKER HOT PLATE.  REMOVED AND REPLACED COFFEE MAKER, OPS CHECK GOOD.


REMARKS:
FLT NR 283-2 - IAD-FLL - DIVERTED TO ATL, UNABLE TO CONROL CABIN PRESSURE AT FL 230, CABIN ALT WAS 9,000 AND CLIMBING AT 700 FPM WITH OUTFLOW VALVE FULLY CLOSED.  RECONNECT DUCT FWD OF RIGHT WATER SEPARATOR HOUSING, PRESSURIZED A/C, OPS CHECK GOOD.  REF MM 36-10.


REMARKS:
FLT NR 381 - BOS-BOS - AIR RETURN, LANDING GEAR HANDLE WOULD NOT MOVE TO RETRACT POSITION FOLLOWING TAKEOFF.  FOUND NOSE STRUT UNDER INFLATED, SERVICED NOSE STRUT FULLY.  IN FLIGHT MODE WAS OBTAINED, LOWERED STRUT TO PROPER LEVEL, OPS CHECK GOOD.  REF MM 32-30.


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND SEVERAL AREAS OF LEVEL 1 CORROSION PREVIOUSLY REWORKED APPROXIMATELY 1 INCH BY 2 INCH SECTIONS FROM STATION 370 T0 427 CARGO DOOR PAN LOWER SECTION.  SPLICED IN NEW LOWER PAN SECTION PER SRM 53-05 FIG 44.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND 1 INCH CRACK IN STATION 1437 LONGERON 4L FUSELAGE SKIN.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND A 1 INCH CRACK IN STATION 1437 LONGERON 4R FUSELAGE SKIN.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27.  (M)


REMARKS:
PIT - DURING C-3 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LEFT DORSAL FIN DRAG ANGLE AT STATION 1126.  STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-05 PG 506.  (M)


REMARKS:
PIT - DURING C-4 CHECK INSPECTION, FOUND .125 INCH CRACK IN SKIN COMING FROM RIVET AT LOWER AFT CORNER OF MED STAIR DOOR OPENING STATION 200.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 57A.  (M)


REMARKS:
PIT - DURING C-4 CHECK INSPECTION, FOUND .125 INCH CRACK AT SKIN CLIP EMINATING FROM RIVET AT STATION 775 ON RIGHT SIDELONGERON NR 1.  INSTALLED CLASS 2 REPAIR DOUBLER PER SRM 53-04 FIG 12B.  (M)


REMARKS:
PIT - DURING C-4 CHECK INSPECTION, FOUND .125 INCH CRACK AT SKIN CLIP EMINATING FROM A RIVET AT STATION 699 RIGHT LONGERON NR 1.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 12B CLASS 2.  (M)


REMARKS:
PIT - DURING C-4 CHECK INSPECTION, FOUND .125 INCH CRACK IN SKIN CLIP EMINATING FROM RIVET AT STATION 658 RIGHT SIDE LONGERON NR 1.  INSTALLED DOUBLER REPAIR CLASS 2 PER SRM 53-04 FIG 12B.  (M)


REMARKS:
PIT - PILOT REPORTED AFTER WALK AROUND THAT THERE WAS A 1 INCH CRACK IN THE LEFT WING LEADING EDGE NR 1 SLAT SKIN AT STATION XF-126 ABOVE TELESCOPING ANTI-ICE DUCT.  REMOVED CRACK AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 57-02 FIG 6.  AIRCRAFT RETURNED TO SERVICE.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND .25 INCH BY 2 INCH CHAFFED .021 DEEP AT VERTICAL STABILIZER FORWARD LEFT SKIN.  INSTALLED DOUBLER REPAIR PER SRM 55-01 FIG 2 SHEET 2.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND SEVERAL 1 INCH BY 2 INCH AREAS OF LEVEL 1 CORROSION FLOOR BEAM RIGHT AFT LAV STATION 1338 IN UPPER CAP ANGLE '1'.  CORROSION TASK NR C58-53300.  SPLICED IN NEW SECTION OF UPPER CAP ANGLE PER USAIR TYPICAL REPAIR 53-10-14.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL I CORROSION FORWARD CARGO LOWER DOOR PAN AT STATION 370 TO 427.  CORROSION TASK NR C51-53300.  REMOVED AND REPLACED LOWER PAN WITH MODIFIED PAN P/N J060228-3 PER SRM 53-05 FIG 44.  (M)


REMARKS:
PIT - DURING Q-4 INSPECTION DISCOVERED A CRACK 38.75 INCH LONG FORWARD FUSELAGE EXTERIOR SKIN FROM XPONDER ANT TO TCAS ANT STATION 247 TO 285 RUNNING ALONG LONGERON NR 1.  AREA UNDER ADF CORRODED.  (M)


REMARKS:
DURING Q-3/C-5 CHECK INSPECTION, FOUND 3.5 INCH CRACK IN FORWARD UPPER CORNER OF DOOR FRAME IN DOOR JAM 'Z' CHANNEL.  RIGHT INBOARD GEAR DOOR.  INSTALLED DOUBLERS J060200-52 AND -54 PER SRM 52-05 FIG 28.  (M)


REMARKS:
PIT - DURING Q6/C3 INSPECTION, FOUND LEVEL I CORROSION AT SKIN CLIP STATION 1307 FROM FLOOR LINE TO BULKHEAD SUPPORT.  CORROSION TASK NR C-58-53305 PREVIOUSLY REWORKED.  MFG NEW SKIN CLIP P/N 9912043 PER DOUGLAS DRAWING 9912243.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 13 INCH CRACK FORWARD RIGHT SERVICE DOOR, LOWER GATE HINGE.  REPAIRED PER EA 40887.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 30 INCH BY 1 INCH FLOOR BEAM STATION 1006 BL '0' TO LBL 30.  INSTALLED FILLER AND STRAPS, REPAIRED PER TR 53-10-01A.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA ON STRINGER 20L, BS 767 STRINGER.  INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 1.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 5 INCH BY 2 INCH, 1 INCH BY 2 INCH AND 1 INCH BY 4 INCH FLOORBEAM STATION 967 LBL 6, LBL 30, LBL 20 TO LBL 25.  INSTALLED T-CAP, REPAIRED ANGLES AND STRAPS.  REPAIRED PER TR 53-10-05C.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 10 INCH BY 2 INCH, 2 INCH BY 33 INCH FLOOR BEAM STATION 987 RBL 12 TO RBL 45, LBL TO LBL 30.  INSTALLED T-CAP REPAIR ENTIRE LENGTH, REPAIRED PER TR 53-10-05C.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SIX 1 INCH BY 1 INCH CORRODED AREA AT FLOOR BEAM BS 344 LBL 50 INCH TO BL 'O'.  SPLICED IN NEW SECTION OF T-ANGLE CAP.  INSTALLED REPAIR ANGLES.  REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO CORRODED AREAS 7 INCH BY 1 INCH AT STRINGER BS 967 TO BS 974 AND BS976 TO BS 982, S-25 L.  REMOVED CORRODED STRINGER SECTION, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-3.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 3 CRACKS .25 INCH AT WEB FOR FLOOR BEAM BL '0' BS 708 TO BS 713 WL 203. INSTALLED DOUBLERS, REPAIRED PER SRM 51-40-2.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKED WEB, FLOOR BEAM BS 709 TO 712 BL 25 R WL 203.  CUT OUT CRACKED SECTION OF WEB, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2 FIG 1.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK FRAME INNER CHORD, STATION 616 WL 203 LBL 60 LEFT SIDE.  INSTALLED DOUBLER, PER EA 40894.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK SKIN LOWER HINGE CUTOUT LOWER CORNER OF SERVICE DOOR.  INSTALLED DOUBLER, REPAIRED PER TR 52-10-05.  (M)


REMARKS:
PIT - DURING Q6/C3 INSPECTION, FOUND LEVEL 1 CORRSION PREVIOUSLY REWORKED AT STATION 1250 ON CUSP MEMBRANE.  CORROSION TASK NR C58-53301.  FABRICATED NEW SECTION OF CUSP MEMBRANE OF 7075-T6 .040 INCH BY 10 INCHES WIDE FROM FUSELAGE TO SEATTRACK PER SRM 53-05 FIG 97.  (M)


REMARKS:
PIT - DURING Q6/C3 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON FLOOR BEAM UNDER RIGHT LAV FLOOR PAN AT STATION 1322 UPPER FLANGE.  CORROSION TASK NR C58-53300.  CUT OUT DAMAGED AREA AND INSTALLED FABRICATED DOUBLERS PER SRM 53-05 FIG 73A AND USAIR EA 32198.  (M)


REMARKS:
ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 2.5 INCH CRACK FUSELAGE SKIN STRINGER 18L BS 767.  INSTALLED DOUBLER, REPAIRED PER SRM 53-30-01.  (M)


REMARKS:
ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORROSION S-27L BS 980 TO 992 STRINGER.  REMOVED DAMAGED STRINGER, INSTALLED NEW STRINGER AND STRINGER SPLICE.  REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
PIT - DURING SIP VISIT INSPECTION, FOUND 2 INCH CRACK LEFT WING FUEL TANK 'Z' STRINGER NR 13 JUST OUTBOARD OF STATION 4700, SIP REF 57-10-01.  INSTALLED DOUBLER REPAIR PER USAIR EA NR 32309.  (M)


REMARKS:
PIT - DURING SIP VISIT INSPECTION, FOUND .125 INCH CRACK IN FRAME STRIP AFT LEFT CORNER OF NOSE LANDING GEAR WHEEL WELLSIP REF 53-10-24.  ROUTED OUT CRACKED AREA AND PRIMED AND PAINTED PER SRM 53-02-18 FIG 10 PARA 7.  (M)


REMARKS:
PIT -DURING SIP VISIT INSPECTION, FOUND .375 INCH CRACK IN FUSELAGE SKIN AT LEFT NR 2 WINDOW POST ATTACH FLANGE.  EDDY CURRENT INSPECTION REF SIP 53-10-08, PG 2.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER USAIR EA NR 32299.  (M)


REMARKS:
PIT - FLT 10 - DURING TAKEOFF FROM PIT, THE LEFT AIR CONDITIONING PACK KICKED OFF.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE PERFORMED BITE ON THE PACK CONTROLLERS.  NO FAULT WAS FOUND.  THE RIGHT PACK TEMPERATURE CONTROL VALVE WAS REPLACED AS PRECAUTION.  (M)


REMARKS:
LGA - FL 8002 - CREW REPORTED, THAT THE AIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FEET.  FLIGHT DIVERTED TO LGA AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE CABIN PRESSURE AMPLIFIER.  (M)


REMARKS:
DCA - FLT NR 2287 - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW COULD NOT RETRACT THE NOSE GEAR.  CREW CYCLED THE GEAR TWICE WITH THE SAME RESULT.  FLIGHT RETURNED TO DCA AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE CHECKED THE RETRACTION OF THE NOSE GEAR, AND CYCLED IT SEVERAL TIMES.  CHECKED GROUND SENSE CONTROL AND ANTI-RETRACTION CABLE RIG.  NO PROBLEMS FOUND.  SERVICED STRUT TO CORRECT PRESSURE.  (M)


REMARKS:
PIT - FLT 858 - FLT RETURNED TO FIELD WHEN APU SHUTDOWN.  LEFT GENERATOR WAS ON MEL.  MAINTENANCE REPLACED THE APU BURNER CAN AND THE LEFT GENERATOR, CSD AND COOLER.  (M)


REMARKS:
FLT NR 349 - BWI - DURING RETRACTION NOSE GEAR MADE LOUD NOISE, CYCLED NO HELP.  MAINTENANCE FOUND RT DOOR OPEN, CLOSEDDOOR, BOTH DOOR LATCHES CHECKED OK.  (M)


REMARKS:
FLT NR 517 - PHL - GALLEY EMERGENCY CHUTE PRESSURE IS 2500 PSI IN RED ZONE.  REPLACED GALLEY EMERGENCY CHUTE.  (M)


REMARKS:
FLT NR 307 - LGA - LEFT AFT CABIN DOOR CHUTE DEPLOYED WHEN IT FELL FROM THE DOOR AFTER UTILITY ENTERED.  GIRT BAR WAS STOWED AND CAUGHT ON DOOR WHEN SLIDE PACK FELL.  (M)


REMARKS:
FLT NR 307 - LGA - LEFT AFT CABIN DOOR CHUTE DEPLOYED WHEN IT FELL FROM THE DOOR AFTER UTILITY ENTERED.  GIRT BAR WAS STOWED AND CAUGHT ON DOOR WHEN SLIDE PACK FELL.  MAINTENANCE REPLACED THE AFT DOOR EMERGENCY SLIDE.  NO PROBLEM EXISTED WITH THE SLIDES AS IT FUNCTIONED AS DESIGNED.  (M)


REMARKS:
FLT NR 1426 - BNA - UPON GEAR RETRACTION THE CREW GOT TWO GREEN LIGHTS ON THE MAIN GEAR AND RED LIGHT ON THE NOSE GEAR. CREW ALSO, HEARD A LOUD NOISE FROM THE NOSE GEAR AREA.  RETURNED TO FIELD.  (M)


REMARKS:
CLT - FLT 1426 - IMMEDIATELY AFTER TAKEOFF FROM CLT, THE RIGHT ENGINE 'B' FIRE LOOP LIGHT ILLUMINATED.  SHORTLY THEREAFTER, THE RIGHT ENGINE FIRE WARNING LIGHTS ILLUMINATED.  CREW REDUCED POWER ON THE ENGINE AND THE LIGHTS WENT OUT.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  ENGINE WAS NOT SHUT DOWN IN FLIGHT.  MAINTENANCE FOUND THE THIRTEENTH STAGE FUEL HEAT MANIFOLD LEAKING, REPLACED IT.  (M)


REMARKS:
YUL - FLT 451 - ON APPROACH, WITH GEAR SELECTED DOWN, CREW RECEIVED NOSE GEAR UNSAFE LIGHT.  CREW CYCLED THE GEAR, AND INDICATIONS WERE NORMAL.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE NOSE LANDING GEAR PROXIMITY SENSOR.  (M)


REMARKS:
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LIGHTING STRIKE HOLE APPROXIMATELY .250 INCH IN DIAMETER IN UPPER SKIN 30 INCH FROM INBOARD END AND 18 INCH AFT OF LEADING EDGE.  INSTALLED DOUBLER REPAIR PER SRM 55-03 FIG 15.  (M)


REMARKS:
ON DESCENT AT 24,000 FL, NUMBER 1 ENGINE O/B THRUST REVERSER SLEEVE PARTIALLY SEPARATED FROM AIRCRAFT.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT AUS.  REINSTALLED NEW SLEEVE PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 7 FT AFT OF AFT CARGO DOOR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED BC3 CHECK, FOUND CRACK AT RT HORZ STAB AT RIB STA 120.3 AND 129.5 ON AFT SPAR ON RT LOWER IN SPAR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C-CHECK, FOUND RT WING, AFT I/B PYLON PANEL CRACKED AT AFT BOTTOM PANEL(NR 5843R).  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C-CHECK, FOUND SKIN WRINKLED AT AFT PRESSURE BULKHEAD AT BS 1016, BETWEEN S9L TO S11L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR BEAM SUPPORT STRAP CORRODED AFT OF BS 727D, RBL 16.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND WEB AT LOWER AFT CORNER OF FWD CARGO DOOR CUTOUT DAMAGED.  REPAIRED PER SWA RA 1-A53-1285.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND A 3 INCH CRACK, 41 INCHES FWD OF OUTFLOW VALVE AT RIGHT AFT FUSELAGE.  REPAIRED PER SWA RA 1-A53-1285.


REMARKS:
BAGGAGE CART STRIKE TO LEFT SIDE FUSELAGE WHILE PARKED AT GATE, BETWEEN BS 807 AND 827, AT S24L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND LOWER FUSELAGE SKIN CRACKED 2 PLACES, FWD OF AIR CONDITIONING SERVICE PANEL,  MEASURING .25 BY 1.5.  REPAIRED BOTH PER BOEING SRM.


REMARKS:
FLT NR 2278 - LGA - AT FL 150 LOST RIGHT CSD.  THE FLIGHT RETURNED TO FIELD AT LGA.  THE APU WAS ON MEL.  NR 2 CSD DISCONNECTED FOR HIGH OIL PRESSURE.  MAINTENANCE FOUND NR 2 CSD OVER SERVICED WITH OIL.  DRAINED OIL LEVEL TO NORMAL.  REMOVED AND REPLACED CSD FILTER AS PRECAUTION.  CHECKED IAW MM OPS CHECK OK.  (M)


REMARKS:
FLT NR 430 - OKC - AFTER TAKEOFF, FOLLOWING GEAR RETRACTION, GEAR DOOR LIGHT STAYED ON.  CHECKED AND LUBRICATED LANDINGGEAR CONTROL VALVE.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
ON FLT NR 525 - ATL-DFW - RIGHT ENGINE FUEL HEAT VALVE STUCK IN THE OPEN POSITION.  AIRCRAFT RETURNED TO ATL.  REMOVED AND REPLACED ENGINE FUEL HEAT VALVE PER MM 73-10.  LEAK CHECK GOOD.  (M)


REMARKS:
ON FLT 101 - ATL - AIR RETURN, AFTER GEAR RETRACTION THE LEFT GEAR UNSAFE LIGHT STAYED ON AND GEAR DOOR OPEN LIGHT STAYED ON, CYCLED ONCE, NO CHANGE.  FOUND BUNGEE CYCLE PISTON ROD BROKEN.  REPLACED PER MM 32-10.  ACCOMPLISHED GEAR SWING.(M)


REMARKS:
ON FLT NR 248 - AIR RETURN, DURING CLIMB-OUT OF ATL IN MANUAL PRESSURE AND CABIN AT 5000 FEET.  CLIMBING AT 500 FPM NR 1 FLIGHT ATTENDANT ADVISED THE CREW THAT ALL OXYGEN MASKS HAD DROPPED.  NO WARNING FROM THE COCKPIT AND NO CABIN PRESSURE LIGHT.  PERFORMED OPERATIONAL CHECK OF MASKS, CLEANED AND RESTOWED MASKS, OPS CHECK GOOD PER MM 35-20-00.  (M)


REMARKS:
ON FLT NR 236 - DFW - THE LEFT ENGINE FAILED AFTER TAKEOFF.  REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL PER MM 73-00, NO HELP.  REMOVED AND REPLACED ENGINE PER MM 71-00, OPS CHECK AND LEAK CHECK GOOD.  (M)


REMARKS:
ON FLT NR 236 - DFW-DFW - AIR RETURN AFTER TAKEOFF, LEFT ENGINE FAILED.


REMARKS:
ON FLT NR 270 - ATL - AIR RETURN, WEATHER RADAR INOP.  REMOVED AND REPLACED CONTROL PANEL.  OPS CHECK NORMAL PER MM 34-40.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK, 2 INCH CRACK, 1 INCH CRACK AND .5 INCH CRACK AT 178 BULKHEAD WEB AT LOWER LEFT RADAR DISH MOUNT.  INSTALLED DOUBLER REPAIR, REPAIRED PER TR 53-10-11.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 BULKHEAD SKIN.  INSTALLED DOUBLER, REPAIRED PER TR 53-10-11.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH LONG CRACK STATION 727 UPPER COMPRESSION CHORD ANGLE.  INSTALLEDREPAIR ANGLE, REPAIRED PER TR 53-10-03.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 178 WL 210 AT SKIN.  INSTALLED DOUBLER, REPAIRED PER TR53-10-11.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 767 STRINGER 19 R FUSELAGE SKIN.  INSTALLED REPAIR, REPAIRED PER SRM 53-30-3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 767 STRINGER 19 RT.  INSTALLED REPAIR, REPAIRED PER SRM53-10-3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER APPROXIMATELY 10 INCHES BY .5 INCH STRINGER 29L STATION 947 TO 957.  REPLACED APPROXIMATELY 22.5 INCHES OF STRINGER.  REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK SKIN BS 970 STRINGER 21L.  DOUBLER INSTALLED PER SRM 53-30-3, REPAIRED PER SRM 53-30-3.  (M)


REMARKS:
ROA - DURING CX-4 CHECK VISUAL INSPECTION FOUND 2 INCH BY 20 INCH CORROSION STRINGER 27 LEFT FROM BS 947 TO BS 967 DUE TO LAV SPILLS.  REMOVED DAMAGED SECTION OF STRINGER.  FABRICATED NEW STRINGER, DOUBLERS, SPLICES AND SHIMMS, INSTALLED SAME.  REPAIRED PER SRM 53-10-3 FIG 1.  (M)


REMARKS:
BOS - FLT NR 16 - EN ROUTE PHL-CDG, CREW NOTED THE LEFT FUEL BOOST PUMP LIGHT ILLUMINATED.  CREW ELECTED TO DIVERT TO BOS.  MAINTENANCE REPLACED THE LEFT FORWARD FUEL BOOST PUMP OUTPUT PRESSURE SWITCH.  (M)


REMARKS:
CLT - FLT 2052 - CREW COULD NOT RETRACT GEAR AFTER TAKEOFF.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  (M)


REMARKS:
CLT - FLT 2052 - CREW COULD NOT RETRACT GEAR AFTER TAKEOFF.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LANDING GEAR LEVER LATCH SOLENOID.  (M)


REMARKS:
FLT NR 2195 - DCA - ON CLIMB-OUT, NR 1 ATTITUDE FLAG CAME IN VIEW.  HEADING FLAG ON HSI IN VIEW.  MAINTENANCE REPLACED NR 1 IRU AND PERFORMED OPS CHECK.  SYSTEM CHECKS NORMAL.  (M)


REMARKS:
FLT NR 627 - PIT - TEN MINUTES AFTER LEVEL OFF (31,000) IN CRUISE THERE WAS A (4) KNOB THROTTLE SPLIT.  ENGINE 1 WAS BEHIND ENGINE 2.  PMCS WERE TURNED OFF.  THE SPLIT REMAINED.  ALL OTHER INDICATIONS WERE NORMAL.  MAINTENANCE ACCOMPLISHEDMEC ADJUSTMENT OF NR 1 ENGINE IAW MM 71-00-00 TEST 6.  ACCOMPLISHED PART POWER TRIM RUN AND TAKEOFF RUN.  NO THROTTLE SPLIT NOTED.  RIG CHECK NORMAL.  (M)


REMARKS:
LAX - FLT 41 - AT FL 240, RT ENGINE EXPERIENCED COMPRESSOR STALL.  PASSENGER REPORTED SMOKE AND FLAMES FROM RT ENGINE, AND ACRID SMOKE FILLED THE CABIN.  SMOKE DISSIPATED QUICKLY.  CREW DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE PERFORMED A BORESCOPE OF THE COMPRESSOR, COMBUSTION CHAMBER, AND TURBINE NOZZLE SECTIONS OF THE RT ENGINE.  FAN BLADE TAP TEST AND CHIP DETECTOR INSPECTION WERE COMPLETED.  NO DISCREPANCIES WERE FOUND.  AIRCRAFT WAS RETURNED TO SERVICE.  (X)


REMARKS:
CLT - FLT 242 - AFTER TAKEOFF, CREW RECEIVED A NR 2 BLEED FAULT MESSAGE AND THEN A NR 2 DUCT LEAK MESSAGE.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND A CRACKED LINE IN THE NR 2 ENGINE SUB WING TEST BLOCK AREA.  A TEMPORARY LINE WAS INSTALLED AND A PERMANENT LINE PROGRAMMED.  (M)


REMARKS:
GSO - FL 8028 - AT APPROXIMATELY 600 FEET AGL AFTER TAKEOFF FROM GSO, THE LEFT ENGINE EXPLODED.  TOWER ADVISED CREW THAT ENGINE WAS TRAILING SMOKE AND FIRE.  FLIGHT RETURNED TO GSO AND GROUND EMERGENCY CREWS EXTINGUISHED THE ENGINE FIRE.  NO FIRE WARNINGS RECEIVED IN COCKPIT.  SINGLE ENGINE TIME 4 MINUTES.  MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE AND TRIM RAN PER JOB CARD.  (M)


REMARKS:
ON CLIMBOUT, NUMBER 1 ENGINE START VALVE LIGHT ILLUMINATED, UNABLE TO RESET.  PERFORMED ENGINE SHUTDOWN CHECKLIST AND AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING.  REMOVED AND REPLACED START VALVE PER BOEING M/M.


REMARKS:
ON CLIMBOUT, CREW HAD TO USE OVERRIDE TRIGGER TO RAISE GEAR HANDLE, GEAR EXTENDED NORMALLY.  AIRCRAFT RETURNED TO SLC AND MADE AN UNEVENTFUL LANDING.  AIRCRAFT MX FERRIED TO PHX, ADJUSTED GROUND SHIFT SENSOR PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E S15R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND BULKHEAD SKIN CRACKED AT CONTROL CABIN LEFT SIDE, 6 INCHES UP FROM FLOOR AND 6 INCHES FROM O/B EDGE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LEFT FRAME CRACKED AT BS 349 WL 225.  REPLACED FRAME CHORD PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 294 RBL 55 WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED FWD OF SERVICE DOOR AT BS 289 WL 248.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 302 AT S10L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND AFT SECTION OF CABIN FLOOR TRACK LIGHTING INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, 1.5 INCH LENGTH.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C-CHECK, FOUND EXTERNAL POWER DOOR JAMB CRACKED, 1.5 INCH LENGTH.  REPAIRED PER SWA RA 1-353-1447.


REMARKS:
FLT NR 360, RDU-BOS, LEFT MAIN GEAR UNSAFE INDICATION ON GEAR DOWN.  REPLACED NR 1 MLG DOWN LOCK SWITCH, OPS CHECK NORMAL, REF 32-50-1.  GEAR SWING ACCOMPLISHED.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 747 AT STRINGER 5R TIE CLIP.  MODIFIED PART NR 69-35352-14, REPAIRED PER EO 5393G227.  (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND 1.5 INCH CRACK UPPER LEADING EDGE SURFACE HORIZONTAL STABILIZER LEFT SIDE APPROXIMATELY 6 FEET OUTBOARD OF VERT STAB.  INSTALLED DOUBLER REPAIR .071 2024TS ALU PER SRM 55-03 FIG 3 AND SRM 55-01 FIG 2. (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND TWO 2 INCH CRACKS IN CUSP MEMBRANE STATION 617 RIGHT SIDE.  REPLACED SECTION OF CUSP MEMBRANE FROM STATION 598 TO 637 PER SRM 53-05 FIG 97.  (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND 1 INCH CRACK IN LONGERON 17L, AT STATION 945.  SPLICED IN LONGERON SECTION PER USAIR TYPICAL REPAIR 53-10-17.  (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACKS AT FASTENER HOLES LONGERON 23L STATION 180 AND STATION 200.  SPLICED IN SECTION OF LONGERON FROM STATION 160 TO STATION 230 PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN LONGERON 4L AT STATION 180.  SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN LONGERON 12R AT ATTACH FASTENERS STATION 965.  REPLACED SECTION OF LONGERON BY SPLICING PER USAIR TYPICAL REPAIR 53-10-17.  (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK AT FASTENER HOLES STATION 160 LONGERON 25L.  SPLICED IN NEW SECTION OF LONGERON STATION 150 TO 190 PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND .5 INCH CRACK IN FORWARD LEFT OVERWING EMERGENCY EXIT IN DOOR PAN BOTTOM FORWARDNR 5 STOP.  INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03 AND SRM 52-05 FIG 51.  (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN FASTENER HOLES LONGERON 24L STATION 160 AND 200.  REPLACED SECTION OF LONGERON BY SPLICING PER SRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING SIP VISIT INSPECTION, FOUND .375 INCH CRACK RIGHT AIRCONDITION BAY SKIN REF SIP 53-10-19.  INSTALLED DOUBLER REPAIR PER SRM 53-02-18 FIG 12.  (M)


REMARKS:
PIT - DURING SIP VISIT INSPECTION, FOUND 1.5 INCH CRACK RIGHT NOSE LANDING GEAR BAY SKIN STATION 2620 AND 2200,  SIP REF 53-10-19.  STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-02-07.  (M)


REMARKS:
PIT - DURING SIP VISIT INSPECTION, FOUND .375 INCH CRACK UPPER AFT CORNER SKIN OF SERVICE DOOR FRAME AT STATION 4850, REF SIP 53-10-20.  INSTALLED DOUBLER REPAIR PER SRM 53-02-16.  (M)


REMARKS:
PIT - DURING C-6 CHECK INSPECTION, FOUND TWO .25 INCH CRACKS IN LONGERON 16R FRAME 427 AND LONGERON 17R FRAME 408, 427 EDDY CURRENT INSPECTION.  INSTALLED NEW SECTIONS OF LONGERON 16R AND 17R PER SRM 53-02 FIG 2 AND USAIR EA NR 32408.  (M)


REMARKS:
PIT - DURING C-6 CHECK INSPECTION, FOUND THREE .5 INCH CRACKS IN SKIN 7TH, 8TH AND 13TH RIVITS ABOVE STOP TOP FORWARD CORNER FORWARD CARGO DOR FRAME EDDY CURRENT INSPECTION.  INSTALLED DOUBLER REPAIR PER USAIR EA NR 32409 AND SRO 09530117. (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION IN STRINGER CHANNEL ,APPROX 10 INCHES IN LENGTH AND THREE 4 INCHES IN LENGTH, STATION 950-990 STRINGER 27L.  REPLACED STRINGER FROM BS 950-990, REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 706 AT STRINGER 4L TIE CLIP.  MODIFIED PART NR INSTALLED 69-35352-14, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 706 AT STRINGER 6L TIE CLIP.  MODIFIED PART NR INSTALLED, 69-35352-14, REPAIRED PER EO 5393G227.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK APPROXIMATELY 1 INCH AT WEB NOSE GEAR ACTUATOR SUPPORT BRACKET STATION 233.  INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 71 INCHES BY 3 INCHES CORROSION FLOOR BEAM BS 986.5 LBL 25 TO RBL 46.  FILLER T-CAP AND SPLICES, REPAIRED PER SRM 53-10-9 TR 53-10-05C.  CORROSION TASK NR C53-107-02.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 71 INCHES BY 30 INCHES CORROSION FLOOR BEAM BS 947.5 LBL 51 TO RBL 20.REPAIRED FLOOR BEAM, REPAIRED PER TR 53-10-05C, EA 41019.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 14 INCH CORRODED AREA COCKPIT ENTRANCE BS 270.0 4 INCHES LBL - 10 INCHES RBL FLOOR SUPPORT.  INSTALLED Z-ANGLE REPAIR, REPAIRED PER TR 53-20-04.  CORROSION TASK NR C53-107-01.  CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH GOUGES AT BS 360 BL ZERO LBL 12 FLOOR BEAM.  INSTALLED REPAIR STRAPS, REPAIRED PER TR53-10-01A.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT LOWER FAST HOLE OF INNER CHORD ANGLE BS 616 RIGHT FRAME WL 203.  INSTALLED REPAIR ANGLE AND FILLER, REPAIRED PER EA 40996.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CORRODED AREA STRINGER 26R BS 520-540.  INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3.  CORROSION TASK NR C53-202-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION IN STRINGER (APPROX 3 INCHES LONG) STRINGER 26L AT STATION 966.  INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3 FIG 1.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT 2 NUT PLATE HOLES T-CAP, STATION 344 LBL 12 TO RBL 12.  REPLACED T-CAPS, REPAIRED PER TR 53-10-13.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2.  (M)


REMARKS:
DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA ON FRAME AT BS 500 STRINGER 26R.  INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3.  CORROSION TASK NR C53-208-01, CORROSION LEVEL 2.   (M)


REMARKS:
PIT - FL 441 - AFTER TAKEOFF FROM PIT AND REACHING 6000 FEET, CREW COULD NOT PRESSURIZE THE AIRCRAFT.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND A CRIMPED SENSE LINE TO THE PRESSURE CONTROLLER.  LINE WAS REPLACED AND REPOSITIONED SO AS NOT TO CAUSE A CRIMPING CONDITION.  (M)


REMARKS:
YOW - FL 1171 - UPON GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT FAILED TO EXTINGUISH.  NOISE FROM THAT AREA INDICATED THAT THE DOORS WERE NOT CLOSED.  FLIGHT RETURNED TO YOW AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND TWO BOLTS MISSING FROM THE NOSE GEAR SPRAY DEFLECTOR AND INSTALLED REPLACEMENTS.  (M)


REMARKS:
BWI FL 349 - CLIMBING THROUGH 9000 FEET OUT OF BWI, LEFT ENGINE FAILED.  CREW HEARD LOUD BANG (SIMILAR TO A COMPRESSOR)STALL AND ENGINE RPM BEGAN TO DECREASE.  CREW SHUT DOWN ENGINE.  FLIGHT RETURNED TO BWI AND LANDED WITH NO FURTHER INCIDENT.  SET 8 MINUTES.  MAINTENANCE REPLACED THE ENGINE.  (M)


REMARKS:
CAE - FL 256 - EN ROUTE SRQ-CLT, IN THE VICINITY OF CAE, CREW NOTED LOSS OF CABIN PRESSURIZATION.  CREW PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET.  FLIGHT CONTINUED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND AND REPAIRED A SEPARATED DUCT ON THE FORWARD OUTLET ON THE LEFT AIR CONDITIONING PACK. (M)


REMARKS:
BIRD STRIKE ON TAKEOFF ROLL.  DROP IN LEFT ENGINE EPR.  PERFORMED ENGINE INSPECTION FOR BIRD STRIKE PER MM 72-00, PAGE 612.  FOUND DAMAGE TO C1 BLADE.  REMOVED AND REPLACED LEFT ENGINE IAW MM AND JOB CARD J971-00-01.  (M)


REMARKS:
FLT NR 492 - PHL - FOUND OVERWING EXIT LIGHT INOP AT LEFT AISLE SEAT EXIT.  MAINTENANCE REPLACED LIGHT ASSEMBLY.  (M)


REMARKS:
MIA FL - 652 - AFTER TAKEOFF, CREW NOTED OIL PRESSURE RISE ON LEFT ENGINE.  CREW REDUCED POWER ON ENGINE AND NOTED OIL TEMPERATURE RISE.  CREW SECURED THE LEFT ENGINE.  FLIGHT RETURNED TO MIA AND LANDED WITH NO FURTHER INCIDENT.  SET - 12 MINUTES.  MAINTENANCE CLEANED AND SECURED THE CANNON PLUG ON THE NR 1 ENGINE OIL PRESSURE TRANSMITTER AND REPLACED THE OIL TEMPERATURE BULB.  THE NEXT FLIGHT EXPERIENCED SIMILAR READINGS.  MAINTENANCE FOUND THE OIL OVERSERVICED AND DRAINED TO THE PROPER LEVEL.  (M)


REMARKS:
CLT - FLT 1632 - AFTER TAKEOFF, CREW RECEIVED FLAP ASYMMETRY LIGHT UPON RETRACTION OF FLAPS.  NO UNCOMMANDED ROLL WAS EXPERIENCED.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE FLAP INDICATOR.  (M)


REMARKS:
PIT - FL 975 - AFTER TAKEOFF, CREW COULD NOT GET THE FLAPS TO RETRACT.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE ATTACH PIN FOR THE NR 7 FLAP JACKSCREW BACKED OUT, JAMMING THE FLAP TRANSMISSION.  THE PIN WAS REINSTALLED AND SECURED.  (M)


REMARKS:
FLT NR 830 - PHL - AIRCRAFT WOULD NOT PRESSURIZE DUE TO LARGE LEAK ON LEFT SIDE FORWARD ENTRY DOOR.  MAINTENANCE COULD NOT DUPLICATE THE PROBLEM.  FOUND THAT THE FORWARD ENTRY DOOR WARNING LIGHT AND DOOR OPERATED NORMAL.  PRESSURE CHECK WAS GOOD.  (M)


REMARKS:
SAT - FLT 199 - DURING CRUISE, AFT AIRSTAIR LIGHT ILLUMINATED IN COCKPIT.  REMOVED UPLOCK OVERCENTER BUNGEE, CLEANED AND LUBRICATED AND REINSTALLED, CHECKED CABLE RIG, ADJUSTED SWITCH STRIKERS AND PERFORMED UPLATCH MECHANISM CHECK.  OPERATION NORMAL.  CHECK C-4 - 10-25-95 - MCI.


REMARKS:
CMH - FL 868 - AFTER DEPARTURE FROM CMH, NR 2 AND NR 3 TRANSFORMER RECEIVER UNITS FAILED.  FLIGHT RETURNED TO CMH AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND A LOOSE ENGINE GENERATOR FEED HARNESS WIRE.  WIRE 'S' WAS LOOSE AT THE NR 2 GENERATOR.  SECURED WIRE IN TO TERMINAL.  (M)


REMARKS:
FLT NR 311 - PHL - DURING TAKEOFF ROLL, LEFT WING BODY OVERHEAT LIGHT CAME ON.  FLIGHT RETURNED TO FIELD.  REPLACED CONNECTOR D886.  OPS CHECKS SATISFACTORY.  (M)


REMARKS:
FLT NR 1126 - DCA - AIRCRAFT DIVERTED FROM BWO TO DCA DUE TO LOSS OF 'A' SYSTEM HYDRAULIC SYSTEM.  MAINTENANCE FOUND NR1 SPOILER ACTUATOR CRACKED.  REMOVED AND REPLACED NR 1 SPOILER ACTUATOR.  AS A PRECAUTIONARY MEASURE BOTH 'A' SYSTEM HYDRAULIC PUMP WERE CHANGED.  OPS CHECK AND LEAK CHECKS WERE SATISFACTORY.  (M)


REMARKS:
PIT - DURING Q-4/C-6 INSPECTION, FOUND A .25 INCH CRACK AT FASTENER STA 180, BELT FRAME LONGERON 23L.  INSTALLED FILLERAND DOUBLER REPAIR PER SRM 53-03, FIGURE 4.  (X)


REMARKS:
FLT NR 571 - CLT - NR 1 ENGINE WAS SHUT DOWN IN FLIGHT.  LOUD BANG WAS HEARD AND SHORTLY THERE AFTER THE ENGINE FAILED. NO FIRE WARNING OR OTHER INDICATIONS WERE NOTED.  TOTAL SINGLE ENGINE TIME WAS APPROXIMATELY 30 MINUTES.  MAINTENANCE REPLACED NR 1 ENGINE ASSEMBLY PER JOB CARD.  OPERATIONAL CHECK AND LEAK CHECK NORMAL.  (M)


REMARKS:
FLT NR 0731 - PIT - WINDSHIELD CRACKED WHILE CLIMBING THROUGH FL 205.  AIRCRAFT DIVERETED TO PIT.  MAINTENANCE REPLACEDCAPTAINS WINDSHIELD.  (M)


REMARKS:
PHL - FLT 343 - DURING CRUISE, NR 1 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED.  SHUT DOWN NR 1 ENGINE.  REMOVED AND REPLACED ELECTRONIC OVERHEAD ANNUNCIATOR PANEL, MFG P/N 102ADP1-2.  OPERATIONAL CHECK NORMAL.  CHECK C-1D - 6-25-95 - MCI.


REMARKS:
LNK - FLT 235 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, SN 1402, DUE TO OIL LOSS.  FOUND OIL LEAK IN TURBINE AREA.  REPLACED NR 2 ENGINE AND ENGINE OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  9,465 HOURS; 4,437 CYCLES.  CHECK C-1D - 12-23-95 - JFK.


REMARKS:
STL - FLT 712 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 3215, DUE TO OIL FILTER DIFFERENTIAL PRESSURE LIGHT ILLUMINATION.  FOUND OIL LINE, MFG PN 7938314, TO DIFFERENTIAL PRESSURE SWITCH RUPTURED.  REPLACED OIL LINE.  ENGINE OPERATION, LEAK CHECK AND INDICATION WAS NORMAL.  ENGINE TOTAL TIME:  33,308 HOURS; 17,329 CYCLES,  CHECK C-1D - 4-1-95 - MCI.


REMARKS:
STL - FLT 692 - AFTER TAKEOFF FOLLOWING GEAR RETRACTION, THE RT MAIN GEAR UNSAFE LIGHT REMAINED ON.  ADJUSTED RT MAIN GEAR DOOR LATCH ASSY.  PERFORMED GEAR SWING, OPERATION NORMAL.  CHECK C - 2-17-95 - MCI.  (X)


REMARKS:
STL - FLT 85 - DURING CRUISE, NR 2 ENGINE, SN 3240, OIL FILTER CLOG LIGHT ILLUMINATED.  ENGINE WAS SHUT-DOWN AND SUBSEQUENTLY CHANGED.  ENGINE TOTAL TIME 28,723 HOURS; 14,781 TOTAL CYCLES.  CHECK C-2D - 6/5/95 - MCI.


REMARKS:
LNK - FLT 235 - DURING CRUISE SHUT DOWN NR 2 ENGINE, SN 1402, DUE TO OIL LOSS.  FOUND OIL LEAK IN TURBINE AREA.  REPLACED NR 2 ENGINE AND ENGINE OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME:  9,465 HOURS; 4,437 CYCLES.  CHECK C-1D - 12-23-95 - JFK.  FURTHER INVESTIGATION INTO NR 2 ENGINE SHUT-DOWN REVEALED A FAILED LPT 3 SEAL RESULTING IN THE OIL LOSS.  THESEAL HAS BEEN REPLACED AND ENGINE, SN 1402, HAS BEEN RETURNED TO SERVICE.


REMARKS:
SEA - FLT 740 - DURING CLIMB, NR 1 ENGINE, SN 4609, SURGED.  POWER WAS REDUCED TO IDLE.  CHANGED NR 1 ENGINE.  ENGINE TOTAL TIME:  29,752 HOURS; 8,040 CYCLES.  CHECK C-4C - 10-25-95 - LAX.


REMARKS:
DCA - FLT 1126 - EMERGENCY FLOOR LIGHTING BROKEN RIGHT SIDE, ROW 9.  MAINTENANCE FOUND BROKEN WIRE AT RIGHT SIDE, ROW 9.  SPLICED BROKEN WIRE AND RESECURED LIGHT STRIP.  (X)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND KEEL BEAM I/B SPLICE-T CRACKED AT BS 727 LBL 6, WL 154.  REMOVED AND REPLACED WITH NEW PART PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 344 LBL 35 LBL 7.5 BL 0 AND RBL 1.5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827 S9L AT FASTENER HOLE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B/C CHECK, FOUND FWD UPPER AIRSTAIR DOOR STOP AFT T-CAP SECTION CRACKED 1.5 LONG.  REPLACED PER BOEINGSRM.


REMARKS:
AT GATE, FOUND AFT O/B EMERGENCY FLASHLIGHT TEST LIGHT INDICATOR INOP.  REPLACED FLASHLIGHT PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR BEAM STRAP CRACKED AT BS 315 LBL 12.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND Z-ANGLE SUPPORT STRIP AT BS 303.9 CORRODED.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND SEVERAL CRACKS AT BLOW OUT PANEL CUTOUT IN CENTER OF BULKHEAD AT BS 948.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND AFT SERVICE DOOR THRESHOLD Z-ANGLE CORRODED AT BS 947 AND 986.5.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND RT HORIZ STRAP CRACKED AT FWD END AT BS 727 BULKHEAD, AT S22R.  REPLACED PER BOEINGSRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER TO LT FRAME TIE CLIP CRACKED AT I/B END, BS 663.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND UPPER ANGLE WEBS CRACKED EXTENDING FROM CLIP NUT, BS 380 TO 400, BL 0 AND AT BS 482TO 520.  REPLACED ANGLES PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED BETWEEN S10 AND 9R AT BS 291.5.  REPLACED ANGLE PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND U-CHANNEL CRACKED AT BS 727 BULKHEAD AT RBL 3.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN AFT EDGE OF RT W/W STRINGER 18A SHEAR BEAM O/B HOLE.  REPAIRED PER SWA ACO6580-53.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND RT SKATE ANGLE CRACKED AT BS 294.5 RBL 55.  REPAIRED PER TI-A53-0233.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND LT AFT STRINGER 18A CRACKED TO 1ST FASTENER AT BS 727.  REPAIRED PER ACO 6580-53.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SUPPORT ANGLE CRACKED AT BS 540, O/B OF SWING LINK AT BL 0 LEFT SIDE.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND FLOOR BEAM SUPPORT CORRODED AT BS 284 TO 286 LBL 11 WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND FWD ENTRY DOORWAY MOPSILL CORRODED AT BS 316 TO 344 LBL 57 TO 59 WL 208.  REPLACED PERBOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND AFT SERVICE DOORWAY MOPSILL CORRODED AT BS 955 TO 996 RBL 47TO 52 WL 208 TO 209.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND O/B CHORD CRACKED AT BS 1156 WL 240 RBL 18.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND UPPER FLOOR BEAM CORRODED AT BS 1016 RBL 10, 20 TO 34, WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND ANGLE CRACK AT BS 291 RBL 60 WL 248 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND CRACKED DOOR FRAME AT BS 296 RBL 57 WL 216.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND ANGLE CRACKED AT BS 291 RBL 60 WL 248.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND CRACK LOWER FWD DOOR FRAME AT BS 296 RBL 57, WL 216.  REPLACED FRAME PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND FLOOR BEAM CRACKED AT BS 294 RBL 55 WL 208.  REPLACED BEAM PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND TENSION STRAP CRACKED AT BS 326 RBL 31 WL 200.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND CRACKED ANGLE AND STRAP AT FWD ENTRY DOOR STOP FITTINGS NR 9 AND 10 BS 348.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND CRACKED ANGLE ABOVE STRINGER 10L AT BS 302.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND Z-ANGLE CRACKED BS 663, AFT SIDE LBL 6 WL 170 LEFT WHEEL WELL.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500A S24L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND STRINGER CLIPS CRACKED AT BS 520 S19L AND AT BS 400 S27L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND WEB CRACKED AT AFT CARGO DOOR BS 787 TO 794, S 24 TO 25.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD SIDE CHORD CRACKED AT BS 178 WL 195.  INSTALLED REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LOWER FWD CORNER OF AFT GALLEY DOOR CUTOUT CRACKED.  INSTALLED REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED BC4 CHECK, FOUND CRACK IN RT HORIZ STAB LOWER SKIN, 3.75 INCHES O/B OF FUSELAGE AND 2 INCHES FWD OF REAR SPAR.  INSTALLED REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED BC2 CHECK, FOUND FWD CARGO DOOR CRACKED AT LOWER FWD STOP ATTACH POINT.  INSTALLED REPAIR PER SWA RA 1-A52-198.


REMARKS:
DURING SCHEDULED BC1 CHECK, FOUND LOWER AFT KEEL BEAM PANEL CRACKED AT LT SIDE JUST I/B OF RIVET LINE.  INSTALLED REPAIR PER SWA RA 1-A53-1273.


REMARKS:
AFTER T/O, NOTED CAPT L1 WINDOW HAD PRESSURE LEAK.  AIRCRAFT RETURNED TO SAN AND MADE AN UNEVENTFUL LANDING.  RETORQUEDWINDOW SCREWS AND RESEALED PER BOEING M/M.


REMARKS:
AFTER T/O, NOSE GEAR WOULD NOT RETRACT.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  REMOVED AND REPLACEDLOCK ACTUATOR PER PER BOEING M/M.


REMARKS:
IN FLIGHT, CREW REPORTED AN ELECTRICAL BURNING SMELL.  AIRCRAFT DIVERTED TO ABQ AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND C/B FOR GASPER FAN TRIPPED.  RESET AND IT TRIPPED AGAIN.  DEFERRED AND CONTINUED PER MEL 21-26.


REMARKS:
RECYCLED LANDING GEAR DUE TO RIGHT MAIN GEAR RED TRANSIT LIGHT REMAINING ILLUMINATED, THEN GOING GREEN.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT HOU.  REMOVED AND REPLACED A SYSTEM RETURN FILTER AND CHECK VALVE LOCATED DOWNSTREAM OF UPLOCK ACTUATOR.


REMARKS:
CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 5 INCHES BY 4 INCHES AT STATION 356, STRINGER 15L AND 16L.  INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 DETAIL I AND TABLE III FIG 17.  (M)


REMARKS:
PIT - DURING THE C-1 INSPECTION, FOUND TWO CRACKS, 1 INCH AND 2 INCHES AT STATION 1437 LONGERON 4L IN FUSELAGE SKIN.  REMOVED CRACK AND INSTALLED FILLER AND DOUBLER SRM 53-04 FIG NR 27.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH AREA OF CORROSION ON FLOOR BEAM BS 312 8 INCH RBL.  REPLACED T-CAP AND INSTALLED SPLICE ANGLES, REPAIRED PER TR NR 53-10-13.  CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)


REMARKS:
BOS - FL 816, CREW RECEIVED EICAS MESSAGE 'L HYD QTY', QUANTITY READ .45.  FLIGHT RETURNED TO BOS AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE DIFFERENTIAL PRESSURE INDICATOR LEAKING AT THE PRESSURE MODULE AND REPLACED IT.  (M)


REMARKS:
CLT - FLT 1851 - AFTER TAKEOFF FROM CLT, CREW COULD NOT PRESSURIZE AIRCRAFT AND ALSO RECEIVED THE E/E DOOR LIGHT.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE E/E DOOR NOT LATCHED PROPERLY.  THE MECHANISM WAS CHECKED AND FOUND TO BE IN PROPER WORKING ORDER.  AIRCRAFT RELEASED FOR SERVICE.  (M)


REMARKS:
PIT - FL 209 - ON CLIMB-OUT, CAPTAINS WINDSHIELD BEGAN TO ARC AND THEN CRACKED.  FLIGHT RETURNED TO PIT AND LANDED WITHNO FURTHER INCIDENT.  MAINTENANCE REPLACED THE TEMPERATURE CONTROL (P/N 9615059002) UNIT AND THE WINDSHIELD.  (M)


REMARKS:
STRONG BURNING RUBBER SMELL AFTER TAKEOFF (OUT OF ATL).  DECLARED EMERGENCY INBOUND TO CLT.  LANDED UNEVENTFULLY.  INSPECTED BOTH ENGINE INTAKES, GROUND RAN PACKS.  NO SMELLS PRESENT.  FOUND BOTH NOSE TIRES WORN.  REMOVED AND REPLACED BOTHNOSE TIRES.  (M)


REMARKS:
FLT 904 - PIT - AFTER TAKEOFF UNABLE TO CONTROL CABIN ALTITUDE.  WENT TO STANDBY MODE ON CONTROLLER, STILL UNABLE TO CONTROL CABIN.  USING MANUAL AC MODE, REGAINED CABIN CONTROL.  MAINTENANCE VISUALLY INSPECTED EXTERIOR DOORS.  FOUND THE MAIN ENTRANCE DOOR 'FALSE LOCKED'.  CYCLED THE MAIN ENTRANCE DOOR SEVERAL TIMES.  DOOR OPENS AND CLOSED NORMALLY.  AIRCRAFT OK FOR SERVICE.  (M)


REMARKS:
FLT NR 15 - IAD - NOSE GEAR RED UNSAFE LIGHT ON.  NO GREEN LIGHT, FOLLOWED ALL USAIR PILOT HANDBOOK PROCEDURES.  PERFORMED TOWER FLYBY.  DECLARED AN EMERGENCY.  LANDED SAFELY IN IAD.  MAINTENANCE FOUND THE GROUND WIRE FROM SWITCH S845 DOWNLOCK SWITCH PULLED FROM A SPLICE.  REPAIRED SAME.  (M)


REMARKS:
FLT NR 380 - MKE - 1500 FEET AFTER TAKEOFF FROM MKE, LOST CABIN PRESSURE.  NO INDICATION IN COCKPIT, RETURNED TO MKE.  MAINTENANCE FOUND AFT CARGO DOOR OPEN.  REPLACED AFT CARGO DOOR WARNING SENSOR.  OPS CHECKS GOOD.  (M)


REMARKS:
GSO - DURING 'WALK-AROUND', VISUAL INSPECTION FOUND 1.2 INCH CRACK IN FUSELAGE SKIN BS 767 AT STR 18 RIGHT.  INSTALLED DOUBLER, REPAIRED SRM 53-30-3, FIGURE 6.  (X)


REMARKS:
IND - FLT 102 - ATTEMPTED TO USE WEATHER RADAR EN ROUTE.  RADAR INOPERATIVE SHOWING 'NO WXR'.  TEST SHOWED ANTENNA FAULT.  MAINTENANCE FOUND WEATHER RADAR ANTENNA AT FAULT.  REPLACED RADAR ANTENNA.  TEST MADE.  OKAY FOR SERVICE.  (X)


REMARKS:
PHL - FLT 819 - AIRCRAFT RETURNED TO FIELD DUE TO INGESTION OF BIRD IN NR 1 ENGINE.  MAINTENANCE FOUND DAMAGE FROM BIRDINGESTION THAT WAS CAUSE FOR NR 1 ENGINE REPLACEMENT.  (X)


REMARKS:
AIR RETURN DUE TO NR 2 BOOST PUMP BEING INOP AND ON MEL, PRECAUTIONARY RETURN FOR ADDITIONAL FUEL.  AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING, FUEL WAS ADDED AND AIRCRAFT DEPARTED 35 MINUTES LATE FROM ORIGINAL DEPARTURE TIME.


REMARKS:
APU FIRE WARNING ILLUMINATED IN FLIGHT, DISCHARGED FIRE BOTTLE.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION, CONTINUED PER MEL 26-6 AND 7.


REMARKS:
ON APPROACH, CREW WAS UNABLE TO LOWER LEFT MAIN GEAR.  AIRCRAFT LANDED USING NOSE AND RIGHT MAIN GEAR.  AIRCRAFT SUSTAINED DAMAGE TO NUMBER 1 ENGINE.  REPLACED NUMBER 1 ENGINE AND LEFT MAIN GEAR.  INVESTIGATION UNDERWAY.


REMARKS:
IN FLIGHT, EXPERIENCED A-SYSTEM LOP INDICATION.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  REPLACED HYDRAULIC LINE, BOTH A-PUMPS AND FILTERS PER BOEING M/M.


REMARKS:
DURING CLIMBOUT, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT.  AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING.  REPLACED AIR MIXER VALVE PER BOEING M/M.


REMARKS:
DURING CLIMBOUT, CREW EXPERIENCED NUMBER 2 ENGINE OIL QUANTITY/PRESSURE LOSS.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING.  REPLACED NR 2 ENGINE MEC/PUMP GARLOC SEAL PER BOEING M/M.


REMARKS:
AFTER TAKEOFF, LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETACTION.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  ADJUSTED AIR/GROUND SENSOR AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
AFTER TAKEOFF, LEFT MAIN GEAR UPLOCK FAILURE, RED UNSAFE LIGHT REMAINS ILLUMINATED AND GEAR FREE FALLS TO DOWN AND LOCKED POSITION WITH GEAR HANDLE IN OFF.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  REPLACED LEFT GEAR UPLOCK ACTUATOR, MODULE CHECK VALVE AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
AT GATE, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY LIGHT BLINKING.  REPLACED LIGHT PACK ASSEMBLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY ESCAPE SLIDE LIGHTING INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND CABIN OVERWING EMERGENCY EXIT SIGN INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT CENTER CABIN EMERGENCY EXIT WALL LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FWD AND MID CABIN EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACKS PER BOEING M/M.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND AFT RIGHT OVERHEAD EMERGENCY EXIT SIGN INOP.  REPLACED SIGN PER BOEING M/M.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK AND LIGHT ASSEMBLYPER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND FWD LT AND RT EMERGENCY ESCAPE SLIDE LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND AFT CABIN FLOOR LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND CABIN FLOOR LIGHTS INOP AT OVERWING EXIT.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND MID CABIN CEILING LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY  LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK AND CHARGER HOUSING PER BOEING M/M.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK AND HOUSING PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT MID CABIN.  REPAIRED BROKEN WIRES AND REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND LEFT AFT EMERGENCY EXIT LIGHTING INOP.  REPLACED BATTERY PACK BASE PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EXIT SIGNS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR AND GALLEY EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED RON CHECK, FOUND LEFT AFT DOOR EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED A2 CHECK, FOUND OVERWING EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY AND CENTER OVERHEAD EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACKPER BOEING M/M.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND CENTER AISLE AND LT EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK AND CONNECTOR PINS PER BOEING M/M.


REMARKS:
NEWARK TO TAMPA - FLT 25 - NR 3 TIRE FLAT AFTER LANDING.  ALSO, APPARENT DAMAGE TO WHEEL AND BRAKE.  REMOVED AND REPLACED TIRE, BRAKE, AND AXLE SLEEVE.  (X)


REMARKS:
EWR - POST-FLIGHT - OVERHEAD EMERGENCY EXIT LIGHT ROW 11, INOPERATIVE.  REMOVED AND REPLACED BATTERIES.


REMARKS:
EWR - FLT 58 - EMERGENCY EXIT SIGN MISSING AT ROW 7.  FOUND EXIT SIGN ON FLOOR.  REINSTALLED AND SECURED SAME.  (X)


REMARKS:
EWR - POST-FLIGHT - EMERGENCY LIGHT AT ROW 2 NEEDS LENSE AND TO BE SECURED.  REPLACED LENSE AND SECURED EMERGENCY LIGHT.  (X)


REMARKS:
EWR - POST-FLIGHT CHECK - 'E' PATH LIGHT, ROW 17 INOPERATIVE.  RELAMPED SAME.  (X)


REMARKS:
ATL - FLT 22 - POST-FLIGHT CHECK, FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE.  REMOVED AND REPLACED SMOKE DETECTOR.  (X)


REMARKS:
EWR - FLT 81 - POST-FLIGHT, AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE.  REMOVED AND RPELACED POWER PACK.  (X)


REMARKS:
EWR - POST-FLIGHT INSPECTION - EMERGENCY EXIT SIGN AT ROW 17 CEILING INOPERATIVE.  REMOVED AND REPLACED POWER PACK.  (X)


REMARKS:
EWR - POST-FLIGHT - FORWARD EMERGENCY 'E' PATH LIGHT ASSEMBLY NR 3 LIGHT CAPSULE MISSING.  CAPSULE FOUND AND REINSTALLED.  (X)


REMARKS:
ATL - LOG ITEM - 6TH EMERGENCY RED LENSE WOULD NOT STAY DOWN.  REPLACED MODULE.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH BY .25 INCH CORROSION AROUND FASTENER HOLES, FLOOR BEAM STA 312, RBL 21 TO LBL 48.  INSTALLED SPLICE ANGLES AND NEW T-CAP SECTION, REPAIRED PER SRM 53-10-51.  CORROSION TASK NR:  C53-107-02.  CORROSION LEVEL:  2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH BY 1 INCH CORRODED AREA AROUND CLIP NUT HOLES BL ZERO - RBL 45, BS 294.5 FLOOR BEAM UPPER T-CAP, BL ZERO TO RBL 45.  REMOVED CORRODED SECTION FROM LBL 21 TO RT END.  FABRICATED ANDINSTALLED NEW T-CAP SECTION AND SPLICE ANGLES.  REPAIRED PER SRM 53-10-51, FIGURE 205.  CORROSION TASK NR:  C53-107-02. CORROSION LEVEL:  2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH BY 1 INCH CORRODED AREAS AROUND CLIP NUT HOLES RBL 14 TO RBL55, BS 328, FLOOR BEAM UPPER T-CAP.  REMOVED CORRODED SECTION FROM LBL 36 TO RT END.  FABRICATED AND INSTALLED NEW T-CAP SECTION AND SPLICE ANGLES, REPAIRED PER SRM 53-10-51, FIGURE 205.  CORROSION LEVEL:  2.  CORROSION TASK NR:  C53-107-02.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH BY 4 INCH BY 0.016 INCH MAXIMUM WORN AREAS, 2 EACH, BS 887; TOP OF FUSELAGE SKIN UNDER DORSAL FIN.  BLENDED WORN AREAS, CHECKED FOR CRACKS AND SKIN THICKNESS, FABRICATED AND INSTALLED REPAIR DOUBLER PER T/R 53-30-03 AND SRM 53-00-01, FIGURE 202.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK 1156 BULKHEAD.  STOP DRILLED BOTH ENDS OF CRACK, MANUFACTURED, HEAT TREATED, AND INSTALLED REPAIR.  REPAIRED PER EO 5391G3569.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK NR 1 SLAT LOWER SKIN AFT FASTENER ROW ABOVE INBOARD AUXILIARY TRACK.  CUT OUT CRACKED SKIN SECTION AND INSTALLED DOUBLER PER EA 41028.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK NR 1 SLAT LOWER SKIN AFT FASTENER ROW, 3 INCHES FROMINBOARD END.  CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER PER DRAWING 65C30133.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 3 INCH BY 60 INCH COMBINED AREA OF SURFACE CORROSION UPPER T-CAP OF FLOOR BEAM AT STA 986.5 (CABIN).  INSTALLED T-CAP AND REPAIRED ANGLE, REPAIRED PER EA 986.5, SRM 53-00-51.CORROSION TASK NR:  C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREA OF CORROSION, STA 344 FLOOR BEAM UPPER T-CHORD, RBL 9 TO LBL 18, WL 208, AT CLIP NUT HOLES.  REPAIRED BEAM CHORD CUT OUT FROM LBL 33 TO RBL 19 AND SPLICED IN NEW CHORD SECTION PER SRM 53-10-51.  CORROSION TASK NR:  C53-107-02.  CORROSION LEVEL 2.  (X)


REMARKS:
CLT - FLT 1104 - EN ROUTE PIT/MIA, CREW RECEIVED EICAS MESSAGE:  LT BLD DUCT LEAK.  CREW ISOLATED THE LEAK.  CREW THEN EXPERIENCED A RIGHT PACK OVERHEAT AND RECEIVED THE EICAS MESSAGE:  RT PACK OFF.  CREW PERFORMED AN EMERGENCY DESCENT ANDDIVERTED THE FLIGHT TO CLT.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE COULD NOT DUPLICATE THE LT DUCT LEAK PROBLEM.  HOWEVER, THE RAM AIR DOOR INLET ACTUATOR WAS FOUND STUCK IN THE CLOSED POSITION.  THE ACTUATOR WAS REPLACED.  (X)


REMARKS:
ON CLIMB-OUT LEFT GENERATOR FAILED WITH A GOOD CROSSTIE.  RESET THE LT GENERATOR.  GOOD VOLTS AND FREQUENCY.  LT GENERATOR FAILED AGAIN WITH A CROSSTIE LOCKOUT.  APU STARTED TO BACKUP LT SIDE.  APU FAILED.  RT GENERATOR ONLY OPERATION.  DIVERTED TO PHL.  REPLACED LT GENERATOR GCU.  RAN ENGINE AND APPLIED LOAD TO LT GENERATOR.  STARTED APU, OPS CHECKS GOOD.(X)


REMARKS:
RIGHT NACELLE LIGHT INOPERATIVE IN EMERGENCY LIGHTING MODE ONLY.  REPLACED EMERGENCY LIGHT POWER PACK.  (X)


REMARKS:
CLT - FLT 1138 - AFTER TAKEOFF FROM CLT, CREW NOTED A FLAP DISAGREEMENT.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR 4 FLAP SYNCHRONIZER.  (X)


REMARKS:
PIT - FLT 682 - AFTER TAKEOFF AND REACHING 8,000 FEET, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT.  FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPOSITIONED/SECURED LEFT AIR CONDITIONING ACCESS DOOR.


REMARKS:
RIC - FLT 1294 - AFTER TAKEOFF FROM PHL, NOSE LANDING GEAR WOULD NOT RETRACT.  CREW RECYCLED GEAR USING MANUAL OVERRIDETO RETRACT GEAR.  FLIGHT LANDED IN RIC WITHOUT FURTHER INCIDENT.  AIRCRAFT FERRIED TO PIT FOR REPAIR.  MAINTENANCE REPLACED THE LANDING GEAR ANTI-RETRACTION SOLENOID AND ADJUSTED THE LANDING GEAR SELECTOR VALVE.  OPS CHECK GOOD.  (X)


REMARKS:
DEN - FLT 8641 - EN ROUTE SYR TO LAS, CREW NOTED LOSS IN SYSTEM 'A' HYDRAULIC QUANTITY.  CAPTAIN ELECTED TO DIVERT TO DEN.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE REDUCER FITTING ON THE HYDRAULIC TRANSFER VALVE LEAKING AND REPLACED IT.  (X)


REMARKS:
SJU - FLT 1041 - AFTER TAKEOFF FROM STT, CREW RECEIVED RIGHT MLG UNSAFE LIGHT.  TOWER CONFIRMED RIGHT GEAR STLL IN DOWNPOSTION.  FLIGHT DIVERTED TO SJU AND LANDED WITH NO FURTHER INCIDENT.  AIRCRAFT FERRIED TO TPA.  MAINTENANCE CYCLED THEGEAR TWICE AND COULD NOT FIND A DEFECT.  THE 'A' SYSTEM HYDRAULIC FILTERS WERE CHANGED, AND THE RIGHT MLG HYDRAULIC VALVE AND THE RIGHT DOWNLOCK ACTUATOR WERE REPLACED AS A PRECAUTION.  (X)


REMARKS:
CLT - FLT 1139 - RIGHT A/C PACK WAS ON MEL.  AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE AFT OUTFLOW VALVE.  (X)


REMARKS:
CLT - FLT 1527 - AFTER TAKEOFF, CREW RECEIVED RIGHT GENERATOR HIGH OIL TEMPERATURE LIGHT.  APU GENERATOR WAS ON MEL.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT CSD.  (X)


REMARKS:
FLT 1930 - PHL - NR 1 ENG COMPRESSOR STALLED, WOULD NOT SPOOL UP AFTER.  DURING TAXI BACK IDLE EGT KEPT CREEPING UP, SHUT IT DOWN A T530.  AT GATE GROUND PERSONNEL REPORTED TAIL PIPE FIRE.  FIRED BOTH BOTTLES AND EVACUATED AIRCRAFT.  NO FIRE WARNING, FIRE WARNING WAS CHECKED ON SHUTDOWN OK, TURBINE FAILURE CAUSED DAMAGE TO LEFT HORIZONTAL STABILIZER.  MAINTENANCE REPLACED NR 1 ENGINE AND LEFT LEADING EDGE OF HORIZONTAL STABILIZER.  ENGINEERING ANALYSIS FOUND THAT A T3 BLADE FAILED POSSIBLY FROM EXCESSIVE SHROUD WEAR.  (M)


REMARKS:
DFW/DFW - FLT 234 - AIR RETURN, THE RIGHT ENGINE WAS SLOW TO SPOOL UP ON TAKEOFF, DID NOT PRODUCE FULL POWER.  INSPECTED INTAKE, EXHAUST, AND AIR RETURN FOR DAMAGE.  FOUND NORMAL.  RAN ENGINE AND TRIMMED WITHIN PARAMETERS OF TRIM CHART MM 71-00.  (X)


REMARKS:
AT 35,000 FT CABIN ALTITUDE BEGAN TO CLIMB AT 500 FPM TO 1800 FPM.  AIRCRAFT INITIATED DESCENT AND CABIN PRESSURE STABILIZED AT 12.000.  AIRCRAFT CONTINUED AND LANDED AT STL WITHOUT INCIDENT.  RESET PRESSURE CONTROL SYSTEM CIRCUIT BREAKER AND OPERATION CHECKED PER BOEING M/M.


REMARKS:
DURING CLIMBOUT, NUMBER 6 L/E SLAT WOULD NOT RETRACT.  RECYCLED FLAPS, NO HELP.  AIRCRAFT RETURNED TO ONT AND MADE AN UNEVENTFUL LANDING.  REPLACED NR 6 SLAT ACTUATOR AND OPERATION CHECKED PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT THE FOLLOWING LOCATION:  BS 908 S8L, AT BS 867 S20R, AT BS 663.5 S20L AND S10R, AT BS 500A S1, AT BS 500B AND 520 S1, AND AT BS 727A S19R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, S4L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB AND BULKHEAD STIFFENER DAMAGED AT BS 1016 TO 1020.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED AT BS 957 RBL 5 WL 177.5.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 294 LBL 12 LBL 7 BL 0 WL 208 AND AT BS 344 LBL 7 BL 0 RBL 1,9 WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT NR 5 STOP FITTING.  INSTALLED REPAIR DOUBLER PER TRAMCOEWO 96-0105.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB CHAFING DAMAGE AT BS 727 RBL 6 WL 164 UNDER FLAP DRIVE GEARBOX.  INSTALLED REPAIR PER TRAMCO EWO 96-0115.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR TIE STRAP CORRODED AT BS 500 PLUS 4, LBL 24 WL 157.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INBOARD CHORD CRACKED AT BS 639 RBL 64 WL 208.  ALSO, AT BS 637 RBL 70 WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 540 BL 0 TO LBL 25 WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540 BL 0 TO LBL 25.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORROSION AT BS 280 TO 282, RBL 11 WL 208, AT BS 286 AND 291, LBL 11 WL 208, AT BS 314 LBL 11 WL 208, AT BS 276 RBL 11 WL 208 AND AT BS 296 LBL 11.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN S13 AND 14L AND AT BS 1104, 1 INCH ABOVE S17R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND MOPSILL CORRODED FROM BS 316 TO 346 LBL 55 WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294 S4L.  REPLACED FRAME SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 301 S13L.  REPLACED FRAME SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540 BL 0 TO RBL 25 WL 208.  REPLACED SUPPORT PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE VERTICAL AND HORZ STRAPS CRACKED AT BS 1138 ABOVE S12L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE LOWER CHORD CRACKED FROM BS 1154 TO 1156 S5L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND ANGLES CRACKED AT BS 294.5, RBL 55 WL 208 AND AT BS 328 RBL 33 WL 201, AT BS 290 RBL 59WL 240 AND 248 AND AT BS 328 RBL 33 WL 201.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 523 S15R AND AT BS 967 S27L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AND A CHAFED SUPPORT AT BS 280, S5R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178 WL 277 AND AT RBL 11.7 WL 219.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328 WL 173.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LT SIDE FUSELAGE CHORD CRACKED AT BS 178 WL 193.5 TO 196.5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD EMERGENCY LIGHT INOP.  REPLACED LIGHT PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT PRODUCTION SPLICE AT BS 1016 S27R WL 187.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND V-CHANNEL CRACKED AT HORZ  WEB LOWER SURFACE AT BS 1150 RBL 24 IN RT LOWER TORQUE BOX.REPAIRED PER BOEING DRAWING 65-46585 AND SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 26R CORRODED AT BS 977.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FAIL-SAFE CHORD CRACKED AT BS 927 S27R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND AFT GALLEY DOOR UPPER HINGE CUTOUT CRACKED .125.  REPAIRED PER BOEING TYPICAL REPAIR T1-A52-005.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 298 BETWEEN S28R AND L AND AT BS 315 BETWEEN S28L AND R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LBL 45 TO 48 WL 170.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED 3 PLACES AND GOUGED AT BS 1075 TO 1080, BETWEEN S18L AND 16L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED 3 PLACES AFT OF AFT ENTRY DOOR JUST BELOW LIGHT AT BS 996 LEFT SIDE S12.  REPAIRED PER BOEING SRM.


REMARKS:
AT GATE, FOUND EMERGENCY FLASHLIGHT IN FWD GALLEY INOP.  REPLACED PER BOEING M/M.


REMARKS:
AT GATE, FOUND ONE FWD EMERGENCY FLASHLIGHT INOP.  REPLACED BATTERY PER BOEING M/M.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND AIRSTAIR DOORWAY FWD UPPER STOP ATTACH AFT T-CAP CRACKED.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT UPLOCK HOOK.  REPAIRED PER TI NR T1-A52-003.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 800 S15R, AT BS 727B S17R AND AT BS 727B S16L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 400, BELOW SKIN PATCH AND ABOVE S18L.  ALSO, AT BS 1002 S22R, AT BS 250 BETWEEN S21 AND 22R, AT BS 1001 S15 TO 16R, AT BS 1056, 13 INCHES BELOW APU INLET CUTOUT AND AT BS 926, 2 INCHES ABOVE S23R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND AFT DOOR SLIDE LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
TPA/TPA - FLT 462 - AIR RETURN, THE RIGHT AFT OVERWING EXIT DOOR WAS NOT SEATED PROPERLY.  RESEATED DOOR AND PRESSURIZED AIRCRAFT.  NO LEAKS NOTED.  AIRCRAFT OK TO CONTINUE SERVICE.


REMARKS:
RDU - FLT 994 - AT FL 270, SMOKE STARTED TO APPEAR IN COCKPIT CAUSING THE CREW TO DON THE MASKS AND DIVERT TO RDU.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER COMPLICATIONS.  MAINTENANCE REPLACED THE RADAR INDICATOR AND TRANSCEIVER.  (X)


REMARKS:
ONT - DURING CRUISE SMOKE WAS OBSERVED INSIDE REAR GALLEY OVEN.  OVEN WAS OPENED AND A SMOKING PIECE OF PAPER/NAPKIN WAS REMOVED FROM THE OVEN.  MAINTENANCE CLEANED AND CHECKED OVEN FOR PROPER OPERATION.  (M)


REMARKS:
ATL - DURING CLIMB NR 6 LEADING EDGE FLAP INTRANSIT LIGHT ILLUMINATED.  REMOVED AND REPLACED NR 6 LEADING EDGE FLAP SWITCH, MFG P/N 10-60819-8.  OPERATIONAL CHECK NORMAL.


REMARKS:
DURING SPECIAL CHECK, FOUND LOWER HORIZONTAL STABILIZER STRINGER 5L DAMAGED AT STATION 300.  REPAIRED PER SRM 55-10-03,FIGURE 101, DETAIL NR 1 AND TWA STANDARD PRACTICES.


REMARKS:
DURING CLIMB NR 1 ENGINE, S/N 3810, WAS SHUT DOWN DUE TO OIL STRAINER CLOG LIGHT ILLUMINATION.  ENGINE TOTAL TIME 39,869, TOTAL CYCLES 46,939.


REMARKS:
DURING OP-16, FOUND A 6 INCH CRACK IN RIGHT INBOARD FOREFLAP INBOARD RIB, AND FOUND CRACK IN ANGLE.  REPAIRED BY REPLACING RIB AND ANGLE PER SRM 50-10-01 AND TWA STANDARD PRACTICES.


REMARKS:
DURING C-CHECK, FOUND CRACK ON FORWARD TANG OF HAT SECTION, RIGHT WING WS 601.5.  REPAIRED PER SSRM 57-20-201 AND TWA STANDARD PRACTICES.  (M)


REMARKS:
DURING C-CHECK, FOUND TANG BROKEN OFF, AFT SIDE OF HAT SECTION, WING STATION 656.5.  REPAIRED PER SRM 57-20-201, FIGURE214.  (M)


REMARKS:
DURING C-CHECK, FOUND DOUBLER CRACKED ON WING RIB AT STATION 686.5 AND STRINGER 1.  REPAIRED BY REPLACING DOUBLER PER SRM 57-10-5.


REMARKS:
DURING OP-16, FOUND THREE CRACKS OVER ONE INCH LONG ON LOWER FORWARD CORNER OF NR 32 DOOR OUTER SKIN AND TWO CRACKS ON INNER SKIN.  INSTALLED DOUBLER REPAIR PER SSRM 53-30-303 AND TWA STANDARD PRACTICES.  (M)


REMARKS:
DURING SPECIAL CHECK, FOUND CRACK IN LOWER HORIZONTAL STABILIZER STRINGER 6L, STATION 290.  REPAIRED PER SRM 55-10-03, FIGURE 101, DETAIL NR 1 AND TWA STANDARD PRACTICES.


REMARKS:
DURING SPECIAL CHECK, FOUND FUSELAGE STRINGERS 16, 17L, 18L AND 19L, DENTED AND CRACKED, FS 1582 TO FS 1660.  REPAIRED PER ARA 9958 AND SRM 53-00-03, PAGE 201, FIGURE 201.  (M)


REMARKS:
DURING SPECIAL CHECK, FOUND LOWER HORIZONTAL STABILIZER DAMAGE AT STATION 304, STRINGER 7L.  REPAIRED PER SRM 55-10-03,PAGE 101, DETAIL NR 1 AND TWA STANDARD PRACTICES.


REMARKS:
DURING CRUISE GEAR DOOR LIGHTS ILLUMINATED.  CHECKED GEAR DOOR SENSOR GAPS, FOUND WITHIN LIMITS AND RESEATED PROXIMITY CARDS.  GROUND CHECKS NORMAL.


REMARKS:
DURING C-CHECK, FOUND .5 INCH CRACKS AT UPPER AND LOWER LEGS OF LONGERON 5L, STATION 699.  REPAIRED PER SRM 53-02, FIGURE 2.


REMARKS:
DURING C-CHECK, FOUND .5 INCH CRACKS IN UPPER AND LOWER LEGS OF LONGERON 6L, STATION 688.  REPAIRED PER SRM 53-02, FIGURE 2.  (M)


REMARKS:
DURING OP-15, FOUND CORROSION AROUND TWO ADJACENT NUT PLATES UPPER CAP, FLOORBEAM STATION 980, INBOARD OF CUSP ANGLE.  REMOVED CORRODED AREAS AND INSTALLED REPAIR PER SRM 53-05, FIGURE 20A.


REMARKS:
DURING OP-15, FOUND CORROSION AT LONGERON SPLICE OF LONGERON 30, STATION 400.  REPAIRED BY INSTALLING NEW SECTION OF LONGERON PER ARA 10074 AND SRM 53-07, FIGURE 14.  (M)


REMARKS:
DURING OP-15, FOUND A ONE INCH CRACK IN E/E COMPARTMENT, STATION 160, LONGERON 25L, AT ATTACH POINT.  REPAIRED PER SRM 53-02, PAGE 2A, FIGURE 2.


REMARKS:
DURING OP-15, FOUND A .75 INCH CRACK IN LONGERON 4R, STATION 617.  REPAIRED BY INSTALLING NEW SECTION OF LONGERON PER SRM 53-04.


REMARKS:
DURING OP-15, FOUND TWO CRACKS IN LONGERON 5R, .5 INCH AT STATION 699, AND .25 INCH AT STATION 737.  REPAIRED BOTH PER SRM 53-02, FIGURE 2.


REMARKS:
AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED.  RECYCLE LANDING GEAR, FOUND INTERNAL MALFUNCTION IN LANDING GEAR WARNING PROXIMITY COMPUTER, MFG P/N 8-336-05.  REPLACED PROXIMITY COMPUTER AND LANDING GEAR WARNING SYSTEM CHECKED NORMAL.


REMARKS:
DURING OP-15, FOUND A .75 INCH CRACK AT BELT RING ATTACH POINT OF LONGERON 23L, STATION 200.  REPAIRED BY INSTALLING NEW LONGERON PER SRM 53-02, FIGURE 2.


REMARKS:
DURING OP-15, FOUND .75 INCH CRACK IN LONGERON 22L AND CORROSION AT STATION 190.  REPAIRED BY INSTALLING NEW LONGERON AND HI-LOKS IN LONGERON 22L PER SRM 53-02, FIGURE 2.


REMARKS:
DURING OP-15, FOUND LONGERON 30 CRACKED APPROXIMATELY 10 INCHES FROM STATION 794, AFT TO SPLICE.  REPLACED LONGERON 30 FROM STATION 756 TO 813 PER SRM 51-30 AND TWA STANDARD PRACTICES.


REMARKS:
DURING OP-15, FOUND A SIX INCH CRACK AT LOWER OUTBOARD CORNER OF RIGHT FORWARD ENGINE MOUNT BULKHEAD WEB, STATION 965.REPAIRED PER SRM 53-03, FIGURE 21.


REMARKS:
DURING OP-15, FOUND .75 INCH CRACK IN LEFT PYLON ATTACHED ANGLE VERTICAL LEG TOP SIDE, STATION 980.  STOP DRILLED CRACKAND REPAIRED PER SRM 54-04.


REMARKS:
DURING CRUISE EGRESS LIGHTING IN AFT CABIN WOULD ILLUMINATE.  CYCLED SWITCH OFF AND BACK TO ARMED.  FOUND CONNECTOR AT POWER SUPPLY, NOT FIRMLY CONNECTED.  RESEATED CONNECTOR AT POWER SUPPLY AND EGRESS LIGHTING SYSTEM OPERATION CHECK NORMAL.


REMARKS:
DURING CRUISE, EGRESS LIGHT AT SEAT ROW 15 THROUGH 19 ILLUMINATED.  FOUND BATTERY PACK WEAK.  REPLACED BATTERY PACK ANDEGRESS LIGHTS OPERATION CHECKED NORMAL.


REMARKS:
DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DID NOT EXTEND.  CYCLED LANDING GEAR.  LUBRICATED NOSE LANDING GEAR TRUNNIONS AND DRAG BRACE.  NOSE LANDING GEAR CHECKED NORMAL.


REMARKS:
DURING CRUISE THE EMERGENCY EGRESS LIGHTS ILLUMINATED.  REMOVED AND REPLACED THE POWER SUPPLY, MFG P/N 5822-2.  OPERATIONAL CHECK NORMAL.


REMARKS:
DURNG DESCENT, SMOKE FROM AN UNDETERMINED SOURCE APPEARED IN THE COCKPIT AND CABIN.  PERFORMED MD9-21-02 AIR CONDITIONING DUCT OIL CONTAMINATION CHECK, AND MD9-49-04 APU AND ECS PERFORMANCE CHECK, ALL CHECKS NORMAL.


REMARKS:
DURING A PREFLIGHT CHECK OF THE EMERGENCY EGRESS LIGHTS, THEY REMAINED ILLUMINATE.  REMOVED AND REPLACED EGRESS POWER SUPPLY, MFG P/N 5322-2.  OPERATIONAL CHECK NORMAL.


REMARKS:
DURING TAKEOFF LEFT MAIN LANDING GEAR ACTUATOR TOP SIDE HYDRAULIC LINE FAILED.  REMOVED AND REPLACED HYDRAULIC LINE, MFG P/N AE100880912030.  PRESSURIZED SYSTEM, OPERATIONAL CHECK OK.


REMARKS:
DURING DESCENT NR 1 ENGINE OIL SCREEN CLOG LIGHT ILLUMINATED.  REMOVED AND REPLACE ENGINE OIL FILTER GYPASS SWITCH, MFGP/N 42D109-1A.  ALL FILTERS CHECKED OK.  OPERATIONAL CHECK OK.


REMARKS:
DURING OP-16, FOUND A 23 INCH CRACK AT RIGHT WING TOP, IN LEADING EDGE PANEL, AFT OF CENTER OF NR 18 LEADING EDGE FLAP. REPAIRED PER SRM 51-40-12 AND TWA STANDARD PRACTICES.


REMARKS:
CLT - INSPECTION VISUALLY, FOUND A LEVEL 2 CORROSION LOCATED ENTIRE LENGTH, TOP AND BOTTOM AT S46L TO S46R FLOORBEAM AREA.  REPLACED UPPER FLOORBEAM T-CAP CAP AS PER TYPICAL REPAIR 53-10-05.  (M)


REMARKS:
INT - DURING 'DROP-IN' CHECK VISUAL PCI INSPECTION, FOUND 2.2 INCH CRACK, STATION 706 STRINGER 18A RIGHT.  INSTALLED REPAIR, REPAIRED PER EA 41018.  (M)


REMARKS:
PIT - DURING C-4 CHECK INSPECTION, FOUND A 1.25 INCH AND 3 INCH CRACK IN REAR PRESSURE BULKHEAD Z-63 LEFT SIDE OF DOOR FRAME AT STATION 996.  CUT OUT CRACKED AREAS AND INSTALLED FILLER AND DOUBLER PER USAIR EA NR 32410A.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK FRAME CHORD ANGLE STATION FRAME 727, BETWEEN STRINGER16R AND STRINGER 17R.  REMOVED DAMAGED AREA MANUFACTURED HEAT TREATED AND INSTALLED REPAIR.  REPAIRED PER SRM 51-40-4 FIG 1 SRM 20-30-06.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT TWO FASTENERS AT BS 727, STRINGER 18 IN FRAME CHORD ANGLE.  REPLACED SECTION OF CHORD ANGLE, REPAIRED PER EO 5394G068.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK DOOR FRAME SKIN BS 349, STRINGER 15L.  INSTALLED DOUBLER,REPAIRED PER SRM 51-40-2, FIG 1.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STABILIZER STRAP (FLOOR BEAM BOTTOM) BS 344, RBL 32.  INSTALLED DOUBLER, REPAIRED PER SRM 53-10-9.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STABILIZER STRAP (BOTTOM OF FLOOR BEAM) BS 312, RBL 45.  INSTALLED DOUBLER, REPAIRED PER SRM 53-10-9.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 CRACK STRINGER TIE CLIP STATION 360, STRINGER 4L.  FABRICATED AND INSTALLED NEW TIE CLIP, REPAIRED PER SRM 57-10-1.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK WEB OF BUILD UP STRINGER BS 294, STRINGER 7L.  FABRICATED AND INSTALLED WEB PER BAC PRINT NR 65-27684 SRM 51-30-2, PAGE 5 AND SRM 53-10-1 NOTED.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK EXTERIOR SKIN AND BEAR STRAP BS 328 WL 210 RIGHT SIDE LOWER AFT CORNER OF DOOR CUTOUT.  INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 26.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH LONG STATION 350 AT STRINGER 17L FRAME.  REMOVED DAMAGED AREA FABRICATED REPAIR AND REPAIRED PER SRM 20-30-06 SRM 51-40-4.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 294 AND STRINGER 7 LEFT.  REMOVED CRACK SECTION OF STRINGER WEB, FABRICATED NEW SECTION AND INSTALLED PER SRM.  REPAIRED PER BOEING DRAWING 65-17684 AND SRM 53-10-1 AND 51-30-2 PAGE 5.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT WEB, BS 350 STRINGER 16L.  FABRICATED AND INSTALLED REPLACEMENT WEB.  REPAIRED PER BOEING DRAWING 65-17685.  (M)


REMARKS:
ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 69 INCH CORROSION STRINGER 27L, BS 947 TO 1016.  INSTALLED STRINGER/DOUBLERS.  REPAIRED PER SRM 53-10-3, DETAIL VI.  (M)


REMARKS:
PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND STATION 1380 FORWARD SIDE FRAME CHAFED BETWEEN LONGERON 4L AND5L.  ROUTED OUT CHAFED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2 SHEET 3 AND SRM 53-14-1.  (M)


REMARKS:
PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND 3.5 INCH CRACK RIGHT SIDE DRAG ANGLE LOWER VERT STABILIZER.  INSTALLED DOUBLER REPAIR PER USAIR EA 32426.  (M)


REMARKS:
PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND 3.5 INCH CRACK LEFT SIDE AFT DRAG ANGLE AT LOWER VERT STAB.  INSTALLED DOUBLER REPAIR PER USAIR EA 32425.  (M)


REMARKS:
PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED IN CARGO FLOOR SUPPORT STATION 541, BETWEEN LONGERON 28L AND 28R.  MANU SUPPORT USING 7075-T6 PER DACO DRAWING NR 5936592.  (M)


REMARKS:
PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND A 1.75 INCH CRACK IN SKIN PANEL JUST OUTBOARD OF REAR SPAR STATION XH=7.234 RIGHT SIDE HORIZONTAL STAB.  REMOVED DAMAGE AND INSTALLED FILLER REPAIR PER SR09550010-3 AND USAIR EO NR 5592X156.  (M)


REMARKS:
PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON LONGERON 29R STATION 1211-1250.  CORROSION TASK NR C57-53300.  INSTALLED NEW SECTION OF LONGERON PER USAIR EA 32559.  (M)


REMARKS:
PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED SECTION OF LONGERON 28L STATION 1211-1250.  CORROSION TASK NR C57-53300.  SPLICED IN NEW SECTION OF LONGERON PER USAIR EA 32559.  (M)


REMARKS:
PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND APPROXIMATELY 38 INCHES OF CORROSION IN FWD CARGO DOOR STATION389 THROUGH STATION 427 DOOR PAN.  INSTALLED NEW SECTION OF PAN PER SRM 53-05 FIG 44.  (M)


REMARKS:
SJU - FL 1970 - AFTER TAKEOFF, CREW REPORTED A PNEUMATIC LEAK ON THE LEFT ENGINE (EICAS MESSAGE - 'L ENG OVHT').  FLIGHT RETURNED TO SJU.  MAINTENANCE CONFIRMED A BLEED PROBLEM AND TIGHTENED A CLAMP ON THE LEFT ENGINE DUCTING.  FLIGHT TOOKOFF AND RETURNED A SECOND TIME FOR THE SAME PROBLEM.  MAINTENANCE FOUND THE LEFT ENGINE EXPANSION JOINT CRACKED AND REPLACED IT.  (M)


REMARKS:
ORD - DURING GEAR RETRACTION, RIGHT GEAR LIGHT STAYED ON.  VISUAL CHECK OF ALIGNMENT STRIPES INDICATED GEAR WAS NOT DOWN AND LOCKED.  NEITHER GEAR RECYCLE NOR MANUAL EXTENSION ALIGNED STRIPES.  AIRCRAFT LANDED WITHOUT INCIDENT.  REMOVED AND REPLACED BROKEN DOWNLOCK PUSHROD, MFG P/N 69-15747-2.  PERFORMED BOTH NORMAL AND MANUAL GEAR SWINGS, BOTH CHECKED NORMAL.  (M)


REMARKS:
JFK - DURING TAKEOFF THE CENTRAL AIR DATA COMPUTER FAILED.  AIRCRAFT RETURNED TO JFK.  REMOVED AND REPLACED THE CADC, MFG P/N HG280D80.  SELF TEST AND LEAK CHECK NORMAL.  (M)


REMARKS:
JFK - DURING CRUISE, THE NR 2 CONSTANT SPEED DRIVE FAILED.  REMOVED AND REPLACED NR 2 CSD.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
ON FLT 235, ATL-ATL, GATE RETURN, THE AFT CARGO DOOR LIGHT CAME ON TAKEOFF ROLL.  ADJUSTED SWITCH PER 52-30, OPS CHECK NORMAL.  (M)


REMARKS:
ON FLT 236, DFW-ATL, DIVERTED TO MSY WITH THE LEFT AC BUS INOP.  FOUND THE LEFT GENERATOR CONTROL PANEL LOOSE IN THE RACK, SECURED PANEL, RAN ENGINES WITH AC LOAD, OPS CHECKED NORMAL.


REMARKS:
FLT 11 - EWR-MCO - AFTER TAKEOFF, UNABLE TO MAINTAIN PRESSURIZATION, MANUAL CONTROLLER NO HELP.  FOUND LEFT OUTFLOW VALVE STICKING AND DUMPING CABIN AIR.  REPLACED SAME.  (M)


REMARKS:
LEX - FLT 1147 - AT FL 260, CREW NOTICED AFT CARGO DOOR WARNING LIGHT ILLUMINATED.  THE CREW DESCENDED TO 10,000 FEET, DEPRESSURIZED THE AIRCRAFT AND DIVERTED TO LEX.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT.  MAINTENANCE ACCOMPLISHED FUNCTIONAL TEST OF ALL THREE CARGO DOORS PER MAINTENANCE MANUAL 52-70-2.  (M)


REMARKS:
PIT - EMERGENCY LIGHTS NOT WORKING PROPERLY.  MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK.  (M)


REMARKS:
AFTER T/O, L/E SLATS EXTENDED UNCOMMANDED.  AIRCRAFT RETURNED TO FLL AND MADE AN UNEVENTFUL LANDING.  REPLACED HYDRAULIC FUSE PER BOEING M/M.


REMARKS:
SLC - DURING TAKEOFF NR 2 ENGINE, S/N 1548, SUFFERED A TURBINE FAILURE.  ENGINE TOTAL TIME 33,348.  TOTAL CYCLES 21,618.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, S4R AND S4L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKS AT BS 639, RBL 65, WL 221 AND AT BS 616, RBL 65, WL 221.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM TENSION STRAP CRACKED AT BS 315, WL 200, RBL 30.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORTS CORRODED AT BETWEEN BS 277 AND BS 294.  ALSO, BETWEEN BS 294 AND BS 312,LBL 12.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND MOP SILL CORRODED BETWEEN BS 312 AND BS 322, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF FORWARD GALLEY DOOR CUTOUT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND RT AFT SERVICE DOOR EMERGENCY EXIT LIGHTS INOPERATIVE.  REPLACED BATTERY PACK HOUSING PER BOEING M/M.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN DENTED 15 INCHES AFT OF AFT ENTRY DOOR, 26 INCHES BELOW EMERGENCY EXIT LIGHT.  REPAIRED PER BOEING SRM.


REMARKS:
ON APPROACH, NOSE GEAR DID NOT EXTEND, SLOWED AND RETRIED.  NOSE GEAR EXTENDED.  AIRCRAFT LANDED NORMALLY IN PHX.  REPLACED UPLOCK ACTUATOR, NOSE GEAR SEQUENCING VALVE AND OPS CHECKED PER BOEING M/M.


REMARKS:
DURING SCHEDULED RON, FOUND EMERGENCY LIGHTS INOPERATIVE FROM BS 500 TO BS 616.  REPAIRED SHORTED WIRE OVER LEFT EMERGENCY EXIT AND REPLACED M1134 DUE TO BLOWN FUSE.  OPS CHECKED NORMAL PER BOEING M/M.


REMARKS:
FOUND AFT LOWER EMERGENCY FLASHLIGHT INOPERATIVE.  REPLACED FLASHLIGHT BATTERY PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND MULTIPLE DENTS AND CRACKS IN FUSELAGE FRAME AT BS 481, LBL 35, LBL 59, WL 162-182.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND RT WING SKIN CRACKED AT NR 5 L/E SLAT ACTUATOR CUT-OUT.  REPAIRED PER BOEING DRAWING 65C30133.


REMARKS:
ON TAKEOFF, AIRCRAFT HAD LIGHTNING STRIKE TO RADOME AREA.  ALL SYSTEMS FUNCTIONING NORMALLY.  AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING.  PERFORMED LIGHTNING STRIKE INSPECTION AND REPLACED RADOME PER BOEING M/M.


REMARKS:
ON LANDING ROLL, AIRCRAFT LEFT GEAR LEFT RUNWAY.  AIRCRAFT RETURNED TO RUNWAY AND CONTINUED TO GATE.  PERFORMED GEAR SIDELOAD INSPECTION, REPLACED NR 2 ENGINE DUE TO FOD DAMAGE, REPAIRED 3 SKIN AREAS FOR GOUGES, AND RT I/B AFT FLAP.  REPLACED ONE AND REPAIRED ANOTHER NR 2 ENGINE REVERSER CASCADES.  TEST HOPPED AIRCRAFT.  REPLACED ALL GEAR WHEEL/TIRE ASSEMBLIES.  ALL WORK PER BOEING M/M AND SRM.


REMARKS:
AFTER TAKEOFF, NR 5 L/E SLAT WOULD NOT RETRACT.  AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING.  REPLACED SLAT ACTUATOR PER BOEING M/M.


REMARKS:
FOUND EXIT FLOOR LIGHTING INOPERATIVE IN ONE AREA.  REPAIRED TRACK WIRING PER BOEING M/M.


REMARKS:
FOUND CABIN EMERGENCY FLOOR LIGHTING INOPERATIVE AT MID-CABIN AREA.  REPAIRED TRACK WIRING PER BOEING M/M.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED AT WL 213, RBL 6.7.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED 3 PLACES AT WL 201, WL 199 AND WL 198, RBL 4.7.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED 3 PLACES AT WL 213, LBL 4.7 AND LBL 6.7, WL 209.5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND INTERCOSTAL TO FRAME ANGLE CRACKED AT BS 380, LBL 24, WL 155.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, S19L, WL 192.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN DENTED AT BS 294.5 TO BS 312, BETWEEN S20 AMD 21R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE OUTER SKIN CRACKED AT BS 328, WL 211, RBL 65.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND WEB CRACKED AT BS 639, RBL 66, WL 221.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CREASED AT BS 460 TO BS 480, RBL 1 TO RBL 4, WL 149.  REPAIRED PER BOEING SRM.


REMARKS:
CABIN PRESSURIZATION FAILED AT FL 350 (1,000-1,500 FEET FPM CABIN CLIMB), CABIN PRESSURE MASTER WARNING ILLUMINATED ANDALL MASKS DROPPED.  RESECURED DUCT AFT SIDE OF LEFT WATER SEPARATOR.  PRESSURIZATION CHECK OK PER MM 21-30 SYSTEM.  OPSCHECK GOOD, SECURED MASKS.


REMARKS:
ABORTED TAKEOFF, NR 1 ENGINE WOULD NOT MAKE TARGET EPR (1.95) N1 INDICATED 847 DEGREES WITH LEFT THROTTLE ALL THE WAY TO STOP (N2, FUEL FLOW, EGT APPEARED NORMAL ON NR 1 ENGINE).  EPR WOULD ONLY MAKE 1.84 THROTTLE FULL FORWARD.  TRIMMED NR1 ENGINE TO MM REF 71-00, PAGE 549, FIGURE 508, SHEET 11.


REMARKS:
WHILE SITTING AT GATE IN MCO MAKING PA ANNOUNCEMENTS, THE CIRCUIT BREAKER'S FOR PA INTERPHONE, 'NO SMOKING' AND 'FASTENSEAT BELT' LIGHTED SIGNS TRIPPED.  SMOKE SMELL IN THE CABIN.  ACCOMPLISHED VALUJET AIRLINES EO DC-9-3396005, SEAT BELT,NO SMOKING SIGN, PASSENGER WARNING SYSTEM WIRING.


REMARKS:
SEA - FLT 350 - DURING THE TAKEOFF ROLL AT APPROXIMATELY 40 KNOTS, THE 'WHEEL NOT TURNING' LIGHT ILLUMINATED.  THE TAKEOFF WAS ABORTED.  REINSTALLED TRANSDUCER PINS.  OPERATIONAL CHECK AND BITE CHECK NORMAL.  CHECK C-1D - 11/3/95 - JFK.


REMARKS:
MCO - FLT 2208 - AISLE EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE FOUND FUSE BLOWN IN POWER SUPPLY.  REPLACED FUSE, LIGHT OPS CHECK SATISFACTORY.  (X)


REMARKS:
STL - FLT 463 - DURING CRUISE, AIRCRAFT CABIN PRESSURIZATION BLED OFF.  REMOVED AND REPLACED NR 2 PACK FLOW CONTROL VALVE, MFG PN 396130-1-1.  OPERATIONAL CHECK AND LEAK CHECK NORMAL.  CHECK C-1D - 5-18-95 - MCI.


REMARKS:
DURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IN LONGERON 6L, STA 639.  REPAIRED PER SRM 53-02, PAGE 2A, FIGURE 2.  AIRCRAFT TOTAL TIME:   68,821 HOURS.  CYCLES, 8,390.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND RT WING LOWER SKIN CRACKED JUST I/B OF NUMBER 6 AUX TRACK.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND CHANNEL CRACKED ABOVE VHF ANTENNA, IN FWD CARGO BIN.  REPLACED CHANNEL PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND RIGHT TRANSITION ANGLE CRACKED AT BS 787.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 747 LEFT SIDE, AT 727B, 747 AND 500 RIGHT SIDE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT A/C GROUND SERVICING CUTOUT, FWD LT CORNER.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SC CHECK, FOUND RT FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 474, S22 TO 23L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 455, S17 TO 18L AND AT BS 500A PLUS 15 BETWEEN S14 AND 15L.REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE DAMAGED AT BS 277, BETWEEN S23 AND 24R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED AT RBL 5.7, WL 193 TO 202, AT LBL 5.7, WL 195 TO 202, AT RBL10 TO 5.7 AND LBL 5.5, WL 207 TO 214.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AROUND GROUNDING WIRES AT BS 294, LBL 56, WL 219.  REPAIRED PERBOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AFT SIDE AT RBL 1, WL 189.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND UPPER SIDE OF FRAME CORRODED AT AFT SIDE OF LOWER NOSE COMPARTMENT, BS 219 WL 165 LBL 7.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 729, BL 0, WL 164.  REPLACED CRACKED SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 827, LBL 32, WL 163.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT FASTENER HOLE BS 540, LBL 1, WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663 S10L ,S10R AND AT BS 867 S9L.  REPLACED PER BOEING SRM.


REMARKS:
FOUND EMERGENCY TRACK LIGHTING AT MID CABIN INOP.  REPAIRED WIRING PER BOEING M/M.


REMARKS:
DURING 1/4 D-CHECK, FOUND RT TRANSITION ANGLE CORRODED AT BS 767 TO 793.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 800, S15R AND AT BS 727B, S17R AND S16L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING WALKAROUND CHECK, FOUND SCRAPED AREA ON LOWER FUSELAGE SKIN NEAR MAIN OUTFLOW VALVE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND CRACKED SKATE ANGLE AT BS 570, WL 171, LBL 43 TO 60.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FWD GALLEY DOOR UPPER HINGE CUTOUT OUTER SKIN CRACKED AT UPPER OUTER EDGE.  REPAIRED PER SWA ACO 3189-52.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE FRAME DENTED AT BS 727E, S25R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND WEB CRACKED AT BS 178, BL 0, WL 188.1.  REPAIRED PER TRAMCO EWO 96-0228.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, LBL 5.5, WL 184.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, RBL 36, WL 162.  REPAIRED PER TRAMCO EWO 96-0229.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CREASE AT BS 807, BL 0, WL 148.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FWD SERV DOOR, LWR FWD FRAME CRACKED AT BS 295, RBL 56, WL 209.  REPLACED FRAME PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND AFT CARGO BULKHEAD SUPPORT BRACKET CRACKED AT BS 727 PLUS 4, BL 0, WL 160.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 947 TO 957, BETWEEN S18 AND 19L.  REPAIRED PER BOEING SRM.


REMARKS:
ON FLT NR 270, ATL-ATL, AIR RETURN FOR MTC CONVENIENCE, THE NR 1 VHF RADIO WOULD NOT TRANSMIT OR RECEIVE ON MOST FREQUENCIES.  THE NR 2 AZIMUTH AND RMI NEEDLE INOP.  REMOVED AND REPLACED NR 1 VHF CONTROL PANEL PER 23-10, OPS CHECK GOOD, AND REMOVED AND REPLACED NR 2 NAV/COMM PANEL PER 34-51, OPS CHECK GOOD.


REMARKS:
FLT 520 - ATL-ATL, AIR RETURN FOR MTC CONVENIENCE, THE RIGHT CSD ROSE INTO THE CAUTION RANGE, APPROACHING THE RED LINE. LEFT GENERATOR PREVIOUSLY ON MEL.  CLEARED MEL ON LEFT GENERATOR BY ADJUSTING CSD FREQUENCY PER 24-10 AND ASSIGNED MELTO RIGHT CSD.  (M)


REMARKS:
DURING TEST FLIGHT FOR NOSE GEAR INDICATION PROBLEMS, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON.  GEAR POSITION VISUALLYVERIFIED.  MAINTENANCE FOUND BROKEN WIRE ON RIGHT GEAR PROXIMITY SWITCH.  MAINTENANCE REPAIRED WIRING SYSTEM GROUND CHECK GOOD.  (M)


REMARKS:
FLT NR 383 - BOS-BOS, AIR RETURN DUE TO RIGHT GEN FLUCTUATES ON AND OFF AFTER TAKEOFF.  APU PREVIOUSLY ON MEL.  ASSIGNED MEL TO RIGHT GEN AND CLEARED MEL ON APU.  REMOVED AND REPLACED NR 2 CSD PER VJ MM 24-10-1.  (M)


REMARKS:
ON FLT 555 - MDW-MDW- ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN ON TAKEOFF ROLL.  ADJUSTED FLAP POSITION SWITCH AND TAKEOFF WARNING SYSTEM.  OPS CHECK NORMAL, IAW MM 27-55.  (M)


REMARKS:
ON FLT 498 - ATL-ATL, AIR RETURN, THE NR 2 EGT WENT INOP.  REMOVED AND REPLACED NR 2 EGT INDICATOR PER VJ MM 77-20-00, OPS CHECK GOOD.  (M)


REMARKS:
FLT NR 396 - PBI-BOS, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION.  EXECUTED MISSED APPROACH, NOSE LIGHT ILLUMINATED DURING CLIMB AND LANDED NORMALLY.  CHECKED NOSE GEAR ASSEMBLY SWITCH, NO DEFECTS FOUND.


REMARKS:
FLT 471 - IAD-MSY - DIVERTED TO ATL, BOTH ATC TRANSPONDERS BECAME INOP.  REMOVED AND REPLACED NR 1 ALTIMETER AND REPAIRED BROKEN WIRE ON NR 2 TRANSPONDER.  ASSIGNED MEL TO NR 1 TRANSPONDER READING LOW.


REMARKS:
ON FLT 229 - ATL-ATL, AIR RETURN, CAPTAINS WINDSHIELD SHATTERED (OUTER PANE) NO IMPACT.  REMOVED AND REPLACED CAPTAINS SIDE WINDSHIELD IAW 56-10-2.  NO DEFECTS NOTED.


REMARKS:
FLT 248 - ATL-ATL, AIR RETURN, DURING CLIMB-OUT OF ATL IN MANUAL PRESSURE AND CABIN AT 5000 FEET CLIMBING AT 500 FPM NR1 FLIGHT ATTENDANT ADVISED THE CREW THAT ALL OXYGEN MASKS HAD DROPPED.  NO WARNING FROM THE COCKPIT AND NO CABIN PRESSURE LIGHT.  FOUND OUTFLOW VALVE ACTUATOR INTERMITTENT.  REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR.  PERFORMED OPERATIONAL CHECK OF MASKS, CLEANED AND RESTOWED MASKS, OPS CHECK GOOD PER MM 35-20-00.


REMARKS:
FLT NR 470, IAD-MCO, UPON GEAR EXTENSION NO GREEN LIGHT ON, NOSE GEAR CYCLED FOUR TIMES, CHECKED VISUALLY.  CLEANED DOWNLOCK SENSOR OF RUST AND ELECT COMM.  PERFORMED NOSE GEAR SWING, CHECK PER MM 32-30 7-11-0 PAGE 201-211.  OPS CHECK NORMAL.


REMARKS:
FLT 206 - MCO-MCO, AIR RETURN, AFTER TAKEOFF THE RED LEFT GEAR UNSAFE LIGHT REMAINED ON.  RECYCLED GEAR, NO HELP, LIGHTREMAINED ON.  GEAR DOOR OPEN LIGHT WAS OUT.  REPAIRED AND ADJUSTED LEFT MLG UPLOCK PROXIMITY SWITCH SYSTEM.  OPS CHECKED OK IAW 32-10-0.


REMARKS:
FLT N 360 - RDU-IAD, THE LEFT GEAR UNSAFE LIGHT INDICATION CAME ON DURING GEAR RETRACTION.  CYCLED GEAR AND THE LIGHT STAYED ON, SAFE INDICATION ON APPROACH AND LANDING.  TROUBLESHOT SYSTEM AND PERFORMED OPS CHECK.  REMOVED AND REPLACED PROXIMITY SWITCH CONTROL BOX.  SYSTEM OPS CHECKS GOOD IAW DC-9 MM 32-30-0.


REMARKS:
LEFT GEAR UNSAFE LIGHT REMAINS ILLUMINATED FOLLOWING GEAR EXTENSION.  GEAR VISUALLY VERIFIED DOWN.  REMOVED AND REPLACED MAIN LANDING GEAR DOWN LOCK SWITCH, OPS CHECK NORMAL, REF 32-50-1 MM GEAR SWING.


REMARKS:
FLT 402 - ATL-ATL, TAKEOFF WAS ABORTED DUE TO FORWARD CARGO DOOR WARNING LIGHT ON.  ASSIGNED MEL TO FORWARD CARGO DOOR WARNING LIGHT ON PREVIOUS MRR ON 4/9/96.  ADJUSTED FORWARD CARGO DOOR LIGHT SWITCH, OPS CHECKED NORMAL.


REMARKS:
FLT 412 - ATL-ATL - AIR RETURN, FIRST OFFICERS ADI QUIT WORKING.  REMOVED AND REPLACED FIRST OFFICERS VERTICAL GYRO.  OPS IAW 34-20 GOOD.  NO DEFECTS NOTED.


REMARKS:
FLT 509 - ATL-ATL, AIR RETURN, THE RADAR WAS MALFUNCTIONING AND THE WEATHER PRESENTATION WAS UNUSABLE.  REMOVED AND REPLACED RADAR INDICATOR AND RADAR R/T.  OPS CHECK NORMAL.


REMARKS:
FLT 462 - TPA-TPA, AIR RETURN, THE RIGHT AFT OVERWING EXIT DOOR WAS NOT SEATED PROPERLY.  RESEATED THE DOOR AND PRESSURIZED THE A/C.  NO LEAKS NOTED.  A/C OK TO CONTINUE SERVICE.


REMARKS:
FLT 383 - BOS-B0S - AIR RETURN, DUE TO RIGHT GEN FLUCTUATES ON AND OFF AFTER TAKEOFF.  APU PREVIOUSLY ON MEL.  ASSIGNEDMEL TO RIGHT GEN AND CLEARED MEL ON APU.  REMOVED ADN REPLACED NR 2 CSD PER VJ MM 24-10-1.


REMARKS:
FLT NR 383 - BOS-BOS - AIR RETURN, DUE TO RIGHT GEN FLUCTUATES ON AND OFF AFTER TAKEOFF.  APU PREVIOUSLY ON MEL.  ASSIGNED MEL TO RIGHT GEN AND CLEARED MEL ON APU.


REMARKS:
FLT 498 - ATL-ATL - AIR RETURN, THE NR 2 EGT WENT INOP.  REMOVED AND REPLACED NR 2 EGT INDICATOR PER VJ MM 77-20-00, OPS CHECK GOOD.


REMARKS:
FLT NR 412 - ATL-ATL - AIR RETURN, FIRST OFFICERS ADI QUIT WORKING.  REMOVED AND REPLACED FIRST OFFICERS VERTICAL GYRO. OPS IAW 34-20 GOOD.  NO DEFECTS NOTED.


REMARKS:
FLT NR 360 - RDU-IAD - THE LEFT GEAR UNSAFE LIGHT INDICATION CAME ON DURING GEAR RETRACTION.  CYCLED GEAR AND THE LIGHTSTAYED ON, SAFE INDICATION ON APPROACH AND LANDING.  TROUBLESHOT SYSTEM AND PERFORMED OPS CHECK.  REMOVED AND REPLACED PROXIMITY SWITCH CONTROL BOX.  SYSTEM OPS CHECKS GOOD IAW DC-9 MM 32-30-0.


REMARKS:
FLT NR 206 - MCO-MCO - AIR RETURN, AFTER TAKEOFF THE RED LEFT GEAR UNSAFE LIGHT REMAINED ON.  RECYCLED GEAR, NO HELP, LIGHT REMAINED ON.  GEAR DOOR OPEN LIGHT WAS OUT.  REPAIRED AND ADJUSTED LEFT MLG UPLOCK PROXIMITY SWITCH SYSTEM.  OPS CHECKED OK IAW 32-10-0.


REMARKS:
DURING TEST FLIGHT FOR NOSE GEAR INDICATION PROBLEMS, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON.  GEAR POSITION VISUALLYVERIFIED.  MAINTENANCE FOUND BROKEN WIRE ON RIGHT GEAR PROX SWITCH.  MAINTENANCE REPAIRED WIRING SYSTEM GROUND CHECK GOOD.  (M)


REMARKS:
FLT NR 396 - PBI-BOS - THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION.  EXECUTED MISSED APPROACH, NOSE LIGHT ILLUMINATED DURING CLIMB AND LANDED NORMALLY.  CHECKED NOSE GEAR ASSEMBLY SWITCH, NO DEFECTS FOUND.


REMARKS:
FOUND LEFT OVERWING EMERGENCY LIGHT INOP.  MAINTENANCE REMOVED AND REPLACED POWER PACK AND BATTERY CHARGER ASSY.  OPS CHECKS GOOD.  REFERENCE IXKA960024.


REMARKS:
ON POST FLIGHT INSPECTION FOUND RIGHT AFT OVERWING HATCH LIGHT INOP.  MAINTENANCE REMOVED AND REPLACED BATTERY PACK.  OPERATIONALLY CHECKS GOOD.  (M)


REMARKS:
ON POST FLIGHT INSPECTION FOUND RIGHT FORWARD OVERWING HATCH EMERGENCY LIGHT INOP.  MAINTENANCE REMOVED AND REPLACED BATTERY PACK.  OPERATIONALLY CHECKS GOOD.  (M)


REMARKS:
INBOUND ITEM ON FLIGHT 46 TRACK LIGHTING COMING OUT OF FLOOR (NEAR ROW2).  MAINTENANCE INSTALLED NEW 'E' PATH TRACK ANDSECURED LENS.  PERFORMED OPS CHECK, NO DEFECTS NOTED.  (M)


REMARKS:
FOUND LEFT OVERWING EMERGENCY LIGHT INOP.  MAINTENANCE REMOVED AND REPLACED POWER PACK AND BATTERY CHARGER ASSY.  OPS CHECKS GOOD.  (M)


REMARKS:
FLT 44 - ATL - AFT FLASH LIGHT NO BLINKING.  REMOVED AND REPLACED AFT FLASH LIGHT BATTERY PACK.  (M)


REMARKS:
MEL CI NR 050001-C FORWARD RED EMERGENCY PATH LIGHT OUT.  MX TROUBLESHOT EMERGENCY TRACK LIGHT INOP, DUE TO BAD SPLICE AT PIGTAIL.  REPAIRED SPLICE AND EMERGENCY PATH LIGHTS CHECK GOOD.  (M)


REMARKS:
RSW - FL 1028 - AFTER TAKEOFF, CREW RECEIVED MASTER WARNING LIGHT DUE TO THE TAIL HIGH TEMPERATURE SIGNAL.  FLIGHT RETURNED TO RSW AND LANDED WITH NO FURTHER INCIDENT.  MX FOUND THE DUCTING AT THE WATER SEPARATOR ON THE RIGHT PACK LEAKING. DUCTING WAS SECURED AND THE AIRCRAFT RELEASED FOR FLIGHT.  (M)


REMARKS:
IN FLIGHT, AIRCRAFT DIVERTED TO PHX DUE TO CHEMICAL SMELL IN AFT CABIN AREA.  AIRCRAFT LANDED AT PHX WITHOUT INCIDENT.INSPECTED AND FOUND MIRROR LIGHT C/B TRIPPED.  AFT LAVATORY BALLAST HAD OVERHEATED AND WAS CAUSING SMELL.  REPLACED BALLAST AND SOCKET PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND FWD I/B EMERGENCY FLASHLIGHT LOW BATTERY.  REPLACED BATTERY PER BOEING M/M.


REMARKS:
DURING SCHEDULED B/C CHECK, FOUND EMERGENCY TRACK LIGHTING INOP AT ROWS 12 DEF AND 14ABC.  REPLACED BATTERY PACK AND HOUSING PER BOEING M/M.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND AFT SERV DOOR UPPER HINGE CUTOUT CRACKED.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND FWD ENTRY DOORWAY CRACKED AT LOWER HINGE CUTOUT AND AT FWD UPPER CORNER.  REPAIRED PER BOEING SRM.


REMARKS:
FOUND ESCAPE PATH LIGHTING INOP AT ROW 10.  RECONNECTED NUMEROUS WIRES AND REPLACED BATTERY PACK AT MID CABIN AREA PER BOEING M/M.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND UPPER LOBE FUSELAGE SKIN GOUGED AT BS 312, BETWEEN S4 AND 5L, ABOVE FWD ENTRY DOOR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B AT S18R.  REPAIRED PER BOEING SRM.


REMARKS:
INBOARD INTO DAL, RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED.  GEAR WAS RECYCLED AND RECEIVED NORMAL INDICATION.  AIRCRAFT LANDED AT DAL WITHOUT INCIDENT.  GEAR RETRACTION TESTED SEVERAL TIMES AND CHECKED SENSORS PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND FWD TRACK LIGHTING INOP.  REPLACED BATTERY CHARGER PER BOEING M/M.


REMARKS:
FOUND AFT UPPER EMERGENCY FLASHLIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
FOUND AFT CABIN UPPER EMERGENCY FLASHLIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
ON TAXI OUT, APU FIRE WARNING SOUNDED.  CREW PERFORMED APU SHUTDOWN PROCEDURES AND FIRE BOTTLE DISCHARGED.  AIRCRAFT RETURNED TO GATE.  INSPECTED WITH NO EVIDENCE OF FIRE OR OVERHEAT CONDITION.  REPLACED FIRE BOTTLE PER BOEING M/M, CONTINUED PER MEL 26-6.


REMARKS:
IN FLIGHT, RED NOSE GEAR LIGHT ILLUMINATED, NO AIR NOISE NOTED.  CYCLED GEAR HANDLE, NO HELP.  ON GEAR EXTENSION HAD ALL GREEN INDICATION.  INSPECTED AND FOUND A WIRE PULLED FROM SPLICE IN NOSE W/W.  REPAIRED PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 956, 1 BELOW S19R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND LEFT FUSELAGE SKIN CRACKED AT BS 727 BELOW WINDOW 7TH FROM EMERGENCY EXIT S15.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND RIGHT FUSELAGE SKIN CRACKED AT GROUND SERVICE DOOR CUTOUT LT CORNER.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP DAMAGED AT BS 747, S20L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 540, LBL 41, WL 156.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACK AT BS 727, LBL 15, WL 176.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE GOUGED AT BS 947.5 BETWEEN STRINGER 22 AND 23R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 867 AT S20R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CORROSION ON O/B SIDE OF STRINGER PRODUCTION SPLICE AT BS 907, S25L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR FRAME WEB CRACKED AT BS 847, RBL 26, WL 166.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME AT BS 400 DENTED AT LBL 28, WL 157, LBL 36, LBL 161, LBL 53, WL 173.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT NR 3 STOP FITTING CUTOUT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR LOWER GATE BEAM CRACKED AT LOWER FORWARD CORNER.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED JUST FWD OF FWD ENTRY, BS 308 BETWEEN S10 AND 13L.  REPAIRED PER BOEING SRM AND EWO 96-0187.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CHORD SPLICE CAP CORRODED AT BS 1016, LBL 4, WL 188.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, AFT LEFT ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED.  REPLACED AND PERFORMED EMERGENCY LIGHT TEST PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 27L DAMAGED AT BS 997.  REPLACED DAMAGED SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, WL 184, LBL 4.7.  REPAIRED PER BOEING SRM.


REMARKS:
SFO - FLT 56 - AFTER TAKEOFF FROM SFO, CREW RECEIVED OVETEMP LIGHT ON LEFT ENGINE.  LIGHT EXTINGUISHED WHEN THROTTLE RETARDED.  FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENTS.  MX REPLACED THE HP2 AND P6 DUCTS DUE TO LEAKAGE.REFERENCE USAABB96015.


REMARKS:
PIT - DURING SCHEDULED PRODUCTION CONTROL ITEM, FOUND A 2 INCH CRACK RIGHT SIDE SKIN LONGERON 14R-15R AT STATION 965.  INSTALLED TITANIUM DOUBLER PER USAIR EA NR 32460.  (M)


REMARKS:
ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 6 INCH CORROSION ON STRINGER, FORWARD OF AFT PRESSURE BULKHEAD STRINGER 26R BS 1016.  INSTALLED NEW STRINGER, REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
PIT - DURING A Q-1C-1 CHECK INSPECTION, FOUND .75 INCH CRACK RIGHT PYLON TOP DRAG ANGLE AT STATION 1019.  INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10.  (M)


REMARKS:
PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED APPROXIMATELY 3 FEET LONG FLOOR BEAM STATION 996 LEFT SIDE ON CAP ANGLE.  CPCP TASK  NR C58-53300.  REPLACED CORRODED SECTION OF CAP ANGLE PER USAIR TYPICAL REPAIR NR 53-10-14.  (M)


REMARKS:
PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND 2 CRACKS, ONE CRACK IS 1 INCH LONG AND THE OTHER CRACK IS 2.25 INCHES LONG IN BELTFRAME SKIN STATION 1038 LEFT SIDE BETWEEN LONGERON 12L AND 13L.  INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 3. (M)


REMARKS:
PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN LEFT FUSELAGE SKIN BETWEEN LONGERON 3L AND 4L STATION 1095.  INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27.  (M)


REMARKS:
PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND A 1 INCH CRACK RIGHT PYLON LOWER ATTACH ANGLE STATION 945 BETWEEN LONGERON 15R AND 16R.  INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10.  (M)


REMARKS:
PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND TWO 3 INCH CRACKS IN THE FORWARD HORIZONTAL PRESSURE PANEL AT FS 105 UNDER COCKPIT FLOOR NOSE WHEEL WELL.  REMOVED CRACKED SECTION AND INSTALLED REPAIR DOUBLER PER USAIR EA 32641.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORRODED FLOOR BEAM T-CAP STATION 328 RBL 12 TO RBL 48.  REMOVED OUT OFLIMITS FLOOR BEAM, FABRICATED T-CAP AND SPLICED NEW SECTION IN, REPAIRED PER 737 TR 53-10-13 PART 2.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND DENT 6 INCHES BY 1 INCHES AREA FUSELAGE SKIN BS 397 BETWEEN STRINGER 22L AND STRINGER 23L.  INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK LOWER AFT CORNER FORWARD SERVICE DOOR CUTOUT OUTER SKIN AND BEAR STRAP, BS 324 WL 210 RBL 68.  INSTALLED DOUBLERS, REPAIRED PER SRM 53-30-3 FIG 26.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH BY .50 INCH DEEP DENT IN SKIN AT BS 891 BETWEEN STRINGER 22R AND STRINGER 23R.  CUT OUT DAMAGE AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 40 INCH AREA OF SURFACE CORROSION, FLOOR BEAM UPPER T-CAP AT STATION 986.5 LBL 45 TO RBL 45.  INSTALLED T-CAP SPLICE, REPAIRED PER SRM 53-10-05C.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 3 INCH BY 40 INCH AREA OF SURFACE CORROSION, FLOOR BEAM T-CAP STATION 967, LBL 22 TO RBL 32.  REPLACED T-CAP, REPAIRED PER TR 53-10-05C.  (M)


REMARKS:
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 5 INCH AREA OF SURFACE CORROSION, FLOOR BEAM UPPER T-CAP, STATION 1016, RBL 1 TO RBL 6.  CUT OFF ENTIRE T-CAP, FABRICATED NEW PART AND INSTALLED PER EA 41077.  (M)


REMARKS:
ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 12/32 INCH BY .065 DENT RIGHT FUSELAGE SKIN AT STRINGER 20 BS 390.  REMOVED DAMAGED SKIN AND INSTALLED DOUBLER.  REPAIRED PER EA 58327.  (M)


REMARKS:
LAX - FLT 0017 - ON APPROACH TO LAX, CREW RECEIVED NOSE GEAR NOT DOWN INDICATION.  CREW CYCLED THE GEAR TWICE AND DID ATOWER FLYBY.  TOWER CONFIRMED THAT THE NOSE GEAR WAS STILL RETRACTED.  ON THIRD RECYCLE, THE NOSE GEAR EXTENDED.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE NOSE GEAR LOCK ACTUATOR, NOSE GEAR OPERATED SEQUENCE VALVE AND THE NOSE GEAR DOOR SEQUENCE VALVE.  (M)


REMARKS:
SFO - FLT 56 - AFTER TAKEOFF FROM SFO, CREW RECEIVED OVETEMP LIGHT ON LEFT ENGINE.  LIGHT EXTINGUISHED WHEN THROTTLE RETARDED.  FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENTS.  MX REPLACED THE HP2 AND P6 DUCTS DUE TO LEAKAGE.(M)


REMARKS:
FLT 730 - MSY-PHL - CLIMBING THROUGH APPROXIMATELY 12,000 FEET, CABIN AND COCKPIT STARTED TO FILL WITH NOXIOUS FUMES.  PACKS WERE TURNED OFF, AND FUMES BEGAN TO CLEAR.  RETURNED TO MSY.  FOUND BIRD STRIKE AT INTAKE RIGHT ENGINE.  INSPECTEDINTAKE AND EXHAUST AND FOUND NO DAMAGE.  PERFORMED INSPECTION PER MD-80 MM 05-31-08, PG 601 AND 602.  (M)


REMARKS:
FLT 254 - PBI-BWI - AT FL 330, MASTER CAUTION LIGHT CAME ON, LOW OIL PRESSURE LIGHT CAME ON, NOTICED LOSS OF ALL OIL QUANTITY, LOW OIL PRESSURE, AND RISING OIL TEMPERATURE. SHUT DOWN NR 1 ENGINE, DIVERTED TO SAV.  REMOVED AND REPLACED NR 1ENGINE OIL PRESSURE SWITCH LINE.  (M)


REMARKS:
PIT - FLT 1450 - AFTER GEAR EXTENSION, CAPTAIN RECEIVED ALL THREE GREEN LIGHTS BUT HAD THE LEFT LANDING GEAR DOWNLOCK SWITCH MESSAGE.  CAPTAIN RECYCLED THE GEAR WITH NO CHANGE.  LIGHT WENT OUT PRIOR TO TOUCHDOWN.  NO EMERGENCY WAS DECLAREDAND THE FLIGHT MADE A NORMAL LANDING.  MAINTENANCE REPLACED THE LEFT MLG PRIMARY DOWNLOCK SENSOR.  (M)


REMARKS:
LGA - FL 866 - UPON LANDING IN LGA, BRAKE PEDALS WENT TO FLOOR, GRABBED AND CYCLED.  MAINTENANCE REPLACED THE LOWER FUSELAGE STROBE LIGHT DUE TO ELECTROMAGNETIC INTERFERENCE WITH THE ANTI-SKID SYSTEM.  ANTI-SKID TEST ACCOMPLISHED, CHECKED NORMAL.  (M)


REMARKS:
FLT 510 - ROC - MAINTENANCE FOUND THAT THE AFT ENTRY AND SERVICE DOOR EMERGENCY SLIDE LIGHTING SYSTEM WAS INOP.  MX REPLACED THE BATTERY AND THE CHARGER.  SYSTEM CHECKED SAT.  (M)


REMARKS:
FLT NR 2359 - LGA - MX FOUND THAT THE AFT LAV SMOKE DETECTOR WAS INOP.  MX REPLACED THE SMOKE DETECTOR IN THE AFT LAV.OPS CHECKS SATISFACTORY.  (M)


REMARKS:
FLT 1847 - DCA - CABIN EMERGENCY LIGHTS COME ON INTERMITTENTLY IN FLIGHT IN THE WHEN ARMED.  MAINTENANCE REPLACED THE CHARGER ASSEMBLY.  OPS CHECKED SATISFACTORY.  (M)


REMARKS:
FLT NR 2009 - CLT - HARMONIC SURGE FELT IN AIRFRAME DURING CLIMB-OUT AND TO A LESSER EXTENT IN CRUISE.  THIS SURGE FELTMORE PRONOUNCED AT 180 TO 250 KNOTS.  MX RESEALED WING TO BODY FAIRING LEFT SIDE.  INSPECTED FLIGHT CONTROLS, FUSELAGE,AND GEAR.  NO DEFECTS NOTED.  AIRCRAFT OK FOR SERVICE.  (M)


REMARKS:
DURING SCHEDULED MAINT CHECK, FOUND BULKHEAD AT BS 351.2 ATTACH BRACKET CRACKED ON LEFT SIDE.  REPAIRED PER BOEING SRM.


REMARKS:
STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED.  CYCLED LANDING GEAR.  FOUND RIGHT MAIN LANDING GEAR BUNGEE CYLINDER MALFUNCTION.  REPLACED RIGHT MAIN LANDING GEAR BUNGEE CYLINDER, MFG P/N 3914016-5505.  LANDING GEAR OPERATION AND INDICATION THEN CHECKED NORMAL.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT STATION 727 BULKHEAD STIFFENER FITTING IN LOWER FORWARD RADIUS, BL 0 WL 202.5.  REPAIRED PER EO 5394G176.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 178 BULKHEAD SKIN LBL 4.75, WL 198.  INSTALLED DOUBLER, REPAIRED PER EA 40743.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 178 BULKHEAD SKIN LBL 4.75, WL 201.  INSTALLED DOUBLER, REPAIRED PER EA 40743.  (M)


REMARKS:
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1875 INCH CRACK STATION 178 BULKHEAD SKIN RBL 4.75 WL 201.  INSTALLED DOUBLER, REPAIRED PER EA 40743.  (M)


REMARKS:
PIT - FL 1137 - CLIMBING OUT OF PHL EN ROUTE DTW, CREW RECEIVED A GEAR DOOR WARNING LIGHT.  FLIGHT DIVERTED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE PROXIMITY SENSOR ON THE LEFT GEAR DOOR LOOSE.  SENSOR WAS ADJUSTED AND TIGHTENED.  (M)


REMARKS:
BOS-YYZ - FL 930 - EN ROUTE THE CENTER WINDSHIELD CRACKED.  FLIGHT RETURNED TO BOS AND LANDED WITHOUT NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE WINDSHIELD AND THE WINDSHIELD HEAT CONTROLLER, (P/N 9615059002.  (M)


REMARKS:
FLT 366 - PIT-STL - DURING CRUISE AT FL 210, CABIN ALTITUDE CLIMBED TO 11,000 FEET.  STOPPED CABIN AT 12,000 FEET, DESCENDED TO 10,000 FEET.  CABIN PRESSURIZATION WORKED IN MANUAL MODE.  REPLACED OUTFLOW VALVE ACTUATOR.  (M)


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR INOPERATIVE.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED C2/C4 CHECK, FOUND AFT CARGO COMPT DOOR WEB CRACKED .75 INCH AND ANGLE CRACKED AT FWD LOWER DOOR STOP. REPLACED CARGO DOOR PER BOEING M/M.


REMARKS:
DURING SCHEDULED BC1 CHECK, FOUND R1 AND L1 C-D COCKPIT WINDOW POSTS CRACKED.  INSTALLED REPAIR PER SWA RA 1-A53-1156.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4R.  REPLACED SPLICE PER BOEING SRM.


REMARKS:
DURING SCHEDULED A-CHECK, FOUND FUSELAGE SKIN CRACKED, JUST FWD OF WATER SERVICE BAY DOOR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED A-CHECK, FOUND FUSELAGE SKIN CRACKED JUST FWD OF WATER SERVICE BAY DOOR AND ALSO 24 INCHES FWD OF OUTFLOW VALVE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, AT BS 727B, AND AT BS 747 RT SIDE.  REPAIRED ALL PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED AT BS 290, BETWEEN S10 AND S11R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD SERVICE DOOR CUTOUT CRACKED AT LOWER CORNER AT FASTENER HOLE AND Z-ANGLE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM STABILIZING STRAPS CRACKED AT BS 311, BL ZERO, RBL 32, AND AT LBL 14.  REPLACED PER BOEING SRM.


REMARKS:
IN-FLIGHT, NOTED ELECTRICAL/RUBBER ODOR IN AFT CABIN AREA. NO VISIBLE SMOKE.  NO EMERGENCY DECLARED.  AIRCRAFT RETURNEDTO BUR AND MADE AN UNEVENTFUL LANDING.  INSPECTED ALL FLUORESCENT LIGHTING, SIDEWALL LIGHTS, COFFEMAKERS, LAVATORIES, HEATERS, FLIGHT RECORDER COMPT, CARGO COMPTS, PAX LIGHTS AND PSU'S, E & E COMPT, RAN A/C GASPER FANS, NO EVIDENCE OF SMOKE OR SMELL.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT DOOR FRAME CRACKED AT BS 492, RBL 36, WL 162.  REPAIRED PER TRAMCO EWO 96-0212.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKS AT BL ZERO, WL 187, AT RBL 5.7, WL 200, AND AT LBL 5.7, WL 200/204.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR LOWER AFT CORNER INSIDE DOUBLER CRACKED.  REPAIRED WITH NEW DOUBLER PERBOEING SRM.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND FWD CABIN EMERGENCY LIGHTS INOP.  REPLACED BATTERY SUPPLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED BC1 CHECK, FOUND A .5 INCH CRACK AT COOLING DUCT CUTOUT SKIN AFT END.  REPAIRED PER BOEING SRM.


REMARKS:
ON CLIMB-OUT, NR 1 ENGINE INDICATED EGT OVERTEMP CONDITION FOR 3 SECONDS.  AIRCRAFT RETURNED TO ABQ AND MADE AN UNEVENTFUL LANDING.  PERFORMED ENGINE INLET AND EXHAUST INSPECTION PER BOEING M/M.  NO DEFECTS NOTED.


REMARKS:
CHARTER FLIGHT EN ROUTE, AIRCRAFT DIVERTED TO BNA DUE TO FLUID SPILL ONTO NAV/COMM CONTROLS, MAKING BOTH ILS AND NR 1 COMM INOPERATIVE.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT BNA.  INSPECTED AREA.  REPLACED CAPT AND F/O NAV CONTROL PANELS, BOTH COMM CONTROL PANELS, AND NR 1 NAV RECEIVER PER BOEING M/M.


REMARKS:
IAD/IAD - FLT 287 - AIR RETURN, LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED AFTER TAKEOFF.  ABNORMAL PROCEDURES FOLLOWED.REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP PER MM 29-10-05.  OPERATIONAL AND LEAK CHECK OK.  SERVICED HYDRAULIC SYSTEM.


REMARKS:
SJU - FLT 11 - DURING CLIMB, A NOSE GEAR DOOR LIGHT FAULT INDICATION WAS OBSERVED.  NOSE GEAR PROXIMITY SWITCHES WERE CHECKED, OPERATION NORMAL.  OP-15 - 12-29-95 - SEA.


REMARKS:
STL  FLT 467 - DURING CRUISE, RED NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED.  FOUND INTERNAL MALFUNCTION IN NLG PROXIMITY SWITCH, MFG PN 8-337-03.  REPLACED NLG PROXIMITY SWITCH AND NLG INDICATION, CHECKED NORMAL.  CHECK C-1D - 12-4-95 - JFK.


REMARKS:
MEM/MCO - FLT 373 - DIVERTED TO ATL, NR 2 EGT AND NAV REC WENT INOP.  EGT CHECKED GOOD ON RUN-UP CHECK FOR SERVICE.  REMOVED AND REPLACED NR 2 NAV-REC, OPS CHECK IAW 34-40.


REMARKS:
BOS/BOS - FLT 361 - ABORTED TAKEOFF, NR 2 ENGINE EGT WAS ERRATIC.  THE NR 2 ENGINE EGT GAUGE STOPS AT APPROXIMATELY 350DEGREES WHEN TAKEOFF POWER WAS APPLIED.


REMARKS:
ATL/CMH - FLT 274 - ALL THE PASSENGER MASKS DEPLOYED IN-FLIGHT.  PERFORMED DROP AND LEAK CHECK, FOUND THE PASSENGER OXYGEN REGULATOR LEAKING.  REMOVED AND REPLACED REGULATOR PER MM 35-20, OPS CHECK GOOD, NO LEAKS NOTED.


REMARKS:
ON FLIGHT 134, FL, ABORTED TAKEOFF, NR 2 ENGINE WOULD NOT REACH TAKEOFF EPR, FULL POWER = 1.80.  REMOVED AND REPLACED FUEL CONTROL UNIT PER MM 73-00.  NO LEAKS NOTED.


REMARKS:
WHILE SITTING AT GATE IN MCO MAKING PA ANNOUNCEMENTS, THE CIRCUIT BREAKER'S FOR PA, INTERPHONE, 'NO SMOKING' AND 'FASTEN SEAT BELT' LIGHTED SIGNS TRIPPED.  SMOKE SMELL IN THE CABIN.  ACCOMPLISHED VALUJET AIRLINES EO DC-9-3396005, SEAT BELT, NO SMOKING SIGN, PASSENGER WARNING SYSTEM WIRING.


REMARKS:
ATL/ATL - FLT 110 - AIR RETURN, LANDING GEAR WOULD NOT RETRACT.  FOUND GEAR BYPASS HANDLE DOWN.  REPLACED RIGHT MAIN GEAR DOOR AND LEFT GEAR DOOR BUMPER.  RESET BYPASS HANDLE, OPS CHECK NORMAL.


REMARKS:
MCO/IAD - FLT 470 - ON LANDING, RIGHT HYDRAULIC FLUID WAS LOST.  AIRCRAFT TURNED OFF RUNWAY ONTO TAXIWAY, GEAR PINS INSTALLED.  REPLACED HYDRAULIC FILTER ASSEMBLY AND CUT PACKING.  LEAK CHECKS OK.


REMARKS:
ATL/ATL - FLT 495 - AIR RETURN, AFTER TAKEOFF, THERE WAS A LOUD WIND NOISE COMING FROM THE NOSE GEAR AREA.  RECYCLED GEAR, HAD A RED NOSE GEAR LIGHT ON.  LIGHT WENT OUT IN SIXTY SECONDS AND HAD A NORMAL LANDING.  JACKED AIRCRAFT, ADJUSTED NOSE GEAR DOORS, CYCLED GEAR.  SYSTEM OPS CHECKED GOOD.


REMARKS:
MCO/IAD - FLT 470 - ON LANDING, RIGHT HYDRAULIC FLUID WAS LOST.  AIRCRAFT TURNED OFF RUNWAY ONTO TAXIWAY, GEAR PINS INSTALLED.  REPLACED HYDRAULIC FILTER ASSY AND CUT PACKING.  LEAK CHECKS OK.


REMARKS:
ATL/ATL - FLT 491 - THE CREW EXPERIENCED A GREEN NOSE GEAR INDICATION WITH THE GEAR RETRACTED.  REMOVED AND REPLACED NOSE GEAR WARNING LIGHT ASSEMBLY AND OPS CHECKED NOSE GEAR.


REMARKS:
ATL/ATL - FLT 519 - AFTER TAKEOFF, AIR RETURN WHILE EXECUTING THE 'GEAR UPLATCH CHECK', THE 'RIGHT GEAR UNSAFE' LIGHT CAME ON COUPLED WITH THE 'GEAR DOOR OPEN' LIGHT.  FOUND SPRING ON RT MAIN GEAR DOOR UPLATCH BROKEN.  REMOVED AND REPLACEDSPRING GEAR DOOR AND LIGHTS.  OPS CHECK OK.


REMARKS:
MCI - DURING CLIMB, UNABLE TO RETRACT FLAPS ABOVE ONE DEGREE.  RESEATED FLAP/SLAT ELECTRONIC UNIT.  OPERATIONAL CHECK AND BYTE TEST NORMAL.  (M)


REMARKS:
MCI - FLT 5034 - DURING CRUISE, SHUT DOWN NR 2 ENGINE DUE TO INCREASE OF VIBRATION ON BOTH A AND B CHANNELS.  FOUND FANOUT OF TRIM BALANCE.  PERFORMED ENGINE TRIM BALANCE.  ENGINE OPERATION AND INDICATION THEN CHECKED NORMAL.


REMARKS:
MCI - DURING C-CHECK, FOUND CORROSION UNDER SKIN BELOW AFT LAV SERVICE AREA, AND RIVET HEADS POPPED.  REMOVED SKIN AND REPAIRED PER ARA 9917 AND SRM 51-20-1, 51-20-2 AND 51-20-4.  (M)


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND 1.5 INCH CRACK IN UPPER FORWARD CHORD OF LEFT WING RIB, STATION 503.76.  STOP DRILLEDAND REPAIRED PER EMLR 66589.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND 1.25 INCH CRACK IN LEFT WING RIB CASTELLATION FORWARD SIDE OF STRINGER 19, TOP CHORD,WS 503.  REPAIRED PER SERVICE BULLETIN 093-57-207, PARA 2B.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND SEVEN CRACKS IN LEFT WING TOP RIB CASTELLATION, STATION 555.  REPAIRED PER SERVICE BULLETIN 093-57-207, PARA 2B.  (M)


REMARKS:
STL - DURING CLIMB, RIGHT THRUST REVERSER LIGHT ILLUMINATED.  REPAIRED WIRING TO RIGHT THRUST REVERSER.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
MCI - DURING C-CHECK, FOUND FRONT AND REAR TANGS CRACKED ON FORWARD VENT BOX, WS 629.  REPAIRED PER SSRM 52-20-201.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND FUSELAGE FORMER, FS 1605, DENTED AND CRACKED, STRINGER 13L TO STRINGER 20L.  REPLACEDFORMER PER ARA 9958.  (M)


REMARKS:
STL - DURING SPECIAL CHECK, FOUND CABIN AREA LONGERON 6L CRACKED AT BOTH ATTACH POINTS, STATION 718.  REPAIRED PER SRM 53-02, FIGURE 2.  (M)


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND LEFT STABILIZER LOWER SKIN DAMAGED.  REPAIRED PER ARA 9959.  (M)


REMARKS:
FLT 707 - STL - DURING DESCENT, TRAILING EDGE OUTBOARD FLAPS WOULD NOT EXTEND.  REMOVED AND REPLACED OUTBOARD TRAILING EDGE FLAP BYPASS VALVE, MFG P/N 106788A103.  OPERATIONAL CHECK NORMAL.


REMARKS:
FLT 680 - STL - DURING LANDING, 'A' SYSTEM HYDRAULIC QUANTITY WAS LOST.  REMOVED AND REPLACED NR 6 LEADING EDGE SLAT ACTUATOR, MFG P/N 1U1095-9-2.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
JFK- DURING C-4D CHECK, FOUND A 1.25 INCH CRACK BETWEEN HOLE AND RADIUS OF RIB LOWER FLANGE AT STRINGER 6, RIB WS 546.5.  REPAIRED EPR SERVICE BULLETIN 727-57A159, PAGES 6, 7 AND 8.  (M)


REMARKS:
JFK - DURING C-4D CHECK, FOUND RIB CRACKED AT RADIUS AREA AT ATTACH POINT TO FIRST STRINGER AFT OF ACCESS HOLE, WL 601.5.  REPAIRED BY STOP DRILLING, FABRICATING AND INSTALLING DOUBLER PER SRM 57-10-05, PAGES 6, 7 AND 8.  (M)


REMARKS:
STL - FLT 501 - DURING CRUISE EMERGENCY EGRESS LIGHT ILLUMINATED.  REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2, OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
MIA - FLT 492 - WHILE AT THE GATE, OVENS BY L-1 DOOR EMITTED BURING SMELL AND SMOKE.  OVENS WERE SHUT DOWN AND CIRCUIT BREAKER PULLED.  BURNED PAPER AND FOOD WAS REMOVED FROM OVENS.  OVENS WERE OPERATED AT THEIR HIGHEST TEMPERATURE SETTINGFOR 30 MINUTES AND NO ABNORMALITIES WERE NOTED.  (M)


REMARKS:
STL - FLT 16 - DURING LAYOVER, MAINTENANCE EMERGENCY EGRESS LIGHTS ON BOTH AISLES, BETWEEN NR 3 AND NR 4 DOORS, REMAINED ON CONTINUOUSLY.  REMOVED AND REPLACED EGRESS LIGHT POWER SUPPLY, MFG P/N 5822-3.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
FLT 402 - STL - DURING CRUISE, AFT CABIN EMERGENCY EGRESS LIGHTS ILLUMINATED.  CLEANED AND DRIED MOISTURE FROM TRACK CONNECTION.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND FOD DAMAGE TO LEFT AFT FUSELAGE, FS 1605 TO FS 1629 AND FROM STRINGER 20L TO STRINGER16L.  REPLACED AND REPAIRED SKIN PANEL PER ATA 9958A AND TWA STANDARD PRACTICES.  (M)


REMARKS:
STL - FLT 547 - DURING CRUISE, L-1 AND R-1 AND REAR DOOR EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY.  CYCLED EMERGENCYLIGHT SWITCH AT FORWARD FLIGHT ATTENDANTS PANEL.  OPERATIONAL CEHCK NORMAL.  (M)


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND FOD DAMAGE TO LEFT HORIZONTAL STABILIZER LOWER SKIN AND FRONT SPAR, FS 186 TO FS 255. REPAIRED PER ARA 9957 AND TWA AND STANDARD PRACTICES.  (M)


REMARKS:
LNK - FLT 677 - DURING APPROACH, SHUT DOWN NR 2 ENGINE, S/N 3808, DUE TO LOSS OF OIL QUANTITY AND LOW OIL PRESSURE.  FOUND OIL LEAK AT NR 6 BEARING OIL TUBE, MFG P/N RD2189-1.  REPLACED OIL TUBE.  ENGINE OPERATION AND LEAK CHECK NORMAL.


REMARKS:
STL - FLT 284 - DURING APPROACH, AFTER LANDING GEAR EXTENSION, LEFT MAIN LANDING GEAR DOOR LIGHT ILLUMINATED.  CYCLED LANDING GEAR.  CLEANED CONNECTOR FOR LEFT LANDING GEAR DOOR SWITCH, MFG P/N H14-6, AND LANDING GEAR DOOR OPERATION AND INDICATION.


REMARKS:
JFK - FLT 31 - AT TOP OF CLIMB, NR 1 ENGINE ENCOUNTERED POWER SURGE.  REDUCED POWER AND REAPPLIED POWER.  FOUND ENGINE VANE BLEED CONTROL, MFG P/N 766555-7, MALFUNCTIONING.  CHANGED ENGINE VANE BLEED CONTROL AND ENGINE OPERATION CHECKED NORMAL.


REMARKS:
JFK - DURING C-4D CHECK, FOUND A CRACK AT STRINGER 13 VENT BOX FORWARD TAB, STATION 656.5.  REPAIRED PER SERVICE BULLETIN 727-57A159.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A 1 INCH CRACK IN LONGERON 6R, STATION 639.  REPAIRED PER SRM 53-02, PAGE 2A, FIGURE 2.


REMARKS:
FLT 382 - TPA-BOS - DIVERTED TO ATL, THE RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED EN ROUTE, DIVERTED FLIGHT, GEAR EXTENDED NORMALLY WITH NORMAL INDICATION.  FOUND RIGHT MLG UPLIMIT SWITCH BINDING ON THE SWITCH STRIKER.  REPLACED STRIKER AND SWITCH IAW MM 32-60-1.


REMARKS:
ON FLT 400 - ATL-ATL - AIR RETURN, AFTER TAKEOFF CLIMB POWER WAS SET, THE NR 2 ENGINE BEGAN TO SURGE, EPR 1.5-1.7, F/F PLUS MINUS 1500 LBS/HR, EGT, N1, N2 ALSO FLUCTUATED.  REPLACED PRBC AND P AND D VALVES IAW MM 73-10-2 (P AND D) AND 75-31-1 (PRBC), RAN NR 2 ENGINE IAW MM 71-00 OPS CHECKED GOOD.


REMARKS:
ON FLT 400 - ATL-ATL - AIR RETURN, AFTER TAKEOFF CLIMB POWER WAS SET, THE NR 2 ENGINE BEGAN TO SURGE.  EPR 1.5-1.7, F/FPLUS MINUS 1500 LBS/HR, EGT, N1, N2 ALSO FLUCTUATED.  REPLACED PRBC AND P AND D VALVES IAW MM 73-10-2 (P AND D) AND 75-31-1 (PRBC), RAN NR 2 ENGINE IAW MM 71-00 OPS CHECKED GOOD.


REMARKS:
FLT NR 72 - TPA-ATL - IN FLIGHT SHUTDOWN, NR 3 ENGINE LOW OIL PRESS OIL FILTER BYPASS LIGHT ILLUMINATED DURING FLIGHT.NR 3 OIL TEMP ROSE FROM 81 TO 110 DEGREES.  SHUT DOWN AS PER EMERGENCY CHECK LIST.  REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE UNION ORIFICE AT OIL PRESS MANIFOLD RUNUP AND LEAK CHECK NORMAL PER MM 79-32-00.  (M)


REMARKS:
FLIGHT NR 2, EWR-BDA - AIR TURN BACK DUE TO OMEGA READING ERROR WITH FLIGHT PLAN.  REMOVED AND REPLACED OMEGA RPU, OPS CHECK OK AS PER MM 34-68-01.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH CORROSION SEAT TRACK BS 344 TO BS 349 LBL 22.  CUT SEAT TRACK AND SPLICED IN NEW, REPAIRED PER SRM 53-10-5.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 3 INCH CORROSION BS 1006 TO BS 996 STRINGER 26L.  INSTALLED REPLACEMENT STRINGER SECTION, REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 1156 OUTBOARD OF LEFT OUTBOARD PIVOT FITTING BULKHEAD. INSTALLED DOUBLER, REPAIRED PER EO 5391G569.  (M)


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 2 INCH BY 3 INCH LEVEL 1 CORRODED AREA PREVIOUSLY REWORKED IN BELTFRAME STATION 1309 LONGERON 30.  CORROSION TASK NR C57-53300.  ACCOMPLISHED SPLICE REPAIR PER SRM 53-03 FIG 2. (M)


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 1 INCH BY 4 INCHES OF CORRODED AREA BETWEEN STATION 446 AND 465 LONGERON 26L.  LEVEL 2 CORROSION REF TASK NR C-51-53300.  REMOVED CORRODED SECTION AND SPLICED IN NEW LONGERON SECTION PER SRM 53-02 FIG 5.  (M)


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AREA 4 INCHES BY 4 INCHES AT STATIC PORT HEATING PAD SKINBETWEEN STATION 446 AND 465 BETWEEN LONGERON 26L AND 27L.  CORROSION TASK REF C51-53300.  REMOVED DAMAGED AREA AND SPLICED IN NEW SKIN SECTION PER USAIR EA NR 32634.  (M)


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, TWO 1 INCH CRACK AT LOWER FLANGE OF LONGERON 17L, STATION 275 AND 294.  ACCOMPLISHED SPLICE REPAIR PER TYPICAL REPAIR 53-10-17.  (M)


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 1 INCH CRACK AT LOWER FLANGE OF LONGERON 17L STATION 408.  ACCOMPLISHED SPLICE REPAIR PER USAIR TYPICAL REPAIR 53-10-17.  (M)


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 3 CLIPS CRACKED RANGING FROM 1.75 INCH TO 2.25 INCH LONG CANTED FRAME STATION 1463 LONGERON 7, 9 AND 10.  REPAIRED IAW SRM 53-14-4 FIG 3 SHEET NR 7 AND DACO DWG 9911839 AND 9911877.  (M)


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND TWO 1 INCH CRACKS IN LONGERON 17R LOWER FLANGE STATION 228 AND 237.  REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2 PG 2A.  (M)


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 1 INCH CRACK IN LOWER FLANGE IN LONGERON 17R, 4 PLACES AT STATION 256, 408,370 AND 389.  REMOVED DAMAGED SECTION OF LONGERON AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-02 PAGE 2A.  (M)


REMARKS:
ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK FUSELAGE SKIN AT BS 727 A BETWEEN STRINGER 15 AND 16 LEFT.  INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 PAGE 01.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND .25 INCH CRACK IN MAIN ENTRANCE DOOR TOP AFT DOOR STOP SKIN BOTH LAYERS.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 26A.  (M)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND .5 INCH LONG CRACK IN LONGERON 3L AT STATION 756.  INSTALLED SPLICE REPAIR PERSRM 53-02 FIG 2.  (M)


REMARKS:
PIT - DURING C-6 CHECK INSPECTION, FOUND A 1.5 INCH CRACK IN T-CAP AT STATION 996 LONGERON 14L (APBH).  SPLICED IN NEW SECTION OF T-CAP PER SRM 53-03 FIG 37A.  (M)


REMARKS:
PIT - DURING C-6 AND ACCOMPLISHMENT OF EO 3495X040, FOUND 3 SMALL AREAS OF CORROSION 20 PERCENT OF SKIN THICKNESS IN DEPTH UNDER NR 1 ADF ANTENNA STATION 266 AND ADF ANTENNA STATION 313 LONGERON NR 1.  REMOVED AND REPLACED CORRODED SKIN AREA PER USAIR EA 32324.  (M)


REMARKS:
FLT 1121 - BOS-DCA - RIGHT ENGINE FAILED AFTER TAKEOFF.  NO INDICATION PRIOR TO FAILURE, NO FIRE WARNING.  SINGLE ENGINE TIME 5 MINUTES.  REPLACED RIGHT ENGINE FUEL PUMP AND FUEL CONTROL UNIT.  (M)


REMARKS:
BOS - FL 478 - AT TOP OF CLIMB, FL 230, LEFT ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT.  OIL TEMPERATURE OF LEFT ENGINE WAS THIRTY TO THIRTY-FIVE DEGREES HIGHER THAN THE RIGHT ENGINE TEMPERATURE.  FLIGHT RETURNED TO BOS AND SHUT DOWN ENGINE ON FINAL APPROACH.  SET: 4 MINUTES.  MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL UNIT.  (M)


REMARKS:
FLT 7003 - ROC - CEILING MOUNTED EMERGENCY LIGHTS BETWEEN ROWS 5 AND 7 INOP.  FOUND DURING OVERNIGHT CHECK.  REPLACED BATTERIES IN POWER PACK.  OPERATIONAL CHECK OK.  (M)


REMARKS:
FLT 1168 - SYR - RIGHT NACELLE EMERGENCY LIGHT INOP.  MAINTENANCE REPLACED THE BATTERY PACK FOR RIGHT NACELLE EMERGENCYLIGHT.  OPS CHECK SAT.  (M)


REMARKS:
FLT 517 - YYZ-PHL - LEFT MAIN GEAR DID NOT INDICATE SAFE WITH GEAR DOWN.  LEFT MAIN GEAR UNSAFE LIGHT DID NOT ILLUMINATE.  FOUND PIN NR 5 AT LEFT MAIN GEAR DOWNLOCK SWITCH PUSHED BACK.  REINSTALLED PIN, OPS CHECKS GOOD.  TWO TOWER FLY-BY'SWERE CONDUCTED TO VISUALLY ASCERTAIN GEAR POSITION.  (M)


REMARKS:
PIT - FL 1036 - UPON REACHING FL 180 OUT OF PIT, CREW NOTED BOTH RIM'S SPINNING AND COULD NOT FIX THE AIRCRAFT POSITION.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT RMI.  (M)


REMARKS:
CLT - FL 498 - ON DESCENT INTO CLT, CREW LOST UTILITY HYDRAULIC SYSTEM.  CAPTAIN EXTENDED THE LANDING GEAR AND FLAPS USING ALTERNATE PROCEDURE.  NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY.  MAINTENANCE REPLACED NR 1 ENGINE DRIVEN PUMP AND PRESSURE FILTER.  THE HYDRAULIC SYSTEM WAS SERVICED, THE ENGINE WAS RUN AND LEAK TESTED AND ALL FLIGHT CONTROLS WERE OPS CHECKED AS NORMAL.  (M)


REMARKS:
DCA - FL 2286 - ON DESCENT INTO DCA, LEFT LANDING GEAR DOOR SWITCH CAME ON MFDU AFTER THE GEAR WAS LOWERED.  CREW HAD THREE GREEN LIGHTS FOR GEAR BUT AS THEY DESCENED BELOW 900 FEET, THE LANDING GEAR AURAL WARNING CAME ON.  CREW RECYCLED GEAR AND LIGHT WENT OUT.  FLIGHT LANDED IN DCA WITHOUT FURTHER INCIDENT.  MX ADJUSTED THE LEFT NR 2 LANDING GEAR DOOR SENSOR PER THE MM.  LANDING GEAR FUNCTIONAL CHECK WAS GOOD.  (M)


REMARKS:
PIT - FL 8075 - DURING DESCENT INTO AVP, THE CREW COULD NOT GET THE FLAPS TO EXTEND.  A DECISION WAS MADE TO DIVERT TO PIT WHERE MAINTENANCE IS AVAILABLE TO MAKE REPAIRS.  THE CAPTAIN DECLARED AN EMERGENCY FOR PRECAUTIONARY MEASURES.  THE FLIGHT LANDED WITHOUT INCIDENT.  MX REPLACED THE LEFT INBOARD FLAP SYNCHRO.  OPERATIONAL CHECK OK.  (M)


REMARKS:
TOA - FL 1250 - AFTER TAKEOFF FROM PIT, THE LEFT GEAR RED LIGHT REMAINED ON AFTER GEAR RETRACTION.  CREW CYCLED GEAR AND ALL LIGHTS WENT OUT.  MAINTENANCE FOUND THE FORWARD LEFT GEAR DOOR SWITCH LOOSE.  SWITCH WAS SECURED AND OPS CHECKED (GEAR SWING).  CHECKED GOOD.  (M)


REMARKS:
CLT - MX FOUND THE FORWARD WING TO BODY FAIRING EMERGENCY LIGHTING SYSTEM INOP.  MX REPLACED THE FORWARD WING TO BODY FAIRING POWER SUPPLY AND BATTERIES.  OPS CHECKED GOOD.  (M)


REMARKS:
FLT 2674 - LGA - EMERGENCY EXIT LIGHT AT FORWARD SERVICE DOOR INOP.  MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK OVER FORWARD GALLEY SERVICE DOOR.  EMERGENCY LIGHTS OPS CHECK GOOD. (M)


REMARKS:
FLT 1862 - BWI - DURING APPROACH TO DCA, GEAR WAS LOWERED BUT WE HAD NO INDICATION OF SAFE INDICATIONS.  DIVERTED TO BWI.  EMERGENCY DECLARED.  MAINTENANCE CYCLED THE GEAR SEVERAL TIMES, COULD NOT DUPLICATE FAULT.  REPLACED THE FOLLOWING ITEMS AS A PRECAUTIONARY MEASURE, L/G AIR GROUND RELAY, LIGHTS C/B, MASTER DIM BUS C/B.  GEAR SWING NORMAL.  (M)


REMARKS:
FLT 84 - SAN - NR 1 IRU FAULT LIGHT ILLUMINATED IN FLIGHT.  IN ATT ADI WOULD NOT RECOVER AND HEADING SELECT WAS UNSUCCESSFUL, HEADING SLEWED TO MANUAL SETTING BUT IMMEDIATELY STARTED TO DRIFT.  RETURNED TO SAN.  MX REPLACED NR 1 IRU.  BITECHECK NORMAL.  (M)


REMARKS:
FLT 357 - MCO - ON ROTATION LOST AUTO-THROTTLE AND FLIGHT OFFICERS AIRSPEED WENT TO ZERO.  ALSO, FLIGHT OFFICERS ALTITUDE STOPPED AT 1500 FEET, WE WERE CLIMBING TO 10'000.  MX REPLACED NR 2 ADC GROUND TEST OK.  SYSTEM  NOT CERTIFIED FOR CAT IIIA.  (M)


REMARKS:
FLT 1886 - ORF - AT 19,000, THERE WAS AN ACRID, ELECTRICAL ODOR, WITH VERY LIGHT SMOKE, LASTED 3 MINUTES.  DIVERTED TO ORF.  MX FOUND R-61 RELAY AT L1 TERMINAL BURNED FOR NR 1 GALLEY.  REPLACED R-61 RELAY AND L1 TERMINAL END.  OPS CHECKS NORMAL.  (M)


REMARKS:
FLT 916 - PHL - COCKPIT EMERGENCY LIGHT INOP.  MX REPLACED COCKPIT EMERGENCY LIGHT ASSY.  OPS CHECK SATISFACTORY.  (M)


REMARKS:
PHL - FL 2526 - FLIGHT RETURNED TO PHL DUE TO THE FIRST OFFICERS WINDSHIELD HEAT BEING INOPERATIVE.  MAINTENANCE COULD NOT FIND A PROBLEM.  THE WINDSHIELD HEAT WORKED PROPERLY.  (M)


REMARKS:
FLT 665 - SAV - FLIGHT DIVERTED TO SAV DUE TO RAPID DEPRESSURIZATION AT FL 330.  MAINTENANCE REPLACED THE RIGHT PRESSURE RELIEF VALVE.  OPS CHECK SAT.  (M)


REMARKS:
IMMEDIATELY AFTER TAKEOFF, FELT AND HEARD LOUD BANG TO AIRCRAFT WITH ASSOCIATED FUMES IN COCKPIT. INSTRUMENTS REMAINED NORMAL.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  FOUND EVIDENCE OF BIRDSTRIKE TO NR 1 ENGINE INLET.  PERFORMED BIRDSTRIKE INSPECTION.  NO DAMAGE NOTED.  REPLACED CSD OIL COOLER AND RIGHT WATER SEPARATOR BAG. PERFORMED ENGINE POWER ASSURANCE RUN.  ALL PER BOEING M/M.


REMARKS:
EXPERIENCED NR 1 ENGINE HIGH OIL TEMPERATURE.  CREW PERFORMED ENGINE SHUTDOWN PROCEDURES.  AIRCRAFT RETURNED TO HOU ANDMADE AN UNEVENTFUL LANDING.  TROUBLESHOT, REPLACED MAIN OIL FILTER, DE-SERVICED OIL TO PROPER LEVEL, REMOVED AND REPLACED OIL TEMPERATURE SENSOR, AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.


REMARKS:
FUEL SMELL NOTED IN FORWARD GALLEY AREA.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING.  INSPECTED CABIN ANDCARGO AREAS, CHECKED A/C PACKS AND PERFORMED ENGINE RUN, NO DEFECTS NOTED.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN BULGING AT RIVETS AFT OF BS 520C, S28L.  REPAIRED PER SWA RA 1-353-1465.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DENTED AT BS 350, S18R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 755, S23L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED LEFT SIDE AFT OF BS 727 BELOW WINDOW 7TH FROM EMERGENCY EXIT S15.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND FORWARD ENTRY DOOR LOWER HINGE CUT-OUT CRACKED.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUT-OUT CRACKED .3750 INCH FROM RADIUS.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR OUTER WEB CRACKED 1.5 INCH ON LOWER FWD SIDE.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT FWD EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED TWO PLACES IN R3 WINDOW FRAME .6250 INCH.  REPLACED PER BOEING SRM AMD S/B 737-53-1115.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FORWARD DOOR LOWER EMERGENCY EXIT LIGHTS INOPERATIVE.  REPLACED BATTERY PACK CHARGER PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUT-OUT DAMAGED ON UPPER AND LOWER EDGES.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 353, JUST BELOW S17L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING LOCATIONS:  BS 315 - 318, AT S24 AND 25L, BS 322,S18, BS 921, S19 AND 20.  BS 1088, BETWEEN 24 AND 25L, BS 1019, BETWEEN S16 AND 17R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BULKHEAD TO STRINGER CLIP SUPPORT ANGLE CRACKED AT BS 947, S22L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND ANGLE BRACKET CRACKED AT BS 727, BL ZERO, WL 154.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FASTENER HOLE CRACKS ON STRINGER SPLICES AT BS 907, S4L AND S4R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 787, S24-25R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF PANEL 3401.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB ANGLES TO SKIN CRACKED AT BS 291, ABOVE AND BELOW S11R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB TO DOOR FRAME CRACKED AT BS 333, S8R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CHAFING DAMAGE TO SKIN AT BS 371, BETWEEN S6L AND 5L.  INSTALLED REPAIR DOUBLER PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500B, BETWEEN S14L AND 15L.  INSTALLED REPAIR DOUBLER PER BOEING SRM.


REMARKS:
FLT NR 340 - JAX-ATL - AT CRUISE ALTITUDE, THE RIGHT HYDRUALIC SYSTEM PRESSURE AND QUANTITY WENT TO ZERO.  USED MANUAL GEAR EXTENSION AND ABNORMAL CHECK LIST, LANDED NORMALLY.  FOUND HOLE CHAFFED IN AUX PUMP HYDRAULIC LINE.  REMOVED AND REPLACED THE HYDRAULIC LINE AND SERVICED RIGHT HYDRAULIC SYSTEM TO PROPER LEVEL WITH SKYDROL, OPS CHECK SYSTEM WITH PRESSURE ON.


REMARKS:
ON FLT 110 - ATL-ATL - AIR RETURN, LANDING GEAR WOULD NOT RETRACT.  FOUND GEAR BYPASS HANDLE DOWN.  REPLACED RT MAIN GEAR DOOR AND LEFT GEAR DOOR BUMPER.  RESET BYPASS HANDLE, OPS CHECK NORMAL.


REMARKS:
FLT 619 - BOS-BOS - AIR RETURN, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON AFTER TAKEOFF.  REMOVED AND REPLACED BLOWN DUCT CONNECTOR, LEAK CHECK OK.  (M)


REMARKS:
AFTER TAKEOFF FOR FLT 519, ATL-ATL, AIR RETURN, WHILE EXECUTING THE 'GEAR UPLATCH CHECK', THE 'RIGHT GEAR UNSAFE' LIGHTCAME ON COUPLED WITH THE 'GEAR DOOR OPEN' LIGHT.  FOUND SPRING ON RT MAIN GEAR DOOR UPLATCH BROKEN.  REMOVED AND REPLACED SPRING GEAR DOOR AND LIGHTS.  OPS CHECK OK.


REMARKS:
ON FLT 585 - BOS-BOS - AIR RETURN, THE AIRCRAFT RETURNED FROM FLIGHT WITH GEAR DOOR WARNING LIGHT ON WITH GEAR UP.  ADJUSTED DOOR SWITCH ADJUSTMENT BOLT ON RIGHT MLG IAW MM 32-60-3.  SWUNG GEAR, OPS CHECKED NORMAL.  (M)


REMARKS:
CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION.  CREW ACCOMPLISHED ABNORMAL PROCEDURE.  LIGHT WENT OUT AFTER GEAR WAS RECYCLED.  MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR,P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1.  REFERENCE USAAF96047.


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND TWO CRACKS .5 INCH LONG EACH, STATION 1437 BETWEEN LONGERON 2L AND 4L, IN AIRCRAFT FUSELAGE SKIN.  REPAIRED WITH EXTERNAL DOUBLER PER SRM 53-04 FIG 27 USAIR EA NR 32644 AND EA NR 32647.  (M)


REMARKS:
PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND TWO CRACKS .25 INCH EACH, STATION 1437 BETWEEN LONGERON 2R AND 4R IN FUSELAGE SKIN.  INSTALLED EXTERNAL DOUBLER PER SRM 53-04 FIG 27.  (M)


REMARKS:
INT - DURING Q-4 CHECK EDDY CURRENT, FOUND TWO CRACKS .125 INCH LONG, STATION 727 STRINGER 18A LEFT FRAME.  REPLACED FRAME SECTION AND REPAIRED PER EO 5394G068.  (M)


REMARKS:
INT - DURING Q-4 CHECK EDDY CURRENT, FOUND TWO CRACKS .125 INCH LONG, STATION 727 STRINGER 18A RIGHT.  REPLACED FRAME SECTION AND REPAIRED PER EO 5394G068.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 NCH AFT ENTRY THRESHOLD 'Z' ANGLE UPPER LEG.  REPLACED UPPER LEG OF 'Z' ANGLE, REPAIRED PER SRM 51-40-3.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS AROUND NUT-PLATES SPANNING A TOTAL OF 86 INCHES, STATION 987 LBL 36 INCHES TO RBL 50 INCHES FLOOR BEAM.  REMOVED T-CAP SECTION OF FLOOR BEAM AND FABRICATED REPLACEMENT SECTION AND SPLICE BBL 36 TO RBL 50.  REPAIRED PER T/R 53-10-05C.  (M)


REMARKS:
CLT - FL 494 - AFTER TAKEOFF FROM CLT, CAPTAIN COULD NOT RETRACT LANDING GEAR.  MANUAL OVERRIDE WAS ATTEMPTED AND UNSUCCESSFUL.  NO EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD IN CLT.  THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENACNE JACKED THE AIRCRAFT AND SWUNG THE GEAR SEVERAL TIMES.  UNABLE TO DUPLICATE.  GEAR SWING CHECKS OK.  (M)


REMARKS:
CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION.  CREW ACCOMPLISHED ABNORMAL PROCEDURE.  LIGHT WENT OUT AFTER GEAR WAS RECYCLED.  MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR,P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1.  (M)


REMARKS:
FLT NR 1021 - PHL - ON CLIMB-OUT AT 2500 FEET, RIGHT ENGINE FIRE WARNING LIGHT AND BELL CAME ON.  COMPLETED ENGINE FIRECHECK LIST.  FIRE WARN LIGHT DID NOT GO OUT UNTIL ENGINE FIRE SHUTOFF HANDLE WAS PULLED.  ENGINE SHUTDOWN FOR 13 MINUTES.  MX REPLACED THE RIGHT STRUT DETECTOR, CHECKED SAT.  (M)


REMARKS:
FLT NR 2316 - RIC - NR 1 ENGINE OIL TEMP REMAINED IN YELLOW ARC FOR MAX 15 MIN RESTRICTION.  PRECAUTIONARY ENGINE SHUTDOWN COMPLETED.  MAINTENANCE REPLACED LEFT ENGINE FUEL/OIL EXCHANGER.  OPS AND LEAK CHECK OK.  (M)


REMARKS:
DCA - FL 1721 - DURING CLIMB AT APPROXIMATELY 6,000 FEET, CREW WAS UNABLE TO MAINTAIN PRESSURIZATION.  FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER.  (M)


REMARKS:
LGA - MAINTENANCE FOUND THE EMERGENCY EXIT AISLE LIGHTS, IN ROW 24 AND 25, WON'T ILLUMINATE.  MAINTENANCE REPLACED FUSEIN BATTERY PACK.  (M)


REMARKS:
PHL - MAINTENANCE FOUND THE OVERWING MID AISLE EMERGENCY LIGHT INOP.  MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERYPACK, CHECKS OK.  (M)


REMARKS:
STL - FL 2129 - AT FL 350, CREW NOTICED THE THRUST WAS BEING REDUCED BY THE AUTOPILOT, THE CAPT'S AIRSPEED WAS DEGRADING DOWNWARD WHILE THE F/O'S WAS GOING TO REDLINE.  THE CAPT TOOK CONTROL OF THE A/C, FLYING MANUALLY, AND STARTED A DESCENT.  AT FL 300 THE A/C LOST ONE PACK AND THE CABIN STARTED TO CLIMB TO 10,000 FT.  THE CREW DECLARED AN EMERGENCY AND DESCENDED TO 10,000 FT.  DURING DESCENT, OTHER PACK FAILED.  MASKS DID NOT DEPLOY.  UPON REACHING 10,000 FT, CREW CANCELLED THE EMERGENCY AND THE FLT LANDED IN MCI W/O FURTHER INCIDENT.  MX REPLACED THE NR 1 AIR DATA COMPUTER, OPERATIONAL CHECK GOOD.  ALSO RESET THE NR 1 AND 2 CABIN PRESS CONTROLLERS, OPS CHECK GOOD.  PRESSURIZED A/C, OPS CHECK GOOD.  (M)


REMARKS:
FLT 1021 - PHL - ON CLIMB-OUT AT 2500 FEET, RIGHT ENGINE FIRE WARNING LIGHT AND BELL CAME ON.  COMPLETED ENGINE FIRE CHECK LIST.  FIRE WARNING LIGHT DID NOT GO OUT UNTIL ENGINE FIRE SHUTOFF HANDLE WAS PULLED.  ENGINE SHUTDOWN FOR 13 MINUTES.  MX REPLACED THE RIGHT STRUT DETECTOR.  CHECKED SATISFACTORY.  (M)


REMARKS:
ATL - FLT 53 - NR 3 ENGINE LOW OIL PRESSURE FILTER BYPASS LIGHT CAME ON AND WOULD NOT GO OUT WITH IDLE POWER.  ALL OTHER INDICATIONS NORMAL.  ENGINE WAS SHUT DOWN.  REMOVED AND REPLACED NR 3 ENGINE LOW OIL PRESSURE BYPASS SW AS PER MM 79-31-1.  REMOVED AND REPLACED MOS FOUND LOOSE GROUND WIRE ON NR 3 ENGINE LOW PRESSURE LIGHT SOCKET ON FORWARD COCKPIT PANEL, RETIGHTENED.  ENGINE RAN UP AND LEAK CHECK OK.  (M)


REMARKS:
FLT 842 - LAX-PIT - AFTER TAKEOFF, LEVEL AT 5000 FEET, LEFT FIRE WARNING AND BELL CAME ON.  AS SOON AS CREW TURNED BELLOFF, THE LIGHT WENT OFF.  RETURNED TO LEX.  REPLACED LEFT ENGINE 13TH STAGE MANIFOLD AND SENSE LINE.  (M)


REMARKS:
FLT 311 - ATL-PHL - DIVERTED TO BWI DUE TO SMOKE IN AFT LEFT LAV AREA.  REPLACED AFT MISC LIGHT CONTROL TRANSFORMER.  (M)


REMARKS:
FLIGHT ATTENDANT NOTED AND REPORTED TO CAPT AN ODOR IN THE CABIN.  A UPS PILOT ONBOARD SUGGESTED THAT IT WAS SIMILAR TOTHAT OF AN ELECTRICAL SMELL.  CREW TURNED GASPER FAN OFF AND SMELL DISSIPATED.  THEN SMELL RETURNED, CREW DECLARED AN EMERGENCY.  AIRCRAFT LANDED AT BWI WITHOUT INCIDENT.  INSPECTED AND FOUND GASPER FAN TO BE THE FAULT, DEFERRED GASPER FANOPERATION AND CONTINUED PER MEL 21-26.  REPLACED GASPER FAN BER BOEING M/M.


REMARKS:
IN FLIGHT, NOTED NR 2 FLAP CANOE FAIRING LOOSE FROM MOUNT.  AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING.  INSPECTED, RESECURED FAIRING PIVOT BUSHING BOLT PER BOEING M/M.


REMARKS:
NUMBER 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT, THROTTLE RETARDED, NO HELP.  CREW PERFORMED ENGINE SHUTDOWN CHECKLIST.  AIRCRAFT DIVERTED AND MADE AN UNEVENTFUL LANDING AT BHM.  INSPECTED, REMOVED AND REPLACED NR 2 MAIN OIL FILTER.  FOUND MINOR CONTAMINATION, PERFORMED ENGINE RUN, REMOVED AND REPLACED OIL FILTER, NO CONTAMINATION NOTED.  ALL ENGINE PARAMETERS NORMAL.


REMARKS:
ON CLIMBOUT, EXPERIENCED BIRD STRIKE TO AREA ABOVE AND AFT OF F/O WINDOW.  AIRCRAFT RETURNED TO SJC AND MADE AN UNEVENTFUL LANDING.  PERFORMED BIRD STRIKE INSPECTION PER BOEING M/M, NO DAMAGE NOTED.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AROUND FASTENER HEAD AT BS 178, WL 234, LBL 9.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 1010, S6R.  SPLICED IN NEW SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AND GOUGED FROM BS 360 TO 380, S3L TO 6L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 382, S17L AND BS 381 BETWEEN S17L AND 16L.  ALSO, DAMAGED CREASE BEAM WEB AND OUTER CREASE BEAM CHORD AT BS 383, WL 208, LBL 70.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND O/B SIDE OF STRINGER CORRODED AT BS 907, RBL 15, WL 166, S26R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FRAME DENTED AT BS 500B S22 TO 25R, BS 400 S21 TO 25L, BS 420, S21 TO 25L, BS 480 S 21 TO 22L AND AT BS 500A 21 TO 25L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED AT BS 959 TO 990, RBL 53 TO 48, WL 209.  REPAIRED PERBOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500, RBL 33 AND RBL 26, WL 161 AND 169.  REPLACED WITH NEW SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 495, S22R.  REPLACED WITH NEW SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500A, RBL 44 AND RBL 52 TO 56, WL 168, 179 TO 177.  REPLACED WITH NEW SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHTS INOP.  REPLACED LIGHT BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND .75 INCH CRACK AT PREVIOUS REPAIR IN NOSE W/W CENTER WEB REPAIR, EXTENDING FROM UNDER RIVET HEAD.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND STRINGER 14R AT BS 1121 CRACKED.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND RT HORIZ STAB GOUGED AND DENTED AT 4 PLACES ON LOWER SURFACE, 122 TO 130 O/B FROM FUSELAGE, 10 FWD OF REAR SPAR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/4 D-CHECK, FOUND CRACK IN RADIUS OF NOSE GEAR ACTUATOR AFT SUPPORT FITTING REINFORCING GUSSET AT BS 259 NLG W/W CEILING.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED .5 INCH ON LOWER AFT ENTRY DOOR CUTOUT.  REPAIRED PER BOEING SRMAND S/B 737-53-1074.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED .25 INCH ON UPPER HINGE CUTOUT AT AFT SERVICE DOOR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND LEFT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND LT HORIZ STAB L/E DENTED 2 PLACES.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, LBL 41.5 ON HORIZ CHORD AFT FLANGE.  REPAIRED PER SWARA 1-253-1468.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOORWAY AFT FRAME CRACKED ON VERTICAL CHORD AT LOWER STOP FITTING, BETWEEN S24 AND 25R.  REPAIRED PER SWA RA 1-253-1463.


REMARKS:
JFK - DURING CHECK C-4D, FOUND A CRACK IN EAR ON VENT TUBE, STA 629, WS ABOVE RIB.  INSTALLED AND SECURED REPAIR PER SB727-57A159.  AIRCRAFT TOTAL TIME:  63,700 HOURS; 42,677 CYCLES.


REMARKS:
PIT - DURING Q-4 CHECK INSPECTION, FOUND 2 INCH CRACK IN DRAG ANGLE RADIUS RT VERTICAL STABILIZER.  DRAG ANGLE STA 1089.  INSTALLED REPAIR ANGLE PER SRM 53-05, FIGURE 23.  (X)


REMARKS:
PIT - DURING A SCHEDULED Q-2/C-6 CHECK INSPECTION, FOUND A .50 INCH CRACK IN LONGERON 17L LOWER FASTENER TO FRAME AT STA 256, VISUALLY.  SPLICED IN NEW SECTION OF LONGERON STA 230 TO STA 273 PER SRM 53-02, FIGURE 2.  (X)


REMARKS:
PIT - DURING A SCHEDULED Q-2/C-6 CHECK INSPECTION, FOUND VENTRAL DOOR JAMB RIGHT OUTBOARD FITTING CRACKED BETWEEN NR 5 AND NR 6 RADIAL.  FITTING WAS REPLACED PER 53-14-3, FIGURE 2, AND DACO DRAWING 5917579.  (X)


REMARKS:
PIT - DURING C-1 CHECK INSPECTION, FOUND A 1 INCH SKIN CRACK STA 1437, LONGERON 3L.  INSTALLED DOUBLER REPAIR 2024T-3.080 INCH PER SRM 53-04, FIGURE 27, PAGE 143.  (X)


REMARKS:
FRA - FOUND THE FLOOR EMERGENCY LIGHTING SECTION L901 INOPERATIVE.  MAINTENANCE REPLACED THE BATTERY CHARGER, PACK, ANDSEVERAL LAMPS.  ALSO, REPAIRED TWO WIRE BREAKS.  (X)


REMARKS:
CLT - ON GROUND, EMERGENCY LIGHTS ARM AND CHARGE, CIRCUIT BREAKER TRIPS.  SECURED LOOSE WIRE IN FLOOR LIGHTING, ROW 20. (X)


REMARKS:
CLT - FLT 2309 - AFTER TAKEOFF, CABIN WOULD NOT PRESSURIZE.  THE CAPTAIN LEVELED OFF AT 9,000 FEET AND RETURNED TO THE FIELD WITHOUT INCIDENT.  MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. (X)


REMARKS:
CLT - FLT 1543 - DURING CLIMB-OUT OF CLT, BOTH LAVATORY SMOKE DETECTORS ACTIVATED IN AIRCRAFT.  CAPTAIN DECLARED EMERGENCY AND RETURNED TO FIELD IN CLT.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE RT PACK OIL QUANTITY OVERSERVICED AND WATER SEPARATOR CONTAMINATED WITH OIL.  MAINTENANCE REPLACED WATER SEPARATOR BAG AND DRAINED OIL TO PROPER LEVEL.  RAN PACK.  NO SMOKE NOTED FROM PACK.  (X)


REMARKS:
EWR - FLT 1293 - AFTER ROTATION FROM LGA AT APPROXIMATELY 100 FEET, CREW SAW 5 TO 9 SEAGULLS AHEAD OF THE AIRCRAFT.  THE RIGHT ENGINE INGESTED ONE LARGE SEAGULL.  CREW ELECTED TO MAKE A PRECAUTIONARY LANDING AT EWR ALTHOUGH ENGINE PARAMETERS WERE NORMAL.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED IN EWR WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND ANDREPLACED THE FOLLOWING ITEMS ON THE RT ENGINE DUE TO BIRD INGESTION:  NR 6, NR 7, AND NR 8 FAN BLADES (DAMAGED), CSD OIL COOLER (CLOGGED) AND THE T-2 AND T-12 SENSORS (DAMAGED).  NOTE:  FAN BLADES NR 25, NR 26, AND NR 27 WERE REPLACED DUE TO REPLACEMENT OF FAN BLADES, NR 6, NR 7, AND NR 8.  (X)


REMARKS:
GSO - FLT 2338 - AFTER DEPARTURE FROM PHL AND GEAR RETRACTED, THE RIGHT MLG DOWNLOCK LIGHT REMAINED ILLUMINATED.  FLIGHT DIVERTED TO GSO AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE TROUBLESHOT SYSTEM TO A BAD DOWNLOCK SENSOR.  THE RIGHT MLG DOWNLOCK SENSOR WAS REMOVED AND REPLACED.  OPS CHECKED GOOD.  (X)


REMARKS:
STL - FLT 619 - DURING PRE-FLIGHT, EMERGENCY LIGHTS AND EGRESS LIGHTS WOULD NOT ILLUMINATE.  FOUND SWITCH HAD BEEN LEFTIN THE ON POSITION.  REPLACED BATTERY POWER PACKS, MFG PN 5822-2 AND VR4D.  EMERGENCY LIGHTS AND EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL.  CHECK C - 5-22-95 - STL.  (X)


REMARKS:
DURING OP-15, FOUND FORMER FOOT CRACKED AT AFT SIDE OF FORMER, BS 1452, STR 3R AND STR 3L.  REPAIRED PER SRM 51-11 AND TWO STANDARD PRACTICES.  AIRCRAFT TT:  37,726 HOURS; 19,564 CYCLES.  (X)


REMARKS:
DURING OP-15, FOUND CRACK IN AFTERBODY INTERCOSTAL, FS 1416, STR 10L.  REPAIRED BY STOP DRILLING AND INSTALLING DOUBLERPER SRM 53-01.  AIRCRAFT TT:  37,726 HOURS; 19,564 CYCLES.


REMARKS:
SAN - FLT 308 - ON TAKEOFF, SHUT DOWN NR 1 ENGINE, SN 1217, DUE TO LOSS OF EPR AND INCREASE IN EGT.  FOUND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL.  ENGINE TOTAL TIME:  22,736 HOURS; 11,408 CYCLES.  CHECK C-1D - 3-4-95 - MCI.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND A 2 INCH CRACK AT TOP OF CLOSURE RIB ATTACH ANGLE IN RIGHT WING, IWS 503.  REPAIRED BY INSTALLING NEW ATTACHED ANGLE PER SB 093-57-207 AND LOCKHEED DWG NR 1647070, SHEET 2.  AIRCRAFT TT:  60,229 HOURS; 22,908 CYCLES.


REMARKS:
STL - FLT 609 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RT MLG DID NOT RETRACT.  EXTENDED ALL LANDING GEARS.  FOUND RT MLG BUNGEE CYLINDER ROD END, MFG PN 3914016-5503, FRACTURED.  REPLACED BUNGEE CYLINDER AND RT MLG OPERATION CHECKED NORMAL.  CHECK C - 1-12-96 - STL.


REMARKS:
MCI - DURING SPECIAL CHECK, FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 13 AND STR 19, TOP IWS 555.  REPAIRED PER SB 093-57-207 AND SRM 51-10-01.  AIRCRAFT TOTAL TIME:  60,229 HOURS; 22,908 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK FOUND CRACKS IN TOP WING RIB CASTELLATION OF RT WING, IWS 503, STRINGERS 18, 19, AND 21.  REPAIRED PER SB 093-57-207 AND LOCKHEED DWG NR 1647070, SHEET 3.  AIRCRAFT TOTAL TIME:  60,229 HOURS; 22,908 CYCLES.


REMARKS:
MCI - DURING SPECIAL CHECK FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 9, BOTTOM IWS 555.  REPAIRED PER SRM 51-10-01.  AIRCRAFT TOTAL TIME:  60,229 HOURS; 22,908 CYCLES.


REMARKS:
STL - FLT 24 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NLG RED UNSAFE LIGHT REMAINED ILLUMINATED.  VERIFIED NLG RETRACTION BY MECHANICAL INDICATOR.  FOUND NLG PROXIMITY SENSOR, MFG PN 8-337-03, FAULTY.  REPLACED NLG PROXIMITY SENSOR.  NLG INDICATION THEN CHECKED NORMAL.  CHECK C-1D - 8-21-95 - MCI.


REMARKS:
STL - DURING PRE-FLIGHT, FOUND EGRESS LIGHTING INOPERATIVE FROM SEAT ROW 31 AND AFT.  FOUND BROKEN WIRE AND BROKEN LENSCOVER.  REPLACED WIRING MODULE, MFG PN 0105606-003, AND TRACK TOP COVER, MFG PN 0105601-003PA7.  EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL.  CHECK C-1 - 6-27-95 - MCI.


REMARKS:
JFK/PIT - FLT 721 - AFTER TAKEOFF, RETRACTING GEAR, NOSE GEAR UNSAFE LIGHT STAYED ON, AND THERE WAS A LOUD VIBRATION.  RECYCLED GEAR, DID SAME THING.  ON WALK-AROUND AFTER LANDING, FOUND RT FORWARD NOSE GEAR DOOR OPEN.  REPLACED LOCK SENSOR PROXIMITY SWITCH AND CONDUIT AND ADJUSTED CLEARANCE PER MM.  SERVICED NOSE STRUT WITH AIR AND OIL PER MM.  ALSO, ADJUSTED RT NOSE GEAR DOOR FORWARD BUNGEE TO PROPER TENSION PER MM.  (X)


REMARKS:
PIT/EWR - FLT 936 - PRIMARY TRIM DOES NOT TRIM FORWARD.  RETURNED TO FIELD.  REPLACED PRIMARY TRIM MOTOR AND TRIM BRAKERELAYS.  (X)


REMARKS:
PIT/MKE - FLT 410 - CAPTAIN'S WINDSHIELD DEVELOPED SMALL CRACK IN LOWER LEFT CORNER AND SPREAD RAPIDLY.  ARCING AND DELAMINATIONS STARTED TO FOLLOW CRACKS.  DIVERTED TO LAN.  REPLACED CAPTAIN'S WINDSHIELD.  (X)


REMARKS:
CLT/FAY - FLT 1527 - STALL INDICATION FAILURE WARNING ILLUMINATED ON DEPARTURE.  FLIGHT RETURNED TO CLT.  ON APPROACH, LIGHT EXTINGUISHED.  REPLACED LEFT AND RIGHT AOA VANES. (X)


REMARKS:
COCKPIT EMERGENCY LIGHTS INOPERATIVE.  REPLACED FORWARD BATTERY PACK.  (X)


REMARKS:
LEFT NACELLE EMERGENCY LIGHT INOPERATIVE.  REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK.  (X)


REMARKS:
LGA/RDU - FLT 1507 - ON APPROACH, FLAPS WOULD NOT GO TO 25 DEGREES WITHOUT HORN SOUNDING.  GEAR WAS DOWN.  REPLACED FLAP SWITCH S1-85.  ALSO, REPLACED DISCONNECT P1-227.  (X)


REMARKS:
RIC/CLT - FLT 761 - CABIN ALTITUDE CONTROLLER FAILED TO MAINTAIN ALTITUDE AND CLIMBED AT A HIGH RATE ABOVE 10,000 FEET. DESCENDED TO 8,000 FEET.  PERFORMED BITE CHECK ON NR 1 AND NR 2 PRESSURIZATION CONTROLLERS.  NO FAULTS FOUND.  RAN NR 1 AND NR 2 PACKS, OPS NORMAL.  (X)


REMARKS:
FORWARD AISLE EMERGENCY LIGHTS AND EXIT SIGNS INOPERATIVE.  REPLACED BATTERY PACK.  (X)


REMARKS:
ORF/CLT - FLT 1139 - TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED AT 11,000 FEET.  RETURNED TO FIELD.  RECONNECTED AIR DUCT TO RIGHT PACK.  (X)


REMARKS:
CLT - FLT 765 - CREW COULD NOT RAISE GEAR OR PRESSURIZE AIRCRAFT AFTER TAKEOFF.  FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED PINS 3 AND 4 IN CONNECTOR D4574P.  GEAR SWING ACCOMPLISHED.  (X)


REMARKS:
DURING OVERNIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING INOP BEHIND ROW 6.  RECONNECTED WIRING ON TRACK LIGHT.


REMARKS:
DIVERTED TO SPS DUE TO APU FIRE WARNING IN FLIGHT.  DISCHARGED FIRE BOTTLE.  INSPECTED AND FOUND NO EVIDENCE OF FIRE OROVERHEAT CONDITION.  DEFERRED APU FIRE DETECT SYSTEM AND FIRE BOTTLE PER MEL AND CONTINUED.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLES CRACKED ABOVE S11R AND S12R, BS 290.  REPLACED PER BOEING SRM.


REMARKS:
DURING OVERNIGHT CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP.  REPLACED LIGHT BASE PER BOEING M/M.


REMARKS:
FUEL FUMES NOTED IN CABIN AREA WHILE APU BLEED ON.  INSPECTED AND FOUND PRESSURE LINE AT ATOMIZER LEAKING.  CONTINUED WITH APU INOP PER MEL 49-1.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 847, AT S7R.  REPAIRED PER BOEING SRM.


REMARKS:
MSP - FLT 1140 - WHILE CLIMBING OUT OF MSP, CREW SMELLED AN ODOR OF UNKNOWN ORIGIN.  FLIGHT ATTENDANT WAS CALLED TO THECOCKPIT TO VERIFY ODOR.  AT THIS TIME, SMOKE WAS SEEN EMITTING FROM THE CENTER WINDSHIELD POST.  THE CREW DONNED OXYGENMASKS AND DECLARED AN EMERGENCY.  THEY TURNED OFF THE WINDSHIELD HEAT AND THE SMOKE STOPPED.  THE FLIGHT WAS 60 MILES FROM MSP AND RETURNED TO FIELD LANDING WITHOUT INCIDENT.  MX CHECKED WIRING TO LEFT WINDOW AND BENEATH GLARESHIELD AND FOUND NO EVIDENCE OF SHORTED WIRES.  OPERATED SYSTEM, CHECKS OK.  MX REPLACED THE FOLLOWING ITEMS PER PRECAUTIONARY MEASURE, LEFT WINDSHIELD TEMP CONTROLLER P/N EAWTC8803-405, LEFT WINDSHIELD TRANSFORMER P/N AE5751MK1.  USAAF96050.


REMARKS:
MCI - DURING CRUISE, SHUT DOWN NR 1 ENGINE, S/N 3208, DUE TO RAPID DETERIORATION OF ENGINE PARAMETERS.  FOUND TURBINE DAMAGE.  CHANGED ENGINE.  ENGINE OPERATION THEN CHECKED NORMAL.  (M)


REMARKS:
LAX - DURING APPROACH WHEN THROTTLES WERE RETARDED FROM HIGH POWER, NR 3 ENGINE REMAINED AT HIGH POWER REGARDLESS OF THROTTLE POSITION.  SHUT DOWN ENGINE.  REMOVED AND REPLACED FUEL FLOW REGULATOR, MFG P/N FFR101MK15.  OPERATIONAL CHECK AND ENGINE RUN NORMAL.


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A 1.5 INCH CRACK AT FRAME ATTACH BOLT, LONGERON L5, STATION 737.  REPAIRED PER SRM 53-02.


REMARKS:
STL - DURING OP-9, FOUND A .25 INCH CRACK ON ONE SIDE AND A .5 INCH CRACK ON OTHER SIDE OF UPPER AFT SKIN PANEL LEFT HORIZONTAL STABILIZER INBOARD ATTACH HOLE.  REPAIRED PER EMLR 66370.


REMARKS:
LAX - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, BOTH RED AND GREEN LIGHTS REMAINED ILLUMINATED.  CYCLED LANDING GEAR.  FOUND LOGIC CARD A8, MFG P/N 69B4753-5, IN LANDING GEAR LOGIC BOX M93, MALFUNCTIONING.  REPLACED A8 LOGIC CARD ANDLANDING GEAR INDICATION CHECKED NORMAL.  (M)


REMARKS:
DURING CRUISE EMERGENCY EGRESS LIGHTS ILLUMINATED INTERMITTENTLY.  REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2.  OPERATIONAL CHECK NORMAL.


REMARKS:
RIGHT OVERWING EMERGENCY DOOR HAS EXIT LIGHT OUT.  REMOVED AND REPLACED LAMPS.  OPS CHECK OK.  REFERENCE IXKA960034.


REMARKS:
CATERER DAMAGED 'E' PATH LIGHTING AT ROW 28 DEF.  REMOVED AND REPLACED LIGHT LENS ASSY AT 28 DEF 'E' PATH LIGHT.  GROUND CHECK OF 'E' LIGHTING OK PER MM 33-50.  REFERENCE IXKA960030.


REMARKS:
ON TAKEOFF WHEN GEAR WAS RAISED, MAIN GEARS CAME UP NORMALLY, NOSE GEAR STAYED DOWN AND LOCKED (GREEN) WITH THE RED NOSE GEAR UNSAFE LIGHT AND GEAR DOOR LIGHT OUT.  RECYCLED DOWN NORMAL GEAR DOWN AND LOCKED RAISED GEAR AGAIN W/SAME RESULTS.  LOWERED GEAR AND RETURNED FOR LANDING.  VISUALLY INSPECTED NLG DRAG BRACES TRUNNION FITTINGS, SUPPORT BULKHEAD LT/RT OVERCTR DOWN LOCK ACTUATOR TORQUE LINKS NO DISCREPANCIES NOTED, JACKED A/C PER VJ WC 0005 AND LUBRICATED NLG FITTINGS PER VJ WC 0223.  PERFORMED RET AND EXT CYCLED 5 TIMES AND EXTEND NLG EMERGENCY EXT PER MM 32-30.  (M)


REMARKS:
AFTER TAKEOFF THE GEAR DOOR OPEN AND LEFT GEAR UNSAFE LIGHT REMAINED ON AFTER RAISING THE GEAR.  LOWERED THE GEAR AND GOT AN IMMEDIATE LEFT GREEN, REMAINING TWO LIGHTS ON.  REMOVED AND REPLACED GEAR BUNGE CYLINDER PERFROMED LEAK CHECK AND GEAR SWING, OPS CHECK GOOD, NO DEFECTS.  (M)


REMARKS:
ON FLT 404 - ATL-CLT - AIR RETURN, THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF, LANDED NORMAL.  TROUBLE SHOT AND ADJUSTED DOORS PER DC MM 32-20-0.  REMOVED AND REPLACED NOSE GEAR RETRACT CYLINDER PER DC MM 32-32-6.  PERFORMED NLG EXTENT, RETRACT AND EMERGENCY EXTENSION PER DC MM 32-30-0, OPS CHECK NORMAL.  (M)


REMARKS:
AFTER RETRACTING LANDING GEAR, THERE WAS A LOUD VIBRATION.  UPLATCH CHECK GOOD.  VIBRATION AND NOISE INCREASED WITH AIRSPEED.  FOUND RIGHT FWD NOSE GEAR DOOR DOWN (DID NOT RETRACT).  NO DEFECTS FOUND.  FORWARD GEAR UPLOCK AND LOCK NORMAL ON GROUND REF MM 32-20-0.  (M)


REMARKS:
AIR RETURN RADAR PAINTS ONE LARGE SPOKE AT 10 O'CLOCK POSITION.  REPLACED RADAR INDICATOR AND NR 1 VERTICAL GYRO OPS CHECK GOOD ON GROUND.  (M)


REMARKS:
THE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON IN FLIGHT.


REMARKS:
FLT 143 - ATL-ATL - AIR RETURN, THE CAPTAIN REPORTED NO INDICATION OF NR 2 EGT GAUGE.  REPAIRED BROKEN PIN ON RIGHT EGTCONNECTOR, OPS CHECK GOOD.  (M)


REMARKS:
ON FLT 642 - ATL-SDF - AIR RETURN, THE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON IN FLIGHT.  REMOVED AND REPLACED LEAKING PERI-SEAL AT DUCT BETWEEN ACM AND FLOW CONTROL VALVE ON RIGHT PACK SYSTEM.  OPS CHECK NORMAL PER DC MM 21-20.  (M)


REMARKS:
ON FLT 157 - ATL-MSY - AIR RETURN, ON CLIMB-OUT BOTH MASTER CAUTION LIGHTS CAME ON INTERMITTENTLY, (FLICKERED DIMLY), NO OTHER INDICATION, ANNUNCIATOR LIGHTS TESTED NORMAL.  FOUND WIRE NR E204A18 CHAFED TO NR 1 ENGINE CASE, REPAIRED WIRE PER DC MM 20 STANDARD WIRING PRACTICE, OPS CHECK GOOD PER DC MM 79-33.  (M)


REMARKS:
ON FLT 230 - DFW-ATL - THE CABIN OXYGEN SYSTEM MANUALLY SURGED, OXYGEN MASKS DOORS DID NOT OPEN.  CONNECTED SUPPLY LINETO AFT FLIGHT ATTENDANT PSU AND OPERATED CABIN OXYGEN SYSTEM, ALL PSU DOORS DROPPED, OPS CHECK GOOD.


REMARKS:
ON POST FLIGHT CHECK, FOUND LEFT AND RIGHT FORWARD OVERWING EMERGENCY LIGHTS INOP.  CLEANED CONTACTS TO BOTH LEFT AND RIGHT FORWARD OVERWING LIGHTS.  OPS CHECK OK.  (M)


REMARKS:
FLT 56 - CXL - FORWARD GALLEY SERVICE DOOR (R1) WILL NOT OPEN.  FOUND LOWER GATE ASSY ON DOOR DAMAGED.  REMOVED AND REPLACED FOWARD GALLEY SERVICE DOOR (R1) LOWER GATE ASSY PER MM 52-10-10.  OP CHECK OK.  (M)


REMARKS:
CATERER DAMAGED 'E' PATH LIGHTING AT ROW 28 DEF.  REMOVED AND REPLACED LIGHT LENS ASSY AT 28 DEF 'E' PATH LIGHT.  GROUND CHECK OF 'E' LIGHTING OK PER MM 33-50.  (M)


REMARKS:
OVERWING EXIT SIGNS DIM, FORWARD RIGHT, FORWARD LEFT, AFT LEFT.  REPLACED LAMPS AT FWD RIGHT, FWD LEFT AND AFT LEFT OVERWING EXIT SIGNS.  (M)


REMARKS:
'E' PATH LIGHT LOOSE AT 4D TO 5D.  REMOVED AND REPLACED 'E' PATH FLOOR TRACK.  OPS CHECKED OK.  (M)


REMARKS:
ON POST FLIGHT INSPECTION, FOUND L1 DOOR PORTABLE EMERGENCY EXIT LIGHT INOP.  REMOVED AND REPLACED INOP BATTERY POWER PACK.  OPS CHECK OK.  (M)


REMARKS:
RIGHT OVERWING EMERGENCY DOOR HAS EXIT LIGHT OUT.  REMOVED AND REPLACED LAMPS.  OPS CHECK OK.  (M)


REMARKS:
RED COVER LENS IN TRACK FOR PATH LIGHTING NOT SECURED.  SECURED RED COVER LENS IN TRACK, OPS CHECK LIGHTS OK.  (M)


REMARKS:
CLT - INSPECTION FOUND TWO APPROXIMATELY .375 INCH CRACK BY ULTRASONIC AND EDDY CURRENT LOCATED AT STATION 727 AT STRINGER 18A RIGHT CHORD.  INSTALLED CHORD SECTION, AUX CHORD AND LOWER SPLICE PER EO NR 9394G068.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 987 LEFTSIDE TO RIGHT SIDE OF CABIN TOP OF FLOOR BEAM.  CUT OFF TOP CHORD OF FLOOR BEAM AND INSTALLED T-CAP REPAIR.  REPAIRED PER EA 4116.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS, BS 294.5 RBL 8, RBL 39, RBL 44.5 INCH FLOOR BEAM.  CUT OUT CORRODED AREA SPLICED IN FLOOR BEAM, COMPLETED REPAIR.  REPAIRED PER SRM 53-10-51 FIG 205. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED FLOOR BEAM, BS 312 LBL .5 INCH LBL 7.5 INCH LBL 21 INCH.  REMOVED CORROSION, SPLICED T-CAP AND COMPLETED REPAIR.  REPAIRED PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORRODED AREAS AROUND NUT PLATE HOLES BS 947 LBL 12 FLOOR BEAM.  INSTALLED T-CAP AND REPAIR ANGLES AND STRAPS.  REPAIRED PER SRM 51-00-53 AND EA 41119.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS BS 228 RBL 14 TO RBL 58 FLOOR BEAM.  CUT OUT CORRODED AREA FABRICATED AND INSTALLED REPAIR PARTS COMPLETED REPAIR PER SRM 53-10-51 FIG 205.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCH BY 1 INCH OF SURFACE CORROSION STATION 270 AT RBL 11, WL 208, COCKPIT ENTRANCE FLOOR SUPPORT BEAM.  CUT OUT AFFECTED AREA AND INSTALLED DOUBLER REPAIR.  REPAIRED PER SRM 51-70-12.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOT CORROSION BS 344 LBL 43 TO RBL 8 FLOORBEAM.  INSTALLED T-CAP AND REPAIR ANGLES AND STRAPS.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 294.5 RBL 48 FRAME.  INSTALLED DOUBLER, REPAIREDPER SRM 51-70-11.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 296 WL 209 RIGHT SERVICE DOORWAY FRAME.  INSTALLED DOUBLER, REPAIRED PER SRM 51-70-11.  (M)


REMARKS:
SYR - FLT 856 - LEFT MAIN GEAR LIGHT (GREEN) DID NOT ILLUMINATE WHEN GEAR EXTENDED.  FLIGHT DIVERTED TO SYR AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT DOWN LIMIT SWITCH HARNESS.  (M)


REMARKS:
SAV - OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 3-7 AND 17-20.  MX REPLACED THE APPLICABLE BATTERY PACKS.  (M)


REMARKS:
FLT NR 1846 - MCO-PIT - 'WHEEL NOT TURNING' LIGHT CAME ON AT 85 KNOTS.  REPLACED OUTBOARD RIGHT WHEEL TRANSDUCER.  (M)


REMARKS:
FLIGHT NR 8001 - CLT-GSP - RIGHT ENGINE OIL TEMP DURING CRUISE WENT TO 130 DEGREES.  WENT TO 155 DEGREES AT IDLE.  SHUTDOWN ENGINE.  REPLACED ENGINE.  (M)


REMARKS:
FLT 345 - ATL-BWI - UPON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON.  CYCLED GEAR AND CONDITION REMAINED.  RETURNED TO FIELD.  FOUND SCHRAEDER VALVE O-RING BROKEN.  REPLACED SCHRAEDER VALVE AND O-RING.  (M)


REMARKS:
FLT NR 447 - DCA-BOS - TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON DURING INITIAL CLIMB.  RETURNED TO FIELD.  REPLACED 8THSTAGE PNEUMATIC DUCT.  (M)


REMARKS:
PIT - FL 8076 - ON DESCENT INTO PIT, CREW LOWERED GEAR AND RECEIVED THREE GREEN LIGHTS WHILE BLUE LIGHTS IN GEAR HANDLEREMAINED ON AND A MFDU MESSAGE THAT READ 'LEFT LG DOWNLOCK SWITCH'.  AT 400 FEET THE THE AURAL WARNING FOR THE GEAR CAME ON.  CREW RECYCLED GEAR AND LIGHT EXTINGUISHED.  FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT MLG PRIMARY DOWNLOCK SENSOR.  (M)


REMARKS:
CLT - MX FOUND THE AFT EXTERIOR EMERGENCY LIGHTS INOP.  MAINTENANCE REPLACED THE AFT EXTERIOR POWER SUPPLY UNIT.  (M)


REMARKS:
CHA - FLT 1421 - CREW HEARD A RUMBLING NOISE FROM RIGHT PACK EN ROUTE TO MSY.  FIFTEEN MINUTES AFTER NOISE, SMOKE ALARMS WENT OFF.  CREW SHUT PACK OFF, DECLARED AN EMERGENCY AND DIVERTED TO CHA.  THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT AIRCO PACK ACM OIL SEAL FAILED.  THE RIGHT AIRCO PACK WAS REPLACED.  OPS CHECKED NORMAL.  (M)


REMARKS:
MSP - FLT 1140 - WHILE CLIMBING OUT OF MSP, CREW SMELLED AN ODOR OF UNKNOWN ORIGIN.  FLIGHT ATTENDANT WAS CALLED TO THECOCKPIT TO VERIFY ODOR.  AT THIS TIME, SMOKE WAS SEEN EMITTING FROM THE CENTER WINDSHIELD POST.  THE CREW DONNED OXYGENMASKS AND DECLARED AN EMERGENCY.  THEY TURNED OFF THE WINDSHIELD HEAT AND THE SMOKE STOPPED.  THE FLIGHT WAS 60 MILES FROM MSP AND RETURNED TO FIELD LANDING WITHOUT INCIDENT.  MX CHECKED WIRING TO LEFT WINDOW AND BENEATH GLARESHIELD AND FOUND NO EVIDENCE OF SHORTED WIRES.  OPERATED SYSTEM, CHECKS OK.  MX REPLACED THE FOLLOWING ITEMS PER PRECAUTIONARY MEASURE, LEFT WINDSHIELD TEMP CONTROLLER P/N EAWTC8803-405, LEFT WINDSHIELD TRANSFORMER P/N AE5751MK1.  (M)


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FRAME DENTED BEYOND LIMITS.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND UPPER FLANGE OF FUSE FRAME CRACKED AT BS 492, RBL 36, WL 162.  REPAIRED PER TRAMCO EWO 96-0249.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 420 AT S26L, ABOVE STRINGER CLIP.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAMES CRACKED IN RADIUS AT BS 178, WL 207, RBL 29 AND LBL 29.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED IN RADIUS AT BS 188, S16R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 344, LBL 45, WL 170.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 188, WL 207, LBL 28.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAMES CRACKED AT BS 328, RBL 54, WL 183 AND AT BS 360, RBL 55, WL 184.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 597, S17R, WL 208.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE SKIN CRACKED AT BS 178, AT S17R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM I/B CHORD CRACKED AT BS 639, RBL 65, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 380 TO 400, BELOW S19R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1104, BELOW S5L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 827, S27R, WL 155.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S26L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 727B, S9R.  REPLACED STRINGER SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 921, BETWEEN S22 AND 23R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 912 TO 921, RBL 0 TO 19, FROM S24R TO S27R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 850 TO 865, S25 TO 27R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B PLUS 2, AT S18L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRAP CRACKED AT BS 1138, S12L.  REPAIRED PER BOEING SRM AND BOEING DRAWING 65C35132.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1138, LBL 27, WL 261.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND LOWER CHORD CRACKED AT BS 1154, AT S5L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1178, LBL 4.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN PUNCTURED AT BS 1134.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN LIGHTNING STRIKE DAMAGE AT BS 354, S17 TO 18.  REPAIRED PER TRAMCO EWO 96-0279.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 135, LBL 8, WL 187.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, AT S21L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR MOPSILL CORRODED AT BS 304 TO 360, WL 208, LBL 56.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 50 TO RBL 8.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE CUTOUT.  REPAIRED PER TRAMCO 96-0270.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND I/B SIDE OF STRINGER SPLICE CORRODED AT BS 907, LBL 12, WL 166 AT S26L.  REPLACED PER BOEING SRM.


REMARKS:
AFTER TAKEOFF, CREW WAS UNABLE TO PRESSURE AIRCRAFT, RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  REPLACED PRESSURECONTROLLER AND OP CHECKED SYSTEM PER BOEING M/M.


REMARKS:
EXPERIENCED NR 1 ENGINE VIBRATION, FOLLOWED BY A/C YAWING TO THE LEFT.  N2 RED WARNING LIGHT ILLUMINATED.  ENGINE THROTTLE WAS RETARDED TO IDLE, BUT VIBRATION CONTINUED.  CREW PERFORMED ENGINE SHUT-DOWN PROCEDURES.  AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING.  REPLACED ENGINE ASSEMBLY PER BOEING M/M.


REMARKS:
ON FLT 266 - IAD-CMH - AIR RETURN, THE WEATHER RADAR BEGAN SPOKING.  REMOVED AND REPLACED RADAR R/T, SYSTEM OPS CHECKEDNORMAL.


REMARKS:
FLT NR 533 - ATL-MSY - AIR RETURN, THE FUEL HEAT LIGHT CAME ON SHORTLY AFTER TAKEOFF.  THE RIGHT FUEL TEMP WENT TO 80 DEGREES WITHIN 10 MINUTES.  THE OIL TEMP WAS 145 DEGREES FOR ONE MINUTE.  THE AVERAGE OIL TEMP WAS 130 DEGREES.  EXCEEDED120 DEGREES FOR 15 MINUTES.  REMOVED FUEL HEAT VALVE.  OIL TEMP LIMITS PER MM 77-01 PG 508.


REMARKS:
DIVERSION DUE TO APU FIRE WARNING IN FLIGHT.  FIRE BOTTLE WAS DISCHARGED.  INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION.  DEFERRED FIRE DETECT SYSTEM PER MEL, FOUND AND REPAIRED SHORTED WIRE PER BOEING M/M.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED .5 INCH LONG ON OUTER SKIN.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, AT S20R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED HD CHECK, FOUND FUSELAGE SKIN DENTED AT BS 370, S25L, AT BS 980, S22L AND AT BS 936 AT S19L.  REPAIREDALL PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 CHECK, FOUND ANGLE CRACKED ABOVE STRINGER 10R, FWD OF SERVICE DOOR, BS 290.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND FWD CARGO DOOR LOWER WEB CRACKED ORIGINATING FROM RIVET HOLE, ADJACENT TO AFT/LOWER STOP FITTING.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERM CHECK, FOUND FUSELAGE SKIN DENTED 30 BELOW CAPT WINDOW.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED BELOW CEILING HOOK.  REPAIRED PER SWA RA 1-A52-198.


REMARKS:
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 1 INCH BY 2.50 INCH CORRODED AREA BS 328, RLB 21, FLOOR BEAM CAP.  INSTALLED DOUBLER, REPAIRED PER TR 53-10-01 A.  (X)


REMARKS:
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CORROSION AT NUTPLATE ON T-CAP .50 INCH BY 1 INCH, STA 294.5 AT BL ZERO, T-CAP OF FLOOR BEAM.  REMOVED CORRODED SECTION OF T-CAP, FABRICATED AND SPLICED IN NEW SECTION PER TR 53-10-04 B.  (X)


REMARKS:
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 2.5 INCH LONG CRACK IN FUSELAGE SKIN AT LOWER AFT CORNER OF FORWARD SERVICE DOOR CUT OUT.  STOP DRILLED CRACK AND INSTALLED DOUBLER PER TR 53-10-19, REV A.  (X)


REMARKS:
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 1 INCH CRACK AT LOWER HINGE CUT OUT ON A/C AFT SERVICE DOOR SKIN.  INSTALLED FUSELAGE SKIN REPAIR AND REPAIRED PER SRM 53-30-3.  (X)


REMARKS:
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND .50 INCH CRACKED FRAME, STA 312, STR 5L.  INSTALLED DOUBLER, REPAIRED PER SRM 53-40-3, FIGURE 1.  (X


REMARKS:
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 1 INCH BY 64 INCHES OF EROSION/FRETTING CORROSION ON LT/RT KEEL BEAM BS663 - BS 727 W/W CUT OUT PANEL ATTACH FLANGES.  INSTALLED REINFORCING/CHAFE STRIPS.  REPAIRED PER EA 41139 SRM 51-10-1. (X)


REMARKS:
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND FASTENER HOLE EDGE DISTANCE OUT OF LIMITS (SHORT EDGE MARGIN) STR 18A, STA 727L, AFT LOWER HOLE.  INSTALLED REPAIR ANGLE, REPAIRED PER EA 41124.  (X)


REMARKS:
INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CREASE IN EXTERIOR DOOR SKIN 6 INCHES LONG AFT CARGO DOOR (NEAR HANDLE).  INSTALLED EXTERIOR SKIN REPAIR, REPAIRED PER TR 52-10-01 A.  (X)


REMARKS:
PIT - FLT 1297 - AT 31,000 FEET, CREW RECEIVED A PRESSURIZATION WARNING HORN ON THE AUTOMATIC SYSTEM.  CREW SWITCHED TOMANUAL PRESSURIZATION CONTROL AND DESCENDED TO 10,000 FEET.  NO EMERGENCY WAS DECLARED.  FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE CABIN PRESSURIZATION CONTROLLER (P/N 7638102) AND THE AFT CABIN PRESSURIZATION OUTFLOW VALVE (P/N 7110033).  OPERATIONAL CHECK GOOD.  REFERENCE USAASB96094


REMARKS:
CLT - FL 1405 - CREW COULD NOT RAISE GEAR USING NORMAL PROCEDURES.  ALTERNATE PROCEDURES WORKED, HOWEVER, THE TAKEOFF WARNING HORN SOUNDED.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURHTER INCIDENT.  MAINTENANCE REPLACED THE R432 AND R276 RELAYS AND PERFORMED A GEAR SWING.  REFERENCE USAASB96101.


REMARKS:
PIT - FLT 1672 - CREW COULD NOT ADVANCE THROTTLES PAST 34 UNITS DURING CLIMB.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE NR 1 THROTTLE FEEDBACK CABLES FROZEN AND BROKEN.  CABLES WERE REPLACED.  REFERENCE USAAF96057.


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 986.5 FLOOR BEAM T-CAP 44 INCH LBL.  INSTALLED STRAP REPAIR, REPAIRED PER TR 53-10-01A.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AFT ENTRY DOOR 3RD STOP FROM BOTTOM AFT END WEB.  INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH DENT BS 807 STRINGER 20R SKIN ON CARGO DOOR.  INSTALLED DOUBLER REPAIRED PER SRM 52-00-3.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 10 INCH CORRODED AREA STRINGER 27L BS 948.  CUT OUT CORRODED SECTION OFSTRINGER FABRICATED NEW SECTION AND SPLICED BACK IN, REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 9 INCH CORRODED AREA AFT CARGO BS 967-987 STRINGER 25L.  INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO 3 INCH DIAMETER DENTS IN EXT FUSELAGE SKIN BS 877-STRINGER 18R.  INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3.  (M)


REMARKS:
ROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND 2 CRACKS .875 INCH AND .125 INCH IN LENGTH AT FUSELAGE SKIN AT STRINGER16L BS 727A.  CONTAINED CRACKS AND INSTALLED DOUBLER, REPARIED PER SRM 53-30-3 FIG 1.  (M)


REMARKS:
ROA - DURING 'TRANSIT CHECK' VISUAL INSPECTION VERIFIED WITH HFEC, FOUND TWO .75 INCH CRACK IN FUSELAGE SKIN JUST ABOVESTRINGER 18L, FORWARD OF BS 787.  INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 53-30-3 FIG 6.  (M)


REMARKS:
ROA - DURING 'BX TRANSIT' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION STRINGER 27L BS 986.5.  INSTALLED DOUBLER AND STRINGER, REPAIRED PER SRM 53-10-3.  (M)


REMARKS:
LEFT NACELLE EMERGENCY LIGHT INOPERATIVE.  REPLACED BATTERY PACK.  (M)


REMARKS:
FLT 985 - BDL-TPA - WITH RIGHT GENERATOR ON MEL AND APU RUNNING FOR ELECTRICAL POWER, GOT APU OIL TEMP HI CAUTION LIGHTAT FL 350.  DESCENDED TO FL 250, AND LIGHT WENT OUT.  FLIGHT DIVERTED TO CLT DUE TO FUEL AND WEATHER CONSIDERATIONS AT NEW ALTITUDE.  FOUND COOLING PLENUM SCREEN PLUGGED.  CLEANED SCREEN.  CHECKS GOOD.  (M)`


REMARKS:
PHL - FLT 328 - CREW LOST PRESSURIZATION AT 33,OOO FEET.  CREW DESCENDED TO 10,000 FEET.  FLIGHT LANDED WITH NO FURTHERINCIDENT.  MAINTENANCE FOUND THE FORWARD CARGO DOOR SEAL LEAKING.  THE DOOR SEAL WAS REPLACED.  AIRCRAFT WAS PRESSURIZED WITH LEAK RATE CHECKING OK AND DOOR CHECKING OK.  (M)


REMARKS:
BOTH LAVATORY EMERGENCY LIGHTS INOP.  REPLACED NR 8 BATTERY PACK.  (M)


REMARKS:
FIRST CLASS FLOOR EMERGENCY LIGHTS INOPERATIVE.  REPLACED INVERTER.  (M)


REMARKS:
PIT - FLT 1297 - AT 31,000 FEET, CREW RECEIVED A PRESSURIZATION WARNING HORN ON THE AUTOMATIC SYSTEM.  CREW SWITCHED TOMANUAL PRESSURIZATION CONTROL AND DESCENDED TO 10,000 FEET.  NO EMERGENCY WAS DECLARED.  FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE CABIN PRESSURIZATION CONTROLLER (P/N 7638102) AND THE AFT CABIN PRESSURIZATION OUTFLOW VALVE (P/N 7110033).  OPERATIONAL CHECK GOOD.  (M)


REMARKS:
MCI - FL 800 - FLIGHT WAS CLIMBING OUT OF MCI WHEN THE A/C STRUCK A DUCK AT 3,500 FEET WITH THE RIGHT ENGINE.  FLIGHT RETURNED TO FIELD AS A PRECAUTIONARY MEASURE.  ALL ENGINE INDICATIONS WERE NORMAL.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE INSPECTED AIRCRAFT PER MM 5-51-201 (BIRD STRIKE INSPECTION).  FOUND THREE N1 FAN BLADES NICKED AND BENT ON NR 2 ENGINE.  DRESSED AFFECTED BLADES PER PW MM 72-00.  (M)


REMARKS:
PIT - FLT 1898 - AT APPROXIMATELY 8,000 FEET, THE NR 4 LE SLAT GREEN LIGHT CYCLED ON AND OFF AFTER FLAPS WERE RETRACTED.  CREW RECYCLED FLAPS WITH NO CHANGE.  CAPTAIN DECIDED TO RETURN TO FIELD.  FLT LANDED IN PIT WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 4 LE SLAT MID EXTEND SENSOR.  OPS CHECK OF LE INDICATION TESTED GOOD.  (M)


REMARKS:
CLT - FL 1405 - CREW COULD NOT RAISE GEAR USING NORMAL PROCEDURES.  ALTERNATE PROCEDURES WORKED, HOWEVER, THE TAKEOFF WARNING HORN SOUNDED.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURHTER INCIDENT.  MAINTENANCE REPLACED THE R432 AND R276 RELAYS AND PERFORMED A GEAR SWING.  (M)


REMARKS:
PHL - MX FOUND SECTION OF EMERGENCY LIGHTING INOP.  MX REPLACED THE NR 8 BATTERY PACK.  (M)


REMARKS:
ON FLT 230 - DFW-ATL - THE CABIN ALTITUDE ROSE TO 12000 FEET AND WAS UNCONTROLLABLE AT FLIGHT LEVEL 330 FEET, INITIATEDEMERGENCY DESCENT.  THE FLIGHT HAD BEEN IN PRECIPITATION AT 33000 FEET FOR APPROXIMATELY 30 MINUTES, CABIN ALTITUDE CONTROL WAS REGAINED AT 14,000 FEET.  PRESSURIZED THE AIRCRAFT TO 7.5 PSI AND HELD FOR 15 MINUTES.  OPS CHECKED NORMAL, REMOVED AND REPLACED PRESSURE CONTROLLER, PRECAUTIONARY.  (M)


REMARKS:
PHL - FL 945 - DESCENDING FROM 20,000 FEET, NR 1 ENGINE BEGAN BANGING SEVERELY.  CREW REDUCED POWER, PARAMETERS LOOKED GOOD.  CREW THEN ADVANCED POWER, BANGING RETURNED.  AS POWER WAS REDUCED TO IDLE, EGT CLIMBED TO RED.  NR 1 ENGINE WAS SHUT DOWN IN FLT.  TOTAL SINGLE ENGINE TIME WAS 15 MINUTES.  MAINTENANCE REPLACED THE NR 1 ENGINE ASSY PER JOB CARD.  OPERATIONAL CHECK AND LEAK CHECK NORMAL.  (M)


REMARKS:
FLT NR 8004 - FLL-PHL - AIRCRAFT FERRY FROM FLL-PHL, WOULD NOT PRESSURIZE.  DIVERTED TO MCO.  REPLACED BLOWN COUPLING AT RIGHT CAU.  REPLACED BOTH SECOND SEGMENT CLIMB SWITCHES.  CLEANED SENSE LINES AT BOTH AUGMENTATION VALVES.  (M)


REMARKS:
PIT - FLT 1672 - CREW COULD NOT ADVANCE THROTTLES PAST 34 UNITS DURING CLIMB.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MX FOUND THE NR 1 THRUST REVERSER FEEDBACK CABLES FROZEN AND BROKEN.  CABLES WERE REPLACED.  (M)


REMARKS:
DURING WALKAROUND CHECK, FOUND A 2.25 INCH FUSELAGE SKIN CRACK, RIGHT SIDE AFT OF T/E FLAP, NEXT TO BODY FAIRING.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING LOCATIONS:  BS 823, AT S26L, BS 341 AT S25R, BS 504, BETWEEN 21R AND 22R, BS 203, 4 INCHES ABOVE S23L, BS 947, AT S19L AND AT BS 891, S25R.  REPAIRED ALL PER BOEING SRM.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, S18R AND S20R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 727+8, WL 156 BL ZERO-LBL 5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D CHECK, FOUND BULKHEAD BS 178 CRACKED AT WL 218, RBL 7 TO 12, AND AT RBL 9.5 TO 12.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, LBL 7 TO 10, AND AT RBL 2 TO 31.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907+5.  REPAIRED PER BOEING SRM AND BOEING T1-A51-004.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD CORRODED AROUND FASTENER HOLES BETWEEN BS 1006 AND 1016, WL 208, UNDER WEB.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D CHECK, FOUND FLOORBEAM ANGLED CHORD CORRODED AROUND FASTENER HOLES BETWEEN BS 1006 AND 986.5, WL 208, LBL 10 TO 19.  REPAIRED PER BOEING SRM.


REMARKS:
ATL/ATL - FLT 233 - AIR RETURN, THE TAIL COMPARTMENT HIGH LIGHT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF.  CLEANED TAILVENT FLAPPER DOOR.


REMARKS:
MCI - FLT 667 - DURING CLIMB WHEN ENGINE ANTI-ICE WAS TURNED ON, A BURNING ODOR WAS NOTICED IN THE CABIN.  TURNED OFF ENGINE ANTI-ICE.  FOUND DIRTY COALESCER, MFG PN 21D10-1.  REPLACED BOTH COALESCERS.  AIR CONDITIONING SYSTEM THEN CHECKEDNORMAL.  OP-16 - 2-16-96 - TUS.


REMARKS:
DURING CHECK C-4D, FOUND A .75 INCH CRACK IN RT WING LOWER AFT END OF RIB, WS 629.  INSTALLED AND SECURED RIB REPAIR PER SRM 57-10-05, PAGES 6, 7, AND 8.  AIRCRAFT TOTAL TIME:  63,700 HOURS; 42,677 CYCLES.


REMARKS:
DURING CHECK C-4D, FOUND ATTACHED LEG BROKEN OFF STR 13, STA 656.5.  REPAIRED PER SB 727-57A159.  AIRCRAFT TOTAL TIME:63,700 HOURS; 42,677 CYCLES.


REMARKS:
DURING CHECK C-4D, FOUND A 1 INCH CRACK IN RIGHT WING LOWER FORWARD END OF RIB AT RADIUS, WS 738.5.  REPAIRED PER SRM 57-10-05.  AIRCRAFT TOTAL TIME:  63,700 HOURS; 42,677 CYCLES.


REMARKS:
DURING CHECK C-4D, FOUND RIB CRACKED AT SECOND HOLE ON BOTTOM, STA 656.5.  REPAIRED PER SRM 57-10-05, PAGE 6, FIGURE 2. AIRCRAFT TOTAL TIME:  63,700 HOURS; 42,677 CYCLES.


REMARKS:
DURING CHECK C-4D, FOUND A 1.50 INCH CRACK IN LEFT WING LOWER AFT END OF RIB, WS 656.5.  REPAIRED PER SRM 57-10-05, FIGURE 2, SHEET 3.  AIRCRAFT TOTAL TIME:  63,700 HOURS; 42,677 CYCLES.


REMARKS:
BOS/BOS - FLT 361 - ABORTED TAKEOFF, NR 2 ENGINE EGT WAS ERRATIC.  THE NR 2 ENGINE EGT GAUGE STOPS AT APPROXIMATELY 350DEGREES WHEN TAKEOFF POWER WAS APPLIED.  FOUND THE BALANCING RESISTOR OUT OF TOLERANCE.  ADJUSTED IAW MM 77-20-0, PAGE 201.  RAN ENGINES TO TAKEOFF POWER, CHECKS NORMAL.


REMARKS:
BDL - DURING CLIMB SHUT DOWN NR 1 ENGINE, S/N 1607, DUE TO FIRE WARNING ON BOTH LOOPS.  DISCHARGED FIRE EXTINGUISHER BOTTLE.  FOUND ANTI-ICE HEAT DUCT, MFG P/N 577957, RUPTURED.  REPLACED ANTI-ICE FUEL HEAT DUCT AND FIRE EXTINGUISHER BOTTLE.  ENGINE OPERATION THEN CHECKED NORMAL.  (M)


REMARKS:
HNL - ON LANDING, NR 1 HYDRAULIC SYSTEM FAILED.  REMOVED AND REPLACED NR 1 HYDRAULIC PUMP, MFG P/N 350880-7.  RAN ENGINES, OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
MCI - DURING OP-16, FOUND CORROSION ON CABIN FLOOR BEAM AT FASTENER HOLES BETWEEN CHAIR TRACKS NR 2 AND 3, FS 1153.  REPLACED SECTION PER SRM 51-01, PAGE 1 AND TWA STANDARD PRACTICES.  (M)


REMARKS:
MCI - DURING OP-15, FOUND CORROSION AROUND SCREW HOLE OF FLOOR SUPPORT TEE ANGLE, FS 1155 TO FS 1212, RBL 8.  REPLACED TEE ANGLE PER SRM 57-01.  (M)


REMARKS:
CDG - DURING CRUISE, NR 1 ENGINE SURGED AT CONSTANT THRUST.  ENGINE PARAMETERS WERE NORMAL AFTER THE SURGE.  CHECKED ENGINE INLET, EXHAUST, 3.5 BLEED VALVE SCREENS AND OIL MAGNETIC CHIP DETECTORS.  ALL CHECKS WERE NORMAL.  ADJUSTED ENGINE VANE BLEED CONTROL.


REMARKS:
MCI - DURING OP-15, FOUND CORROSION ON TOP AND BOTTOM OF FLOOR MEMBRANE, FS 1174, LBL 48 TO LBL 60.  REMOVED CORROSION PER SRM 51-10-3, INSTALLED WEB REPAIR PER SRM 53-01, FIGURE 2 AND 51-30-0, FIGURE 2.  (M)


REMARKS:
MCI - DURING CRUISE, WEATHER RADAR WOULD NOT PAINT KNOWN WEATHER.  REMOVED AND REPLACED RECEIVER/TRANSMITTER UNIT, MFG P/N 622-5132-009, AND RADAR ANTENNA, MFG P/N 622-5136-201.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
MCI - DURING CRUISE WEATHER RADAR WOULD NOT PAINT KNOWN WEATHER.  REMOVED AND REPLACED RECEIVER/TRANSMITTER UNIT, MFG P/N 622-5132-009, AND RADAR ANTENNA, MFG P/N 622-5136-201.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING CRUISE, R-1 WINDOW ARCED AND EMITTED PUFFS OF SMOKE.  TURNED OFF WINDOW HEAT.  FOUND LOOSE WIRE AT R-1 WINDOW TERMINAL.  CLEANED TERMINAL AND SECURED WIRE.  WINDOW HEAT OPERATION CHECKED NORMAL.  (M)


REMARKS:
STL - DURING CRUISE, FORWARD GALLEY OVEN OVERHEATED AND EMITTED SMOKE.  TURNED OFF OVEN.  FOUND DEBRIS AND SPILLED FOODIN OVEN, MFG P/N 5616E.  CLEANED OVEN AND OPERATION NORMAL.


REMARKS:
STL - ON TAKEOFF SHUT DOWN NR 1 ENGINE, S/N 4416, DUE TO NACELLE OVERHEAT LIGHT ILLUMINATION.  FOUND STUB DUCT ELBOW, MFG P/N LK75573, CRACKED.  REPLACED STUB DUCT.  PERFORMED HIGH POWER RUNUP, NO LEAKS NOTED, AND OVERHEAT INDICATION CHECKED NORMAL.


REMARKS:
MCI - DURING OP-15, FOUND CORROSION ON RIGHT TIEDOWN TRACK, FS 1212 TO FS 1322.  REPAIRED PER SRM 51-01, PAGE 1, ITEM C, AND TWA STANDARD PRACTICES.


REMARKS:
MCI - AFTER TAKEOFF, RIGHT MAIN LANDING GEAR DOOR DID NOT CLOSED.  CYCLED LANDING GEAR.  FOUND LANDING GEAR DOOR ACTUATOR, MFG P/N 7-3141-4, MALFUNCTIONING.  REPLACED DOOR ACTUATOR AND DOOR OPERATION AND INDICATION CHECKED NORMAL.  (M)


REMARKS:
JFK - ON LANDING APPROACH, FOLLOWING GEAR EXTENSION THERE WAS NO LEFT GEAR DOWN AND LOCKED INDICATION.  REMOVED AND REPLACED LEFT GEAR DOWNLOCK LIGHT SOCKET, MFG P/N 368-658-1881-17.  OPERATIONAL CHECK NORMAL.


REMARKS:
JFK - DURING CRUISE E6 OVEN EMITTED SMOKE.  TURNED OFF OVEN.  FOUND DEBRIS IN OVEN.  REPLACED OVEN, MFG P/N 8201-11-0000.  OVEN OPERATION THEN CHECKED NORMAL.


REMARKS:
STL - DURING PREFLIGHT, EGRESS LIGHT IN FIRST CLASS DID NOT FUNCTION PROPERLY.  FOUND POWER SUPPLY, MFG P/N 5822-2, MALFUNCTIONING.  REPLACED POWER SUPPLY AND EGRESS LIGHT OPERATION CHECKED NORMAL.


REMARKS:
STL - DURING APPROACH SHUT DOWN NR 2 ENGINE, S/N 1722, DUE TO INCREASING EGT.  ACCOMPLISHED NORMAL LANDING.  FOUND TURBINE DAMAGE AND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE.  ENGINE OPERATION THEN CHECKED NORMAL.


REMARKS:
PIT - FL 1595 - AFTER TAKEOFF, RIGHT MAIN GEAR SHOWED RED WHEN GEAR WAS RETRACTED WITH HANDLE IN UP POSITION.  CREW SELECTED OFF POSITION AND RIGHT MAIN GEAR CAME DOWN.  CREW THEN POSITIONED GEAR HANDLE TO UP POSITION AND GEAR RETRACTED BUT RED GEAR LIGHT REMAINED ILLUMINATED.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MX REPLACED THE RIGHT MAIN LANDING GEARUPLOCK ACTUATOR, UPLOCK ASSEMBLY AND UPLOCK COLLAR.  OPERATIONAL CHECK, LEAK CHECK, GEAR SWING AND FREE FALL CHECKED NORMAL.  REFERENCE USAASB96105.


REMARKS:
PHL - FLT 1868 - ON GEAR RETRACTION, RIGHT MAIN GEAR RED LIGHT STAYED ON WITH HANDLE IN UP POSITION.  CREW RECYCLED BREAKERS AND THEN THE GEAR RED LIGHT WENT OUT APPROXIMATELY TWO MINUTES LATER.  FLIGHT LANDED WITH NO FURTHER INCIDENTS.  MX REPLACED PROX CARDS M982 AND M986.  OPS CHECK PER MX MANUAL GOOD.  REFERENCE 655825029.


REMARKS:
ON FLT 537 - ATL-TPA - AIR RETURN, WEATHER RADAR HAS 'NO RETURNS' IN FLIGHT, GROUND TEST NORMAL.  REMOVED AND REPLACED R/T AND ANTENNA, OPS CHECK NORMAL PER MM 34-40.  (M)


REMARKS:
ON FLT 537 - ATL-TPA - AIR RETURN, WEATHER RADAR HAS 'NO RETURNS' IN FLIGHT, GROUND TEST NORMAL.  REMOVED AND REPLACED R/T AND ANTENNA, OPS CHECK NORMAL PER MM 34-40.


REMARKS:
ON FLT 510 - ATL-BNA - AIR RETURN, AT 20,000 FEET THE LEFT GENERATOR TRIPPED WITH A/C X-TIE LOCK OUT, RESET GENERATOR, VOLTS AND FREQS NORMAL, BUT TRIPPED AGAIN WHEN PUT ON LINE.  CHECKED LEFT ENGINE GENERATOR CABLE FROM GENERATOR TO RELAY, CHECKS OK.  RAN ENGINES PERFORMED CROSS TIE CHECK, OPS CHECK GOOD PER MM 24-20-00.  (M)


REMARKS:
DEN - FL 93 - EN ROUTE SAN AT FL 390, R1 WINDSHIELD SHATTERED.  FLIGHT DIVERTED TO DEN AND LANDED WITH NO FURTHER INCIDENT.  MX REPLACED THE WINDOW AND HEAT CONTROLLER, (P/N 6240664).  (M)


REMARKS:
LEFT NACELLE EMERGNCY LIGHT INOPERATIVE.  REPLACED BATTERY PACK.  (M)


REMARKS:
FORWARD SECTION OF FLOOR EMERGENCY LIGHTS INOP.  REPLACED BATTERY PACK.  (M)


REMARKS:
PHL - FLT 1868 - ON GEAR RETRACTION, RIGHT MAIN GEAR RED LIGHT STAYED ON WITH HANDLE IN UP POSITION.  CREW RECYCLED BREAKERS AND THEN THE GEAR.  RED LIGHT WENT OUT APPROXIMATELY TWO MINUTES LATER.  FLIGHT LANDED WITH NO FURTHER INCIDENTS.MX REPLACED PROX CARDS M982 AND M986.  OPS CHECK PER MX MANUAL GOOD.  (M)


REMARKS:
PIT - FL 1595 - AFTER TAKEOFF, RIGHT MAIN GEAR SHOWED RED WHEN GEAR WAS RETRACTED WITH HANDLE IN UP POSITION.  CREW SELECTED OFF POSITION AND RIGHT MAIN GEAR CAME DOWN.  CREW THEN POSITIONED GEAR HANDLE TO UP POSITION AND GEAR RETRACTED BUT RED GEAR LIGHT REMAINED ILLUMINATED.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MX REPLACED THE RIGHT MAIN LANDING GEARUPLOCK ACTUATOR, UPLOCK ASSEMBLY AND UPLOCK COLLAR.  OPERATIONAL CHECK, LEAK CHECK, GEAR SWING AND FREE FALL CHECKED NORMAL.  (M)


REMARKS:
DCA - FLT 1764 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT.  THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION.  FLIGHT RETURNED TO FIELD AT DCA.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RESET THE LATCH AND CIRCUIT BREAKER AND REPLACED THE AIR SENSING SQUAT SWITCH CARD M991.  PERFORMED INTEGRITY CHECK ON GEAR HANDLE SYSTEM.  OPS CHECK GOOD.  (M)


REMARKS:
DEPARTING PBI, FIRE WARNING INDICATION ON NR 3 ENGINE DURING CLIMB-OUT.  FOLLOWED CHECK LIST AND DISCHARGED BOTH FIRE BOTTLES.  DUMPED FUEL AND RETURNED TO PBI.  REPLACED FIRE LOOP AND BOTTLES.  NR 3 ENGINE FIRE WARNING LIGHT ON DURING CLIMB-OUT AGAIN.  RETURNED TO PBI.  REMOVED AND REPLACED BOTH FIRE BOTTLES LEFT AND RIGHT NR 3 ENGINE FIRE LOOP, PER MM 26-11-00, FIRST TIME.  AFTER SECOND ATB, REPLACED 2 PINS ON C/P D1498.  OPS CHECK OK PER MM 26-11-01.  REPAIRED FIRE WALL DETECTION HARNESS INSIDE NR 3 PYLON AND REPLACED FIRE WALL SENSOR AND OPS CHECK OK AS PER 26-11-01 AND MM 26-11-00.  (M)


REMARKS:
FORWARD CABIN EMERGENCY EXIT SIGN INOPERATIVE.  REPLACED EMERGENCY EXIT SIGN.  (M)


REMARKS:
ON CLIMBOUT, PRESSURIZATION FAILED IN AUTO MODE, WENT STANDBY MODE, BUT CABIN PRESSURE CONTINUED TO CLIMB.  SWITCHED TOMANUAL MODE AND DESCENDED TO 10,000 FT.  AIRCRAFT MADE AN UNEVENTFUL LANDING AT MCI.  INSPECTED AND OPERATION CHECKED PRESSURIZATION SYSTEM NORMAL PER BOEING M/M.


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND FUSELAGE SKIN GOUGED 14 INCHES BELOW AFT ENTRY.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND EXTERNAL POWER DOOR CUTOUT SKIN CRACKED AT T/E.  REPAIRED PER BOEING SRM.


REMARKS:
DURING WALKAROUND, FOUND FUSELAGE SKIN CRACKED BELOW FWD SERVICE DOOR.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE HAD 2 SKIN CRACKS AT BS 757 STRINGER 17L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AIRSTAIR DOOR FRAME CRACKED UNDER FWD UPPER STOP.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C2/C4 CHECK, FOUND OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEINGM/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 25R AT BS 947 CORRODED.  REPLACED CORRODED SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 218, LBL 7 TO 10.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR SEAL WEB CORRODED AT BS 492 AND 490, WL 166, RBL 32.  REPLACED WEB PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FLOOR SUPPORT CORRODED AT BS 504, FROM S25L TO 26R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED QD-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1024, RIGHT SIDE AT S17 AND AT BS 1064, RBL 7, WL 203.  INSTALLED REPAIR DOUBLERS PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP.  REPLACED LEFT POWER SUPPLY HOUSING PER BOEING M/M.


REMARKS:
AFTER TAKEOFF, CREW EXPERIENCED T/R ISOLATION VALVE LIGHT ILLUMINATING.  AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING.  REPLACED ENGINE ACCESSORY UNIT AND BOTH PRESSURE SWITCHES PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND ALL ENTRY SERVICE DOOR EMERGENCY EXIT LIGHT BATTERY PACKS WEAK.  REPLACED BATTERY PACKS PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT BS 756.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP IN CABIN BETWEEN ROWS 15 AND 18.  REPLACED BATTERY PACK PERBOEING M/M.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND FUSLAGE SKIN CRACKED AT BS 869, S24R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED A CHECK, FOUND AFT ENTRY DOOR UPPER HINGE SKIN CUTOUT CRACKED AT LOWER RADIUS.  REPAIRED PER SWA RA T1-A52-005.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP IN CABIN BETWEEN ROWS 4 AND 7.  RECONNECTED WIRES AND OPERATION CHECKED PER BOEING M/M.


REMARKS:
DURING PREFLIGHT, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING PREFLIGHT, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 12.  FOUND AND RECONNECTED WIRE AT SOCKET PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 294, LBL 10 AND AT RBL 35, WL 208.  REPLACED FLOOR BEAM CHORD PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 328, LBL 11, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 967, RBL 28, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, S4L AND S4R.  REPLACED BOTH PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 995, RBL 11, WL 226.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 807 AND 847, AT STRINGER 9L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK UNDER VERTICAL STRAP AT RBL 5, WL 192, BS 178.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 25L DAMAGED AT BS 967.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY FLOOR BEAM UPPER SURFACE CORRODED AT BS 344, RBL 3 TO 10.  ALSO, BS 294,294.5.  REPLACED T-CAP PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR SUPPORT ANGLE AT FWD GALLEY CORRODED AT BS 294.5.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM AT FWD GALLEY CORRODED AT BS 294.5, LBL 11 AND LBL 19.  REPLACED T-CAP PER BOEING SRM.


REMARKS:
STL - DURING OP-15, FOUND A FOUR INCH CRACK IN LONGERON 30, STATION 410 TO 412.  REPLACED LONGERON 30 PER SRM 53-02, FIGURE 15.  (M)


REMARKS:
STL - DURING OP-15, FOUND .5 INCH CRACK IN WHEEL WELL, AFT END OF KEEL BEAM AT GEAR DOOR PIN HINGE LOCKPLATE, RLMG.  REPAIRED PER SRM 53-04, FIGURE 42, SHEET 3.


REMARKS:
JFK - DURING CRUISE, SINGLE SERVING CART NR 412, OVERHEATED AND EMITTED SMOKE.  DISCONNECTED ELECTRICAL POWER.  FOUND DEFECTIVE HEATING PAD.  REPLACED SERVING CART, MFG P/N 953000-119.  NEW SERVING CART OPERATION CHECKED NORMAL.


REMARKS:
MSY - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR DID NOT RETRACT.  FOLOWED ORH PROCEDURES.  FOUNDNOSE LANDING GEAR STRUT DEFLATED AND A DEFECTIVE SCHRADER VALVE.  SERVICED NOSE LANDING GEAR STRUT WITH HYDRAULIC FLUIDAND REPLACED SCHRADER VALVE, MFG P/N B050762, AND DRY NITROGEN.  NOSE LANDING GEAR OPERATION THEN CHECKED NORMAL.


REMARKS:
STL - AFTER TAKEOFF, HAD SMOKE ENTERING CABIN.  TURNED OFF LEFT AIR CONDITIONING PACK AND SMOKE SUBSIDED.  FOUND OIL CONTAMINATION ON WATER SEPARATOR, MFG P/N 179460-8-1.  REPLACED WATER SEPARATOR, PERFORMED AIR CONDITIONING DUCT CLEANOUT. AIR CONDITIONING SYSTEM OPERATION THEN CHECKED NORMAL.  (M)


REMARKS:
STL - DURING OP-15, FOUND LONGERON 2R CRACKED, STATION 718.  REPAIRED PER SRM 52-02, FIGURE 2.  (M)


REMARKS:
STL - ON TAKEOFF AFTER LANDING GEAR RETRACTION, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED.  FOUND TARGET AND SENSOR DIRTY.  CLEANED TARGET AND SENSOR, MFG P/N 8-337-03, AND NOSE LANDING GEAR INDICATION CHECKED NORMAL.  (M)


REMARKS:
BWI - FLT 1257 - ON APPROACH TO DCA, ANTI-SKID INOP LIGHT CAME ON.  FLIGHT DIVERTED TO BWI AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT MLG STRUT HARNESS AND THE LEFT INBOARD ANTI-SKID TRANSDUCER.  OPS CHECK GOOD.  REFERENCE USAASB96113.


REMARKS:
FLT NR 38 - TPA-MDW - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.  TRIED STANDBY AND MANUAL MODE, NO HELP.  EVENTUALLYRT PACK TRIP LIGHT ON.  RESET NO HELP.  SPLIT IN DUCT PSI RT APPROX 80, LEFT 40.  NO INDICATION OF PACK TEMP RISE WITH COOL AIR BEING SELECTED FROM MIX VALVE.  AIR TURN BACK TO TPA.  OPS CHECK OF SYSTEM ON GROUND WITH SYSTEM SWITCHED TO AIR MODE,  OPS CHECK NORMAL AS PER MM 21-31-0.  (M)


REMARKS:
PIT - DURING C-4 INSPECTION, FOUND TWO .25 INCH CRACKS IN MAIN ENTRANCE STAIRWELL DOOR CUTOUT IN THE FUSELAGE SKIN BOTTOM AFT CORNER.  VISUAL EDDY CURRENT CONFIRMED.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 57A.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION, AT NUT PLATE HOLES ACROSS FLOORBEAM, LOCATED AT STATION 967.  INSTALLED NEW CHORD AND REPAIR ANGLES PER T/R 53-15-91A.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT NUT PLATE HOLES, ACROSS FLOORBEAM LOCATED AT STATION 986.5.  INSTALLED NEW CHORD AND REPAIR ANGLES AS PER T/R 53-10-05.  (M)


REMARKS:
CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION ON TOP OF FLOORBEAM LOCATED AT STATION 986.5 RBL 12 AND RBL 14.  INSTALLED NEW CHORD AND REPAIR ANGLES AS PER T/R 53-10-05.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK LOWER AFT CORNER OF PYLON SKIN ACCESS OPENING STRINGER 727L.  CUT OUT CRACK, INSTALLED FILLER AND DOUBLER.  REPAIRED PER EA 41241.  (M)


REMARKS:
FLT 1541 - PIT-ATL - AFTER TAKEOFF, NOSE GEAR UNSAFE LIGHT REMAINED ON.  NOISE INDICATED NOSE GEAR WAS STILL DOWN.  GEAR HANDLE PUT DOWN, AND NOSE GEAR INDICATION REMAINED UNSAFE UNTIL NOSE STEERING WHEEL MOVED.  THEN A THUNK WAS HEARD, AND ALL GEAR INDICATIONS GREEN.  FOUND NOSE GEAR STRUT FLAT AND LEAKING FLUID.  REPLACED NOSE GEAR STRUT SEAL. (M)


REMARKS:
CLEANING DEPARTMENT AT SRQ DEPLOYED TAILCONE AND AFT SLIDE.  SLIDE UNROLLED, BUT DID NOT INFLATE.  REPLACED SLIDE ASSEMBLY.  (M)


REMARKS:
FLT 490 - SDF-CLT - DURING DESCENT LEFT ENGINE FAILED.  13 MINUTES SINGLE ENGINE TIME.  REPLACED LEFT ENGINE.  (M)


REMARKS:
EMERGENCY LIGHT SLIDE COVER LIGHT INOPERATIVE.  REPLACED LIGHT AND INSTALLED NEW BATTERY.  (M)


REMARKS:
FLIGHT 8002 - MDT-CLT - AFTER GEAR RETRACTION, CREW NOTED WIND NOISE FROM NOSE GEAR AREA.  RETURNED TO FIELD.  FOUND CRACK IN RIGHT NOSE LANDING GEAR DOOR HINGE SUPPORT FITTING.  RELEASED FOR SERVICE PER EA 32998.  INSPECTED GLIDESLOPE ANTENNA, NO FAULTS FOUND. (M)


REMARKS:
CLT - FLT 1147 - AFTER LANDING GEAR EXTENSION, CREW HAD ONE RED LIGHT AND NO GREEN LIGHT ON THE RIGHT MAIN LANDING GEAR.  CREW RECYCLED THE GEAR AND NOTED SAME INDICATIONS.  TOWER FLYBY WAS CONDUCTED.  GEAR WAS MANUALLY EXTENDED.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MX REPLACED THE RIGHT GEAR DOWNLOCK ACTUATOR DUE TO INCOMPLETE EXTENSION.  (M)


REMARKS:
CLT - FLT 799 - ON GEAR EXTENSION, CREW RECEIVED RED GEAR DOOR LIGHT.  CREW RECYCLED THE GEAR TWICE WITH SAME INDICATION.  GEAR WAS MANUALLY EXTENDED AND TOWER FLYBY CONDUCTED.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE DOOR UP STOP LOOSE AND ADJUSTED IT.  THE GEAR DOWN SEQUENCE VALVE WAS REPLACED AS A PRECAUTION.  (M)


REMARKS:
MCI - FLT 1193 - UPON GEAR EXTENSION, CREW RECEIVED NOSE GEAR GREEN LIGHT AND THEN THE LIGHT EXTINGUISHED.  ALL OTHER GEAR INDICATION WERE EXTINGUISHED.  CREW PERFORMED ALTERNATE GEAR EXTENSION PROCEDURE AND TWO TOWER FLY BYS.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MX REPLACED THE LANDING GEAR INDICATOR.  (M)


REMARKS:
BWI - FLT 1969 - CREW REPORTED, THAT AFTER STOWING AN OXYGEN MASK, A FOUL ODOR WAS DETECTED IN THE CABIN AND COCKPIT.  A DECISION WAS MADE TO RETURN TO FIELD AT BWI.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE REPLACED CONNECTOR D4074J WHERE TWO PINS WERE FOUND SHORTED.  (M)


REMARKS:
TPA - FLT 984 - AFTER TAKEOFF, CAPTAIN WAS UNABLE TO PRESSURIZE AIRCRAFT.  FORWARD ENTRY DOOR WAS NOT SEALING PROPERLY IN CLOSED POSITION.  FLIGHT RETURNED TO FIELD AT TPA.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE CHECKED AND OPERATED FORWARD ENTRY DOOR SEVERAL TIMES.  OPS CHECK NORMAL.  LUBED DOOR SEAL AS PRECAUTION.  CHECKED PROXIMITY SWITCH.  OPS CHECK NORMAL.  (M)


REMARKS:
BWI - FLT 1257 - ON APPROACH TO DCA, ANTI-SKID INOP LIGHT CAME ON.  FLIGHT DIVERTED TO BWI AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT MLG STRUT HARNESS AND THE LEFT INBOARD ANTI-SKID TRANSDUCER.  OPS CHECK GOOD.  (M)


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY DOOR,  INNER FRAME SKIN CRACKED BELOW LOWER HINGE.  REPLACED FRAME ANGLE PER BOEING SRM.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND RT WING LOWER SKIN AT NR 6 SLAT CRACKED JUST O/B OF PREVIOUS REPAIR AND A CRACK AT EXTREME O/B END OF SLAT.  REPAIRED PER SWA RA 1-357-259 AND BOEING DRAWING 65C30133.


REMARKS:
FLT NR 24 - MCO-MDW - DIVETED TO ATL AFTER 'A' SYSTEM HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO IN FLIGHT.  FOUND HYDRAULIC MOTOR SHAFT SEAL BLOWN ON RIGHT OUTBOARD FLAP POWER UNIT.  REMOVED AND REPLACED RIGHT FLAP POWER UNIT HYDRAULIC MOTOR AND OPS CHECK OK, NO LEAK AS PER MM 27-51-62.  REMOVED AND REPLACED NR 1 ENGINE 'A' SYSTEM HYDRAULIC PUMP AND CASEDRAIN FILTER PRECAUTIONARY AS PER MM 29-11-33 AND 29-11-41 AND REMOVED AND REPLACED NR 2 ENGINE HYD PUMP AND CASE DRAINFILTER PRECAUTIONARY PER ABOVE MM REF.  (M)


REMARKS:
LAX - FLT 125 - RETURNED FROM FLIGHT ACCOUNT NR 3 ENGINE SPOOLED DOWN.  FOUND GEAR TEETH PIECES ON CHIP DETECTORS.  REPLACED ENGINE S/N 4499.  ENGINE TOTAL TIME:  40,097 HOURS.  CYCLES, 13,983.  CHECK C-5C - 8-12-94 - MCI.  INVESTIGATION INTO ENGINE S/N 4499 SPOOLING DOWN REVEALED, FUEL CONTROL UNIT AND HIGH PRESSURE TACHOMETER DRIVE IDLER GEARSHAFT, MFG PNLK77389, TEETH SHEARED OFF AT ROOT.  ENGINE S/N 4499 WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
TWO AREAS OF CORROSION ON SEAT TRACK UPPER FLANGE AT NUT CLIP AREA FOR FLOORBOARDS.  REMOVED SECTION OF SEAT TRACK AND INSTALLED A NEW SECTION OF SEAT TRACK PER SRM 51-72-10, P. 1.  TST:  20,963.17 HOURS.  CYCLES 8,396.  (X)


REMARKS:
DURING SCHEDULED A-CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING WALK-AROUND, FOUND EMERGENCY EXIT LIGHTING WIRES BROKEN, 4 WHITE LIGHTS INOP AT ROW FWD OF OVERWING EXIT.  REPAIRED AND OP CHECKED PER BOEING M/M.


REMARKS:
DURING WALK-AROUND, FOUND SIX WHITE EMERGENCY TRACK LIGHTS INOP.  INSPECTED AND FOUND WIRE PULLED FROM LIGHT ASSEMBLY AT ROW 18.  REPAIRED AND OP CHECKED PER BOEING M/M.


REMARKS:
DURING WALK-AROUND, FOUND FLOOR TRACK LIGHTING LOOSE AT MID CABIN AREA.  REPAIRED AND OP CHECKED PER BOEING M/M.


REMARKS:
DURING WALK-AROUND, FOUND FLOOR TRACK LIGHTING INOP AT LEFT OVERWING EXIT.  FOUND BROKEN WIRE.  REPAIRED AND OP CHECKEDPER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CORROSION ON KEEL BEAM AT BS 500 PLUS 2, LBL 8, WL 149.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 199.5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 200, LBL 4.7.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318, RBL 43, WL 173.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, BL 0, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CREASE AT BS 480, S28L TO 29L, WL 264.  INSTALLED REPAIR DOUBLER PER BOEING SRM.


REMARKS:
AFTER TAKEOFF, NUMBER 1 L/E SLAT WOULD NOT RETRACT.  AIRCRAFT RETURNED TO MCO AND MADE AN UNEVENTFUL LANDING.  REPLACEDSLAT ACTUATOR AND LEAK CHECKED PER BOEING M/M.


REMARKS:
EN ROUTE, EXPERIENCED UNCOMMANDED YAW INPUT AFTER TAKEOFF.  CREW CONTINUED AND LANDED WITHOUT INCIDENT AT OAK.  REPLACED YAW DAMPER AND RUDDER PCU PER BOEING M/M.


REMARKS:
EN ROUTE, NUMBER 1 ENGINE START VALVE LIGHT ILLUMINATED.  PERFORMED ENGINE SHUTDOWN AS PRECAUTIONARY.  LANDED WITHOUT INCIDENT AT HOU.  REPLACED ENGINE START PRESSURE SWITCH,  START VALVE AND OPERATION CHECKED PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED .125 INCH.  REPAIRED PER TYPICAL REPAIR NR T1-A52-005.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND UPPER FUSELAGE SKIN CREASED AT BS 1152, BETWEEN S5 AD 6R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND BELT FRAME CRACKED AT LEFT SIDE OF APU COMPARTMENT, BS 1100 TO 1106.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY FLOOR BEAM T-CAP CORRODED AT BS 312 BL 0.  REPLACED T-CAP PER TYPICAL REPAIR TI-353-012.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 16, 20, 22, 24, 26, 32 AND 36.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND WEB CORROSION AROUND NUTPLATE AT BS 1000, RBL 44.  REPLACED WEB PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND Z-ANGLE CORROSION AT AFT GALLEY DOOR BETWEEN BS 990 TO 927.  REPLACED ANGLE PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT LOWER FLANGE CRACKED AT BS 813, LBL 17, WL 156.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 639, S15L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CRACKED AT BS 344, S10R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 470 BETWEEN S23 AND 22L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERMINAL CHECK, FOUND AFT CEILING EMERGENCY EXIT LIGHT SIGN INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EXIT LIGHT INOP.  REPLACED BATTERY CHARGER PER BOEING M/M.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT BS 294, 8 INCHES ABOVE FLOOR LEVEL.  REPAIRED PER TYPICAL REPAIR AND BOEING SRM.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND FWD SERVICE DOOR WEB ON FWD SIDE OF LOWER SUPPORT CASTING CRACKED.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED A-CHECK, FOUND EMERGENCY LIGHT AT AFT SERVICE DOOR INOP.  REPLACED AND OP CHECKED PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION IN AND AROUND FWD FLANGE AT RBL 15 AND 45, BS 986.5.  REPAIREDPER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION AT UPPER FLANGE, BS 294, LBL 1, 8 AND 11.  REPAIRED PER BOEINGSRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND UPPER AND LOWER SURFACES OF FLOOR BEAM UPPER T-CHORD AFT FLANGE CORRODED, BS 312, LBL 1.  REPAIRED PER BOEING SRM.


REMARKS:
DURING WALKAROUND CHECK, FOUND FUSELAGE SKIN CRACKED NEAR WATER SERVICE PANEL.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS ABOVE OVERWING EXITS INOP.  REPLACED BATTERY PACK AND POWER SUPPLY PER BOEING M/M.


REMARKS:
DURING WALKAROUND CHECK, FOUND FLOOR EMERGENCY LIGHTS AT ROW 16 INOP.  REPAIRED WIRE TO CONNECTOR AT LIGHT PER BOEING M/M.


REMARKS:
STL - FLT 661 - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED.  REMOVED AND REPLACED EMERGENCY EGRESS LIGHT POWER SUPPLY, MFG PN 5822-2.  OPERATIONAL CHECK NORMAL.  CHECK C - 8-27-95 - STL.


REMARKS:
SLC - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO COMPRESSOR STALLS.  FOUND METAL PARTICLES IN ENGINE BLEED AIR DUCT ANDCAPS.  CHANGED ENGINE.  ENGINE OPERATION THEN CHECKED NORMAL.  (M)


REMARKS:
ON FLT 537 - ATL-TPA - AIR RETURN, WEATHER RADAR HAS 'NO RETURNS' IN FLIGHT GROUND TEST NORMAL.  REMOVED R/T AND ANTENNA, OPS CHECK NORMAL PER MM 34-40.  (M)


REMARKS:
OFN FLT 396 - ATL-RDU - THE PRIMARY TRIM STOPPED WORKING APPROXIMATELY 5 MINUTES AFTER TAKEOFF.  REMOVED AND REPLACED THE PRIMARY TRIM BRAKE RELAY, OPS CK IAW 27-40.  (M)


REMARKS:
ON FLT 498 - ATL-PHF - GATE RETURN, THE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON DURING TAXI.  REPLACED LEAKING SLIP JOINT SEAL.  (M)


REMARKS:
THE LEFT ACM OVERHEATED AND FILLED THE CABIN WITH SMOKE, EVACUATED THE AIRCRAFT AT THE GATE.  REMOVED AND REPLACED LEFTACM, IAW MM 21-50-2, OPS CHECK GOOD.  (M)


REMARKS:
LEFT ACM OVERHEATED, FILLED CABIN WITH SMOKE, EVACUATED AIRCRAFT.  AIRCRAFT WAS AT GATE.  SECURED SENSE LINE ON LEFT FLOW CONTROL VALVE, OPS CHECK GOOD.  (M)


REMARKS:
THE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON IN FLIGHT.  (M)


REMARKS:
ON FT 396 - ATL-RDU - THE TAIL COMPARTMENT HIGH LIGHT CAME ON APPROXIMATELY 4-5 MINUTES AFTER TAKEOFF.  FOUND A/C TEMP HIGH SENSOR LEAKING AIR, REMOVED AND REPLACED THE TEMP SENSOR AND SEAL PER MM 36-00.  OPS CHECK AND LEAK CHECK OK.  (M)


REMARKS:
ON FLT 404 - ATL-CLT - AIR RETURN, THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF, LANDED NORMAL.  TROUBLESHOT AND ADJUSTED DOORS PER DC MM 32-20-0.  REMOVED AND REPLACED NOSE GEAR RETRACT CYLINDER PER DC MM 32-32-6.  PERFORMED NLG EXTENT, RETRACT AND EMERGENCY EXTENSION PER DC MM 32-30-0, OPS CHECK NORMAL.  (M)


REMARKS:
DURING C-CHECK, FOUND TEMPORARY REPAIR INSTALLED ON LEFT SIDE OF FUSELAGE FS 242 AT LONGERONS 17 AND 18, ALSO FINGER DOUBLER CRACKED SAME AREA.  REMOVED TEMPORARY REPAIR, FABRICATED AND INSTALLED PERMANENT REPAIR TO PLATING AND FINGER DOUBLER IAW EA 12-5304-29-C0918R1.  (M)


REMARKS:
DURING C-CHECK, FOUND CORROSION ON AFT SIDE OF FLOOR FRAME F/S 965 AT LONGERONS 23 TO 30 LEFT.  REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS, FABRICATED FRAME AND SPLICE REPAIRS IAW SRM 53-03 AND HEAT TREATED IAW SRM 51-10-2A.  INSTALLED REPAIR IAW SRM 51-30-2 PARA 1-12 FIG 1-23 AND 53-03 PARA 1 FIG 1-7.  (M)


REMARKS:
DURING 'A' CHECK, FOUND CRACK IN LEFT WHEEL WELL AT STATION 718 ON FRAME FITTING ABOVE TRAPIZOID PANEL.  REMOVED STATION 718 FRAME, INTERCOSTALS AND SEAT TRACK IAW DC-9 SB 53-131.  INSTALLED NEW FRAME AND ATTACHMENTS DRILLED HOLE IAW DC-9 SRM 51-10-4.  INSTALLED FASTENERS IAW DC-9 SRM 51-30-5, 51-30-2, 51-30-8 AND 51-30-1.  SPLICED IN SEAT TRACK IAW DC-9 SRM 53-05 FIG 4.  INSTALLED MAIN FRAME AND INTERCOSTALS.  (M)


REMARKS:
EMERGENCY FLOOR LIGHTING INOP, WINDOW EXIT.  FOUND BATTERY PACK TILTED IN MODULE.  RESECURED AND CHARGED PER MM 33-30-22.  (M)


REMARKS:
RIGHT SIDE AFT EMERGENCY LIGHT EXTERIOR INOP.  REMOVED AND REPLACED POWER PACK, OPS CHECK OK.  (M)


REMARKS:
CEILING EMERGENCY LIGHT AFT GALLEY AREA NEEDS REWIRING.  INSTALLED EMERGENCY LIGHT PER MM 33-50-01, ALL LIGHTS CHECKED OK.  NO CHAFED OR VISIBLE WIRES.  EMERGENCY LIGHTS OK.  (M)


REMARKS:
RED FLAGS ARE SHOWING AT PSU 29 AND 30 DEF NEEDS TO BE REPACKED.  REPACKED 29 AND 30 DEF PSU PER MM 35-21-42.  (M)


REMARKS:
EMERGENCY FLOOR LIGHTING IS OFF TRACK BY AFT GALLEY AND WIRES ARE EXPOSED.  REINSTALLED AND RESECURED.  (M)


REMARKS:
OVERHEAD EMERGENCY LIGHT, BY AFT GALLEY, FELL OFF.  RESECURED EMERGENCY LIGHT BY AFT GALLEY AREA.  (M)


REMARKS:
AFT CENTER CABIN EMERGENCY EXIT LIGHT INOP.  REPLACED AFT CENTER CABIN EMERGENCY EXIT LIGHT PER MM 33-50-91.  (M)


REMARKS:
FORWARD PASSENGER OVERHEAD EMERGENCY LIGHT INOP.  REMOVED AND REPLACED POWER PACK ASSY AND OPS CHECK OK AS PER MM 33-50-51.  (M)


REMARKS:
AFT EMERGENCY FLASH LIGHT INOP.  REMOVED AND REPLACED BATTERY.  OPS CHECK OK.  (M)


REMARKS:
RIGHT FORWARD OVERWING EMERGENCY LIGHT INOP.  REMOVED AND REPLACED BATTERY PACK AND OPS CHECK PER MM 33-50-71.  (M)


REMARKS:
LEFT FORWARD OVERWING EMERGENCY LIGHT INOP.  TROUBLESHOT SYSTEM AND FOUND CONTACTS CORRODED, CLEANED CONTACTS AND OPS CHECK OK.  (M)


REMARKS:
AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP.  REMOVED AND REPLACED NICAD BATTERY CELLS.  OPS CHECK OK.  (M)


REMARKS:
AFTER TAKEOFF AT ATL, FLT 73, ATL TO MCO, AIR TURN BACK DUE TO UNABLE TO PRESSURIZE ON DEPARTURE IN AUTO OR MANUAL.  TROUBLESHOT PRESSURIZATION TO INTERMITTENT FLOW CONTROL VALVE.  REMOVED AND REPLACED FLOW CONTROL VALVE PER MM 36-12-11.  PRESSURIZED A/C PER MM 21-30-00.  OPS CHECK OK.  (M)


REMARKS:
FORWARD EMERGENCY CEILING LIGHT OUT.  REMOVED BATTERY AND CLEANED CONTACTS INSTALLED BATTERY PACK, OPS CHECK OK AS PER MM 33-50-01.  (M)


REMARKS:
FORWARD 'E' PATH LIGHT INOP.  REPAIRED BROKEN WIRE TO LIGHT, CHECK OK AS PER MM 33-50-01.  (M)


REMARKS:
EMERGENCY LIGHT INOP AT ROW 20.  REMOVED AND REPLACED EMERGENCY LIGHT BULB AND LENSE.  OPS CHECK OK.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREAS OF CORROSION STATION 986.5 FLOOR BEAM UPPER CHORDLBL 45 TO RBL 45, WL 208.  REPAIRED PER EA 41219.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 26 INCH CORROSION, STATION 947 FLOOR BEAM RBL 13 INCHES TO LBL 13 INCHES, WL 208.  FABRICATED PER EA 41220.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRSION AT FRAME AROUND AFT CARGO DOOR CUT OUT BS 787PLUS 8 INCHES, STRINGER 25R.  CUT OUT SECTION OF FRAME AND INSTALLED REPAIR.  REPAIRED PER SRM 53-00-07 FIG 201.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 312 RBL 8 THROUGH LBL 8.  INSTALLED NEW SECTION OF UPPER CHORD, REPAIRED PER SRM 53-10-51 FIG 205.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 344 LBL 21 THROUGHRBL 9.  INSTALLED NEW SECTION OF T-CAP, REPAIRED PER TR 53-10-03.  (M)


REMARKS:
INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREAS OF CORROSION STATION 328 FLOOR BEAM UPPER CHORD AT NUT PLATE HOLES RBL 13 TO RBL 58.  CUT OUT DAMAGED CHORD AND SPLICED IN NEW SECTION PER TR 53-10-03.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.  (M)


REMARKS:
FLT 81 - TPA-ATL - AFTER GEAR RETRACTION, NR 1 ENGINE SHUT DOWN.  RETURNED TO TPA.  FOUND FUEL PUMP SHAFT SHEARED.  REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL AS PER MM 73-11-01 PG 401-408 AND MM 73-21-2, PAGE 401-405.  INSPECTED, RANENGINE AND OPS CHECK OK.  ALL INDICATIONS OK.  (M)


REMARKS:
FLT 476 - ELM-PIT, AFTER TAKEOFF, NR 2 ENGINE OIL QUANTITY STARTED TO DECREASE APPROXIMATELY 2 QUARTS/ 10 SECONDS.  QUANTITY STAYED AT 3 QUARTS.  RETURNED TO FIELD.  ENGINE OIL QUANTITY CHECKED AND FOUND FULL.  AIRCRAFT RELEASED PER MEL 79-3.  REPLACED THE NR 2 OIL QUANTITY TRANSMITTER.  (M)


REMARKS:
ATL/MCO - FLT 505 - WITH GEAR EXTENDED NO GREEN LIGHT INDICATION, RECYCLED GEAR AND LIGHT CAME ON DURING APPROACH.  FOUND MICROSWITCH CONNECTOR HALF WAY OUT, RECONNECTED AND CLEANED CANNON PLUG PER MM 32-60-1.  REMOVED SWITCH AND MANUALLY PERFORMED SATISFACTORY OPS CHECK.


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND LEFT AFT FUSE SKIN DENTED AFT OF AFT ENTRY DOOR, JUST BELOW EMERGENCY EXIT LIGHT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND FWD CARGO DOOR CUTOUT GOUGED BEYOND SRM LIMITS.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND LOWER FUSELAGE SKIN CRACKED FWD OF DME ANTENNA CUTOUT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C4 CHECK, FOUND A .25 INCH CRACK ON BELTFRAME TO SKIN SHEAR TIE AT BS 1104, BETWEEN STRINGERS 12 AND 13L AT LEFT SIDE OF APU.  REPLACED SHEAR TIE PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED IN RADIUS CHORD ON LEFT SIDE AT WL 195 TO 196.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM TO SIDEWALL SUPPORT PLATE CORRODED AT BS 847 TO 947.5, RBL 21.  REPAIRED PERBOEING SRM.


REMARKS:
AT GATE, HAD BURNT SMELL IN COCKPIT.  BATTERY CHARGER C/B TRIPS AND WOULD NOT RESET.  REPLACED CHARGER PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AND CHAFED AT BS 711, BL 0, WL 150.  REPLACED WEB AT BS 711, BL 0, WL 150 PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 947.5, RBL 22, WL 178.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STRINGER 23 TO 25R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SUPPORT BRACKET CRACKED AT BS 947, BETWEEN S24 AND 25L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 747, S18R AND AT S20R.  REPLACED BOTH PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED AT WL 219, RBL 11.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND 8 CRACKS AT BS 178 PRESSURE WEB BETWEEN WL 190 AND 201, LBL 4.7.  REPAIRED PER BOEING SRM.


REMARKS:
AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT.  AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND NOSE GEAR MAIN ACTUATOR HYD HOSE LEAKING.  REPLACED PER BOEING M/M.


REMARKS:
STL - FLT 134 - DURING CRUISE, LEFT ENGINE HYDRAULIC PUMP FAILED.  AIRCRAFT RETURNED TO AIRPORT.  REMOVED AND REPLACED LEFT ENGINE HYDRAULIC PUMP DUE TO A SHEARED SHAFT, MFG PN 566411L5666.  OPERATIONAL CHECK NORMAL.  OP-16 - 4-8-96 - TUS.


REMARKS:
HOU - FLT 639 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED.  CYCLED LANDING GEAR.  FOUND BROKEN WIRE AT NOSE LANDING GEAR DOWNLOCK SENSOR.  MADE AIRWORTHINESS REPAIR TO WIRING.  NOSELANDING GEAR INDICATION THEN CHECKED NORMAL.  CHECK C - 6-2-96 - STL.


REMARKS:
AFTER TAKEOFF, NR 1 T/E FLAP TRANSIT LIGHTS (FWD AND OVERHEAD) REMAINED ILLUMINATED.  AIRCRAFT RETURNED TO PHX AND MADEAN UNEVENTFUL LANDING.  INSPECTED AND REPAIRED BROKEN GROUND LUG WIRE PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 470, BETWEEN S23 AND 22L.  INSTALLED DOUBLER REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986, RBL 5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND CHORD CRACKED AT BS 178 BULKHEAD AT LBL 5.7.  REPAIRED PER BOEING SRM AND T1-253-031.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND WEB UNDER AFT GALLEY CORRODED AROUND NUTPLATE AT BS 1000, RBL 44.  REPLACED WEB PERBOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, ANGLE BELOW S13R FORWARD OF FORWARD SERVICE DOOR CRACKED AT AFT END.  REPLACED ANGLE PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 26R CORRODED AT BS 1006.  REPLACED STRINGER SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND FUSELAGE SKIN CRACKED 8 INCHES BELOW BS 1183.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B/C1 CHECK, FOUND FORWARD GALLEY DOOR UPPER AND LOWER HINGE CUT-OUTS CRACKED .25 INCH.  REPAIRED PER SWA RA 1-352-0251.


REMARKS:
DURING WALKAROUND CHECK, FOUND FORWARD ENTRY FRAME CRACKED.  REPAIRED PER BOEING SRM.


REMARKS:
AFTER TAKEOFF, WHEN GEAR RETRACTED, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED.  RECYCLED GEAR AND RECEIVED SAME INDICATION.  VISUALLY CHECKED NOSE GEAR, UP AND LOCKED. LANDED AT STL WITHOUT INCIDENT, ADJUSTED NLG DOOR LINKAGE AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.


REMARKS:
DURING SCHEDULED B2 CHECK, FOUND FRAME-TO-FRAME INTERCOSTAL CRACKED AT BS 277, AT S14R.  REPLACED FRAME PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 234, RBL 10 AROUND FASTENER HEAD.  INSTALLED DOUBLER REPAIR PER BOEING SRM.


REMARKS:
AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT.  RECYCLED GEAR, NO HELP.  RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND FOUND HYDRAULIC FLUID AROUND SWIVEL.  REMOVED AND REPLACED RETRACT LINE TO LOCK ACTUATOR, RESERVICED SYSTEM, AND RETRACTION TESTED NOSE GEAR PER BOEING M/M.


REMARKS:
PIT - DURING C-4 CHECK, FOUND 1 INCH LENGTH CRACK EXTENDING THROUGH RIVET AT FORWARD AIRSTAIR CUT OUT, BOTTOM FORWARD CORNER, STATION 160.  INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 57A.  (M)


REMARKS:
PIT - DURING UNSCHEDULED MAINTENANCE, FOUND CRACK IN FUSELAGE SKIN, LEFT SIDE 23 INCHES LONG AT STATION 600-623 AT STRINGER 17.  INSTALLED DOUBLER PER EO 5393L023 AND EA 33032.  (M)


REMARKS:
PIT - DURING UNSCHEDULED MAINTENANCE, FOUND CRACK IN FUSELAGE SKIN RIGHT SIDE 19 INCHES LONG AT STATION 600-619 STRINGER 58.  INSTALLED DOUBLER PER EO 5393L023 AND EA 33032.  (M)


REMARKS:
FORWARD EMERGENCY LIGHTS INOPERATIVE.  REPLACED FORWARD BATTERY PACK.  (M)


REMARKS:
FLT 912 - FLL-CLT - DURING CLIMB, CREW HEARD A LOUD BANG AND NOTICED POWER LOSS FROM RIGHT ENGINE.  SHUT DOWN ENGINE.  REPLACED RIGHT ENGINE.  (M)


REMARKS:
FLT 765 - CLT-MSY - ON CLIMB, WHEEL WELL OVERHEAT CIRCUIT BREAKER POPPED.  RETURNED TO FIELD.  REPLACED CIRCUIT BREAKER.  (M)


REMARKS:
FLT 1796 - MCI-BOS - RIGHT SYSTEM HYDARULIC FLUID QUANTITY DECREASING IN FLIGHT.  DIVERTED TO CMH.  FOUND BAD SEAL ON RUDDER CONTROL SHUTOFF VALVE FITTING.  REPLACED SEAL.  SERVICED HYDRAULIC SYSTEM.  (M)


REMARKS:
FLT 1148 - PIT-BGM - ON CLIMB, EXTREME VIBRATION CAME FROM TAIL.  RETURNED TO FIELD.  FOUND AIR CONDITIONING DUCT BLOWNOFF THE COOLING AIR TURBINE.  REATTACHED DUCT.  (M)


REMARKS:
FLT 1258 - PIT-CAK - ON TAKEOFF, GEAR DOOR OPEN LIGHT CAME ON.  AFTER GEAR RETRACTION, DOOR OPEN LIGHT WENT OUT AND LEFT UNSAFE LIGHT CAME ON.  CYCLED GEAR, AND UNSAFE LIGHT REMAINED ON.  RETURNED TO FIELD.  FOUND HYDRAULIC LINE FROM HANDPUMP IN LEFT WHEEL WELL WEDGED BETWEEN LEFT GEAR DOOR AND UPLOCK ASSEMBLY.  RE-ATTACHED LINE.  OPS CHECKS GOOD.  (M)


REMARKS:
EMERGENCY LIGHTS HAVE FAINT GLOW IN CEILING COMPANION WAY AND FIRST CLASS.  REPAIRED SHORTED WIRE AT AFT COMPANION WAY EMERGENCY LIGHT, AND REPLACED POWER SUPPLY B5-24.  (M)


REMARKS:
EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER POPPED ON LANDING, WOULD NOT RESET.  REPAIRED TWO CHAFED WIRES ABOVE RIGHT LAV CEILING.  (M)


REMARKS:
FLT 1200 - DCA-PVD - SLAT DISAGREE LIGHT CAME ON FOLLOWING SLAT RETRACTION.  RETURNED TO FIELD.  FOUND FUELING DOOR HADRESTRICTED SLAT RETRACTION.  REPAIRED FUELING DOOR, REPLACED ONE LATCH, AND HOLD OPEN ROD ON DOOR.  (M)


REMARKS:
COCKPIT EMERGENCY LIGHTS INOPERATIVE.  REPLACED BATTERIES.  (M)


REMARKS:
PHL - FLT 701 - AFTER TAKEOFF, CREW HAD RIGHT LANDING GEAR SELECTOR LIGHT ON THE MFDU.  FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK STOP.  (M)


REMARKS:
MEM - FLT 1229 - ON FINAL TO MEM, CREW STARTED APU.  AFTER NORMAL START, APU FIRE WARNING SOUNDED, SHUT DOWN AUTOMATICALLY AND THE FIRE BOTTLE ACTIVATED.  CREW CONTINUED APPROACH AND LANDED WITH NO FURTHER INCIDENT.  MX FOUND NO EVIDENCE OF A FIRE.  SUBMITTER STATES, THIS INCIDENT WAS MOST PROBABLY CAUSED DUE TO A BACK PRESSURE SITUATION IN THE APU FIRE CONTAINMENT THROUGH DRAWING APU EXHAUST INTO THE SHROUD WHICH ACTIVATED THE FIRE WARNING.  MX WAS PROGRAMMED TO CHECK THE SHROUD, LOAD CONTROL VALVE, AND BLEED AIR SWIVEL JOINTS FOR LEAKS.  (M)


REMARKS:
PIT - FOUND EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE RESET THE EMERGENCY LIGHT CIRCUIT BREAKERS AND REPLACED THE MAINENTRANCE DOOR EXIT SIGN BATTERY PACK.  (M)


REMARKS:
PIT - FL 400 - AFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT.  CREW RECYCLED THE GEAR AND THE GEAR RETRACTED NORMALLY.  FLIGHT CONTINUED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE JACKED THE AIRCRAFT AND SWUNG THE GEAR SEVERALTIMES.  NO PROBLEMS WERE FOUND.  THE GEAR WAS LUBRICATED AND THE AIRCRAFT RELEASED FOR SERVICE.  (M)


REMARKS:
ROC - MAINTENANCE FOUND THE AFT AISLE BULLNOSE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE.  MAINTENANCE REPLACED THE POWER SUPPLY.  (M)


REMARKS:
MCO - FLT 1981 - ON DESCENT TO MCO, CREW NOTICED A VERY STRONG ODOR.  SMELLED LIKE HYDRAULIC FLUID ON A HOT DUCT.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LEFT AIR CONDITIONING RECIRCULATING FAN.  OPS CHECKED GOOD.  (M)


REMARKS:
PHL - FLT 164 - AFTER TAKEOFF FROM PHL, CAPTAIN LOST WEATHER RADAR.  DUE TO WEATHER, FLIGHT WAS NOT ABLE TO CONTINUE TOBTV AND RETURNED TO PHL.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MX REPLACED WEATHER RADAR TRANSCEIVER.  OPS CHECKED NORMAL.  (M)


REMARKS:
FLT NR 1005 - MEM - AT CRUISE ALT AN ELECTRICAL SMELL DEVELOPED IN THE AFT GALLEY.  CAPTAIN CONFIRMED UPON INSPECTION AND DIRECTED FA'S TO PULL ALL AFT GALLEY CIRCUIT BREAKERS.  SMELL DISIPATED.  DIVERTED TO MEM.  MAINTENANCE REMOVED AND REPLACED BALLAST FOR NR 3 GALLEY WORK LIGHT.  OPS CHECK GOOD.  (M)


REMARKS:
LAS - FL 9 - AFT AUXILLIARY TANK FUEL INDICATION WAS ERRACTIC FROM 0 TO 3,300 POUNDS DURING FLIGHT.  CREW WAS UNALE TO TRANSFER FUEL DURING FLIGHT.  FLIGHT DIVERTED TO LAS AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED LENGTH OF COAX AND SENSOR TUBE.  OPS CHECK GOOD.  (M)


REMARKS:
FLT 8560 - PIT-MCO - ON CLIMB, GEAR DOOR OPEN LIGHT ILLUMINATED.  DIVERTED TO CLT.  ADJUSTED RIGHT GEAR DOOR TARGET.  PERFORMED GEAR SWING, CHECKED GOOD.  (M)


REMARKS:
ROA - DURING VISUAL INSPECTION, FOUND 1 INCH CRACK IN FUSELAGE SKIN.  INSTALLED DOUBLER PER SRM 53-30-03.  (X)


REMARKS:
ROA - DURING BX CHECK, FOUND LIGHTNING STRIKE DAMAGE 2 INCHES BY 8 INCHES ON FUSELAGE CROWN SKIN.  BURNISHED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 6.  (X)


REMARKS:
CLT - DURING ANNUAL SLIDE DEPLOYMENT CHECK, RIGHT OVERWING ESCAPE SLIDE DID NOT DEPLOY AUTOMATICALLY WHEN ACTUATED.  SLIDE WAS SUCCESSFULLY DEPLOYED MANUALLY.  MAINTENANCE FOUND A DEFECTIVE FUSE IN POWER SUPPLY M962.  POWER SUPPLY WAS REPLACED.  (X)


REMARKS:
PHL/PWM - FLT 2246 - ON CLIMB, 'RT ENGINE OIL PRESS LOW' WARNING LIGHT FLICKERED WITH CORRESPONDING DROP ON OIL PRESSURE GAUGE.  SHUT DOWN ENGINE, RETURNED TO FIELD.  REPLACED RIGHT ENGINE OIL PRESSURE RELIEF VALVE, AND ADJUSTED PRESSURE PER MM.  (X)


REMARKS:
PIT - EMERGENCY LIGHTS INOPERATIVE.  MAINTENANCE REPLACED THE FORWARD, MID AND AFT EMERGENCY PANELS.  (X)


REMARKS:
RSW - FLT 989 - ON APPROACH INTO RSW AT GEAR EXTENSION, CAPTAIN FAILED TO GET NOSE GEAR LIGHT.  CAPTAIN DID A GO-AROUNDAND RELAMPED NOSE GEAR DOWNLIGHT.  GEAR WAS CYCLED WITH NORMAL GEAR INDICATION.  RELAMPED NOSE GEAR LIGHT.  (X)


REMARKS:
LGA - FLT 2221 - ON APPROACH TO LGA, CREW REPORTED WHILE FLYING WITH AUTOPILOT DISENGAGED, THE ELECTRIC STABILIZER TRIMACTIVATED FOR 3-5 SECONDS.  CREW OVERRODE TRIM AND PERFORMED A GO-AROUND.  FLIGHT THEN LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED SYSTEMS CHECKS ON BOTH THE AUTOPILOT AND STABILIZER TRIM SYSTEMS.  NO FAULTS WERE FOUND.  (X)


REMARKS:
BWI - FLT 2539 - ABOUT 50 MILES OUT OF BWI, THE CREW OBSERVED ZERO OIL PRESSURE ON THE NR 1 ENGINE.  ALL OTHER INDICATIONS WERE NORMAL.  FLIGHT RETURNED TO FIELD AT BWI.  THE ENGINE WAS NOT SHUT DOWN AND NO EMERGENCY EQUIPMENT WAS CALLED OUT.  THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR 1 ENGINE OIL PRESSURE INDICATOR.  (X)


REMARKS:
PIT - FLT 1279 - WHILE CLIMBING THROUGH 8,000/9,000 FEET, FLIGHT ATTENDANT ADVISED CAPTAIN OF A NOISE FROM THE REAR OF THE AIRCRAFT.  AFTER LEVELLING OFF AT 11,000 FEET, DISCOVERED THE SAFETY RESTRAINING STRAP WAS CAUGHT IN THE 2L DOOR.  THERE WAS NO DOOR WARNING INDICATIONS OR ABNORMAL PRESSURE INDICATIONS.  FLIGHT DIVERTED TO PIT AND LANDED WTIH NO FURTHER INCIDENT.


REMARKS:
ORF - FLT 1177 - AFTER TAKEOFF, CREW WAS UNABLE TO RAISE LANDING GEAR.  LANDING GEAR INDICATIONS WERE BLANK.  CREW ACCOMPLISHED CHECK LIST AND FOUND LIGHTS AND LEVER LATCH CIRCUIT BREAKERS TRIPPED.  RESET SAME AND GOT NORMAL INDICATIONS.  CAPTAIN DECIDED TO RETURN TO FIELD.  EMERGENCY WAS DECLARED.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE PERFORMED OPS CHECK (GEAR SWING) OF LANDING GEAR SYSTEM PER MM.  OPS CHECKED GOOD.  (X)


REMARKS:
LIT - FLT 764 - CAPTAIN REPORTED THE WHEELWELL OVERHEAT DETECTION ILLUMINATED IN CRUISE.  EMERGENCY WAS DECLARED.  FLIGHT DIVERTED TO LIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE P8-1 ENGINE AND APU FIRE CONTROL MODULE.  OPERATIONAL CHECK NORMAL.  (X)


REMARKS:
CLE - FLT 273 - FLYING AT 27,000 FEET, THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED.  CREW SHUT DOWN NR 2 ENGINE AND DECLARED AN EMERGENCY.  FLIGHT DIVERTED TO CLE AND LANDED WITH NO FURTHER INCIDENT.  TOTAL SINGLE ENGINE TIME WAS 10MINUTES.  MAINTENANCE FOUND 2 OIL FILTER STUDS PULLED OUT OF CASTING ON THE NR 2 ENGINE.  REPAIR WAS MADE USING HELI-COILS.  REPLACED OIL FILTER.  RAN ENGINE, LEAK CHECKED GOOD.  (X)


REMARKS:
CLT - FLT 1126 - ON GEAR EXTENSION, NOSE GEAR RED LIGHT REMAINED ILLUMINATED.  CREW CYCLED GEAR WITH NO HELP.   GEAR VISUAL CHECK INDICATED GEAR WAS DOWN.  RED LIGHT FINALLY WENT OUT AND GREEN LIGHT ILLUMINATED.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE ADJUSTED THE NLG DOWNLOCK SENSOR PER MM 32-61-51.  PERFORMED GEAR SWING, OPS CHECK GOOD.  (X)


REMARKS:
MSP - FLT 824 - ON CLIMB-OUT ABOVE 15,000 FEET, A LOUD RUMBLING NOISE BEGAN.  CREW DECIDED TO RETURN TO FIELD AT MSP.  ALL AIRCRAFT INDICATORS WERE NORMAL.  CREW SWITCHED EQUIPMENT COOLING FAN TO ALTERNATE, THEN GASPER FAN TO OFF, NO HELP. NOSE EVENTUALLY DIMINISHED AND QUIT BELOW 10,000 FEET.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE INSPECTED DOORS AND WING-TO-BODY FAIRINGS.  NO DEFECTS NOTED.  AIRCRAFT WAS PRESSURIZED AND CHECKED FOR LEAKS.  ALL CHECKED GOOD.  REPLACED EQUIPMENT COOLING AUTO FLOW CONTROL VALVE.  OPS CHECKED GOOD.  (X)


REMARKS:
CLT - FLT 560 - TAKEOFF ROLL-OUT OF PIT WAS NORMAL.  UPON PASSING 100 KNOTS, THE THROTTLES SPLIT UNTIL CLIMB POWER WAS REACHED.  ALL INDICATIONS SHOWED NORMAL THEN.  CREW CONTACTED MAINTENANCE CONTROL VIA ARINC.  DECISION WAS MADE TO DIVERT TO CLT WHERE THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE TRIMMED THE FUEL CONTROL UNIT ON THE NR 2 ENGINE.  (X)


REMARKS:
DEN - FLT 600 - DURING CRUISE, CREW REPORTED A FUSELAGE VIBRATION AT ROW 9 A, B, C.  CAPTAIN CONTACTED MAINTENANCE CONTROL VIA ACARS AND TOGETHER THEY COULD NOT PINPOINT A CLEAR CAUSE OF THE VIBRATION.  A DECISION WAS MADE TO DIVERT TO DENWHERE THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE CONTROL CABIN SUPPLY DUCT IN THE AIR CONDITIONING DISTRIBUTION BAY BLOWN.  REPAIRED SAME.  LEAK CHECK GOOD.  (X)


REMARKS:
BWI - FLT 1176 - EN ROUTE FROM MCO TO BDL, CAPTAIN NOTICED WHAT APPEARED TO BE A FUEL LOSS AND SUSPECTED A FUEL LEAK.  CAPTAIN DECLARED AN EMERENCY AND THE FLIGHT DIVERTED TO BWI.  AFTER LANDING SAFELY AND EXITING RUNWAY, FIRE DEPARTMENT TOLD CREW A BAD FUEL LEAK WAS COMING FROM THE NR 1 ENGINE AND RECOMMENDED TO PULL FIRE HANDLE.  FIRE HANDLE WAS PULLED WHICH DISCHARGED FIRE BOTTLE TO NR 1 ENGINE.  AIRCRAFT WAS TOWED TO GATE WITH PASSENGERS ON BOARD.  MAINTENANCE REPLACED THE FUEL HOSE ASSY IN THE STRUT FOR THE NR 1 ENGINE.  LEAK CHECK GOOD.  THEY ALSO REPLACED THE NR 1 ENGINE FIRE BOTTLE AND SQUIB.  OPS CHECK SATISFACTORY PER MM.  (X)


REMARKS:
PIT - FLT 1589 - DURING APPROACH TO PIT AND LANDING GEAR LOWERED, NOSE GEAR RED LIGHT STAYED ON.  CREW RECYCLED GEAR, BUT NOSE GEAR RED LIGHT STILL SHOWED RED FOR APPROXIMATELY 20 SECONDS, THEN TURNED GREEN.  FLIGHT LANDED SAFELY WITH NO FURTHER INCIDENT.  MAINTENANCE JACKED AIRCRAFT AND LUBRICATED NOSE GEAR.  ACCOMPLISHED GEAR RETRACTION/EXTENSION CHECK.  OPERATIONAL CHECK AND INDICATION NORMAL.  (X)


REMARKS:
GSO - DURING 'WALKAROUND' VISUAL INSPECTION, FOUND .50 INCH CRACK IN EXTERIOR SKIN FORWARD GALLEY DOOR OUTER SKIN AT THE FORWARD UPPER CORNER OF THE LOWER HINGE CUT OUT.  INSTALLED DOUBLER, REPAIRED PER TYPICAL REPAIR 52-10-01 A.  (X)


REMARKS:
INT - DURING 'Q-6' CHECK VISUAL INSPECTION FOUND 3 CRACKS, 1 INCH, 1 INCH, AND .50 INCH, 178 BULKHEAD.  STOP DRILL CRACKS, FABRICATED DOUBLER, FILLERS, AND INSTALLED.  REPAIRED PER SRM 51-10-1, TR 53-10-11.  (X)


REMARKS:
INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK, 178 BULKHEAD.  STOP DRILLED CRACK, FABRICATED DOUBLER, FILLERS, AND INSTALLED.  REPAIRED PER SRM 51-01-1, TR 53-10-11.  (X)


REMARKS:
INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 1156, WL 380 RT OUTBOARD CHORD OF BULKHEAD.  STOP DRILLED AND INSTALLED REPAIR.  REPAIRED PER EO 5391G569.  (X)


REMARKS:
INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STR 18A SHELF, 1 INCH FORWARD OF STA 727 BULKHEAD AT INBOARD VERTICAL FASTENER.  STOP DRILL CRACK AND INSTALLED REPAIR KIT.  REPAIRED PER EO 5393G256.  (X)


REMARKS:
INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 1.6250 INCH CRACK IN OUTER SKIN S18R, BS 727A PLUS 7 INCHES.  DOUBLERINSTALLED, REPAIRED PER SRM 53-30-3.  (X)


REMARKS:
INT - DURING 'Q-6' CHECK EDDY CURRENT, FOUND .50 INCH LONG CRACK AT STIFFENER STA 178, LBL 5.7 INCH, WL 184.  INSTALLEDREPAIR ANGLES AND REPAIRED PER TR 53-10-17.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 7 INCH BY 3 INCH CORRODED AREA, STR 25L, BS 967 TO BS 974.  INSTALLEDREPAIR DOUBLER, REPAIRED PER SRM 53-10-3.  CORROSION TASK NR: C53-202-01.  CORROSION LEVEL:  2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND FRETTING CORROSION 55 INCHES RIGHT KEEL BEAM LOWER CORD STA 672 TO STA 727.  INSTALLED REPAIR STRAP, REPAIRED PER EA 41232.  CORROSION TASK NR:  C53-212-01.  CORROSION LEVEL:  2.  (X)


REMARKS:
INT - DURING Q-CHECK VISUAL INSPECTION, FOUND T-CAP SURFACE CORROSION AT LBL 15, STA 1016.  REMOVED PRE-EXISTING REPAIR, FABRICATED NEW REPAIR AND REPAIRED PER SRM 53-10-9.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED SCREW HOLES ON FLOOR BEAM BS 328 22 INCHES RBL 36 INCHES RBL AND 42 INCHES RBL.  REPLACED SECTION OF FLOOR BEAM AND INSTALLED ANGLES.  REPAIRED PER TR 53-10-13.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS ON FLOOR BEAM UPPER FLANGE BS967 LBL 27 INCHES TO RBL 52 INCHES.  INSTALLED T-SECTION WITH REPAIR ANGLES AND STRAPS, REPAIRED PER EA NR 41242.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 5 INCH BY 3 INCH CORRODED AREA STR 27L BS 967 TO BS 972.  INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3, FIGURE 1.  CORROSION TASK NR:  C53-208-01.  CORROSION LEVEL:  2.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS 1 INCH BY 1 INCH ON FLOOR BEAM BS 947.5 LBL 37INCHES TO RBL 35 INCHES.  INSTALLED T-CAP WITH REPAIR ANGLES, REPAIRED PER SRM 53-10-9.  (X)


REMARKS:
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS ON FLOOR BEAM UPPER FLANGE BS986.5 LBL 27 INCHES TO RBL 52 INCHES.  INSTALLED T-SECTION WITH REPAIR ANGLES AND STRAPS, REPAIRED PER EA NR 41243.  (X)


REMARKS:
ROA - DURING 'BX' CHECK VISUAL INSPECTION, CONFIRMED WITH HFEC, FOUND .75 INCH FUSELAGE SKIN CRACK S19L, BS 760.  STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIGURE 3.  (X)


REMARKS:
ROA - DURING 'BX' CHECK VISUAL INSPECTION, FOUND .4375 INCH CRACK AT AFT ENTRY DOOR CUT OUT FORWARD LOWER HINGE CUT OUTFUSELAGE SKIN.  REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIGURE 34.  (X)


REMARKS:
MCO - DURING CRUISE SHUT DOWN NR 2 ENGINE, S/N 1541, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION.  FOUND METAL PARTICLES IN OIL FILTER.  REPLACED ENGINE.  ENGINE OPERATION THEN CHECKED NORMAL.


REMARKS:
STL - AFTER TAKEOFF SHUTDOWN NR 2 ENGINE, S/N 4413, DUE TO OVERSPEED AND NO RESPONSE TO THRUST LEVER MOVEMENT.  FOUND INTERNAL MALFUNCTION IN FUEL FLOW REGULATOR MFG P/N FFR101MK10.  REPLACED FUEL FLOW REGULATOR.  ENGINE OPERATION THEN CHECKED NORMAL.


REMARKS:
DEN - DURING CRUISE NR 3 ENGINE, S/N 4402, SPUN DOWN.  DESCEND TO FL 240 AND RESTARTED ENGINE.  REPLACED ENGINE FUEL FILTER, MFG P/N QA03403, PERFORMED TEST 19 OF MM 71-00-00.  ENGINE OPERATION CHECKED NORMAL.


REMARKS:
STL - DURING CRUISE, L2 DOOR EVACUATION SLIDE, MFG P/N 100505-201, INFLATED.  DEFLATED SLIDE.  FOUND EVACUATION SLIDE LANYARD HAD CAUGHT ON FOOD SERVING CART.  REPLACED EVACUATION SLIDE.  L2 DOOR OPERATION CHECKED NORMAL.


REMARKS:
STL - DURING CRUISE, EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY.  FOUND ALL EMERGENCY LIGHT BATTERY POWER SUPPLY WEAK,MFG P/N 5822-2.  REPLACED ALL BATTERY POWER SUPPLIES AND THEN EMERGENCY LIGHT SYSTEM OPERATION CHECKED NORMAL.  (M)


REMARKS:
STL - DURING SPECIAL INSPECTION, FOUND .5 INCH CRACK LONGERON 5R STATION 756, REPAIRED PER SRM 53-02 FIGURE 2.


REMARKS:
STL - DURING DESCENT AISLE EGRESS LIGHTS AT SEAT ROWS 15 THROUGH 17 ILLUMINATED.  FOUND POWER SUPPLY BATTERY PACK WEAK,MFG P/N 5822-2.  REPLACED POWER SUPPLY BATTERY PACK AND EGRESS LIGHT SYSTEM, OPERATION CHECKED NORMAL.


REMARKS:
STL - DURING AS-2, FOUND .5 INCH CRACK IN LONGERON 5R STATION 832.  REPAIRED LONGERON 5R PER SRM 53-02 FIGURE 2.


REMARKS:
LAX - FLT 150 - DURING CLIMB, SHUT DOWN NR 2 ENGINE, S/N 4813, DUE TO HIGH VIBRATION MONITORING.  FOUND METAL PARTICLESIN TAILPIPE.  REPLACED ENGINE.  ENGINE OPERATION THEN CHECKED NORMAL.  ENGINE TOTAL TIME 49,344, ENGINE CYCLES 16,215.


REMARKS:
SAN - FLT 308 - ON TAKEOFF, SHUT DOWN NR 1 ENGINE, S/N 1217, DUE TO LOSS OF EPR AND INCREASE IN EGT.  FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL.  INVESTIGATION REVEALED SECOND STAGE LOW PRESSURE TURBINE VANES WORE THROUGH SHROUD, P/N 798157 FLANGE, LIBERATING SHROUD INTO GAS PATH.  ENGINE WAS REPAIRED AND RETURNED TO SERVICE.  ENGINE TOTAL TIME 22,736, ENGINE TOTAL CYCLES 11,408.


REMARKS:
SJU - DURING CRUISE NR 1 ENGINE, S/N 4623, EXPERIENCED A POWER SURGE.  ADJUSTED BETA RATE 1/4 TURN CLOCKWISE.  ENGINE THEN CHECKED NORMAL.  (M)


REMARKS:
PIT - DURING Q3/C5 CHECK, FOUND 3 INCH BY 4 INCH CORROSION IN SKIN AT NR 3 VHF ANTENNA FS 1174 AREA, LONGERON 30.  TREATED AND INSTALLED DOUBLERS PER EO 32910 (10 INCH BY 20 INCH).  CORROSION LEVEL 2, CORROSION TASK NR C50-53300.  (M)


REMARKS:
PIT - DURING AFT PRESSURE BULKHEAD REPAIR, PCI-919, FOUND CRACK APPROX 1.25 INCH LONG AT SKIN CLIP.  AFT SIDE OF BELT FRAME 1019 LT SIDE, BELOW AUG VALVE.  FILLER AND DOUBLER INSTALLED 2014T6 .050 PER EA NR 32448 SRM 53-03 PG 97 FIG 29.  (M)


REMARKS:
PIT - DURING AFT PRESSURE BULKHEAD REPAIR, PCI-919, FOUND CRACK APPROX .5 INCH LONG ON CANTED FRAME STATION 1104 STRINGER 12R.  INSTALLED DOUBLER 2024T3, .063 PER SRM 53-03 FIG 30.  (M)


REMARKS:
PIT - DURING Q3/C5 CHECK, FOUND 1 INCH CRACK THROUGH RIVET AT LT VERTICAL STABILIZER DRAG ANGLE AFT SIDE CANTED STATION1388.  INSTALLED REPAIR STRAPS AND ANGLES PER SRM 55-02 FIG 26 CONFIG 7001.  (M)


REMARKS:
PIT - DURING AFT PRESSURE BULKHEAD REPAIR, PCI-919, FOUND 1 INCH LONG CRACK AT STATION 1076 LONGERON 16 LEFT AT SKIN CLIP.  REPAIRED MFG CLIP FROM 2024T3 .062 PER EA 31776 AND SRM 53-03 FIG 31.  (M)


REMARKS:
CLT - CLT INSPECTION VISUALLY FOUND LEVEL 2 CORROSION 100 BY 4 INCHES LOCATED AT STATION 986.5 FROM RT CREASE BEAM TO LT CREASE BEAM.  REPLACED T-CAP AS PER TYPICAL REPAIR 53-10-05.  (M)


REMARKS:
FLT 551 - RDU-CLT - TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF, FLICKERED, THEN EXTINGUISHED WHEN BLEEDS WERE TURNED OFF.  FOUND LEAKING PERI-SEALS ON DUCT BELOW LEFT ACM.  REPLACED SEALS, RAN BOTH PACKS, CHECKS GOOD.  (M)


REMARKS:
FLOOR LEVEL EMERGENCY LIGHTS (ROWS 19-27) INOPERATIVE.  REPLACED BATTERY PACK, CHECKS GOOD.  (M)


REMARKS:
AFT FLOOR AND CATWALK EMERGENCY LIGHTS INOP.  REPLACED BATTERY PACK.  (M)


REMARKS:
FORWARD FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE.  REPLACED FORWARD BATTERY PACK.  (M)


REMARKS:
FLT 2398 - PHL-BOS - AFTER TAKEOFF, AT 1500 FEET, RIGHT FIRE WARNING LIGHT AND BELL CAME ON.  PULLED RIGHT ENGINE BACK TO IDLE, AND WARNING CEASED.  RETURNED TO FIELD.  FOUND 13TH STAGE CROSSOVER MANIFOLD BLOWN, AND ANTI-ICE CROSSOVER LEAKING AND EXPANSION JOINT.  REPLACED 13TH STAGE CROSSOVER, AND ANTI-ICE CROSSOVER.  (M)


REMARKS:
FIRST CLASS FLOOR TRACK LIGHTING INOPERATIVE.  REPLACED BATTERY PACK.  (M)


REMARKS:
PIT - FL 1050 - ON TAKEOFF, CREW FELT SLIGHT VIBRATION.  VIBRATION INCREASED BEFORE GEAR WAS RETRACTED.  PASSENGER REPORTED SEEING A PIECE OF RUBBER GO BY THE WINDOW.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE FOUND THE NR 1 TIRE HAD LOST ITS RECAP AND DAMAGED THE LEFT WING UNDERSIDE, LEFT FLAP AND THE LEFT OUTBOARD GEAR DOOR. WHEEL WAS REPLACED AND THE DAMAGE REPAIRED.  (M)


REMARKS:
CLT - THE FORWARD EMERGENCY LIGHTS STAYED ILLUMINATED WITH POWER ON.  MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK.  (M)


REMARKS:
PIT - FLT 2049 - CLIMBING THROUGH 12,000 FEET, CREW NOTICED A NOISE FROM LEFT PACK, AFTER WHICH THE OUTPUT TEMPERATURE ROSE TO 150 DEGREES.  RIGHT PACK TEMPERATURE WAS RUNNING HOT BUT COOLED WHEN ENGINE POWER WAS REDUCED ON DESCENT.  CABINBECAME VERY WARM.  FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE RIGHT PRSOV WHICH WAS CAUSING A PRESSURE IMBALANCE AND THE RIGHT AIR CONDITIONING PACK.  (M)


REMARKS:
ATL - FLT 1184 - EN ROUTE MSY-BWI, FL350, CREW NOTED A GRINDING NOISE FROM BOTH PACKS.  CABIN THEN BEGAN TO FILL WITH SMOKE.  FLIGHT DIVERTED TO ATL AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED BOTH PACKS DUE TO TURBINE FAILURES.  (M)


REMARKS:
FORWARD LEFT OVERWING EMERGENCY EXIT HANDLE WAS FOUND BROKEN.  MAINTENANCE REPLACED THE HANDLE.  (M)


REMARKS:
CLT - FL 425 - AFTER TAKEOFF, THE RIGHT BAY OVERHEAT LIGHT ILLUMINATED.  THE LIGHT EXTINGUISHED WHEN THE RIGHT BLEED SYSTEM WAS SECURED.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE LOWER PRESSURE VALVE SEALS.  (M)


REMARKS:
CLT - FLT 2228 - ON APPROACH TO CLT, CREW DID NOT RECEIVE GREEN LIGHTS WITH GEAR EXTENDED.  TOWER FLY-BY WAS CONDUCTED,THEN THE ALTERNATE GEAR PROCEDURE WAS PERFORMED.  SECOND TOWER FLY-BY CONDUCTED FOLLOWED BY AN UNEVENTFUL LANDING.  MAINTENANCE REPLACED THE LANDING GEAR INDICATION LIGHTS.  (M)


REMARKS:
FLT 227 - DAY-CLT - LEFT MAIN GEAR DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE ON GEAR EXTENSION.  CYCLED GEAR 5 TIMES, THEN DOWN AND LOCKED LIGHT ILLUMINATED.  REPLACED LEFT MAIN GEAR DOWNLOCK ACTUATOR.  (M)


REMARKS:
PHL - EMERGENCY LIGHT OVER PASSENGER ENTRANCE DOOR INOPERATIVE.  REPLACED BATTERY PACK.  (M)


REMARKS:
CLT - FLT 1278 - CLIMBING THROUGH 1000 FEET, CREW RECEIVED MID CARGO DOOR UNSAFE LIGHT.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE RESEATED THE DOOR.  (M)


REMARKS:
PHL - EMERGENCY LIGHT OVER LEFT OVERWING EXIT, INOPERATIVE.  REPLACED BATTERY PACK.  (M)


REMARKS:
RDU - MAINTENANCE FOUND THE FORWARD ENTRY AND SERVICE DOOR EMERGENCY LIGHTS INOP.  MAINTENANCE REPLACED THE BATTERY PACK.  (M)


REMARKS:
SYR - MAINTENANCE FOUND THE AFT SET OF AISLE EMERGENCY SEAT LIGHTS BLINKING ON AND OFF.  MAINTENANCE REPLACED THE BATTERY PACK.  (M)


REMARKS:
BDA - FL 1459 - WHILE CLIMBING OUT OF DBA AT 24,000 FEET, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED.  REDUCED THRUST TO IDLE, HOWEVER, LIGHT REMAINED ON.  CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURN TO BDA.  TOTAL SINGLE ENGINE TIME WAS 16 MINUTES.  MAINTENANCE CHECKED FOR AIR LEAKS.  NO LEAKS FOUND.  PERFORMED ENGINE RUN AT HIGH POWER.  CHECKS NORMAL.  FOUND B LOOP WOULD NOT TEST ON GROUND.  ACCOMPLISHED CONTINUITY CK OF NR 1 ENGINE B LOOP FROM M279 PLUG D1002.  FOUND NORMAL.  CHECKED ALL B LOOP CONNECTORS FOR DEFECTS, NONE FOUND.  PERFORMED B LOOP OPERATIONAL CHECK, CHECKED NORMAL.  (M)


REMARKS:
BOS - FLT 788 - ON CLIMB-OUT AT APPROXIMATELY 10,000 FEET, THE NR 1 ENGINE OIL TEMPERATURE GAUGE WENT INTO THE YELLOW BAND.  TEMPERATURE DECREASED WITH POWER INCREASE AND INCREASED WITH POWER DECREASE.  CREW DECIDED TO RETURN TO FIELD AT BOS.  OIL TEMPERATURE WAS IN YELLOW BAND FOR APPROXIMATELY 15 MINUTES.  TEMPERATURE RETURNED TO GREEN BAND DURING DESCENTAND LANDING.  NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY WITH NO FURTHER INCIDENT.  MAINTENANCE INSPECTED THE TEMPERATURE BULB CANNON PLUG.  CHECKED NORMAL.  THEY ALSO REMOVED AND REPLACED THE NR 1 ENGINE OIL COOLER.  LEAK CHECK GOOD.  POWER RUN GOOD.  (X)


REMARKS:
INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION FLOOR BEAM, STA 328, LBL 27.  FABRICATED TEE-CAP REPAIR, REPAIRED PER TR 53-10-13.  (X)


REMARKS:
JFK - DURING CRUISE SHUT DOWN NR 2 ENGINE, S/N 1541, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION.  FOUND OIL FILTER FULL OF CARBIDE CRYSTALS CHANGED OIL FILTER, DRAINED ENGINE OIL AND RESERVICED OIL TANK.  ENGINE OPERATION THEN CHECKED NORMAL.  (M)


REMARKS:
CLT - FLT 464 - AFTER TAKEOFF, THE NR 1 ENGINE WOULD NOT ADVANCE TO FULL THROTTLE AFTER REACHING 8000 FEET.  ENGINE SURGED AFTER 8000 FEET.  FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT.  MAINTENANCE PERFORMED A BORESCOPE ON THE ENGINE.  SEVERAL FUEL NOZZLES WERE COKED AND ONE BURNED THROUGH.  ENGINE WAS REPLACED.  (M)


REMARKS:
SLC - FLT 4355 - DURING TAKEOFF, NR 2 ENGINE, S/N 1548, SUFFERED A TURBINE FAILURE.  ENGINE TOTAL TIME:  33,348 HOURS; 21,618 CYCLES,  CHECK C-01 - 2-13-96 - JFK.  INVESTIGATION INTO TURBINE FAILURE OF NR 2 ENGINE, S/N 1548, REVEALED THAT AN LPT 4 BLADE SEPARATED AND PENETRATED THE OTHER CASE, DUCTING AND COWLING,  ENGINE S/N 1548 WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
STL - FLT 564 - DURING APPROACH, SHUT DOWN NR 2 ENGINE, S/N 1722, DUE TO INCREASING EGT.  ACCOMPLISHED NORMAL LANDING.FOUND TURBINE DAMAGE AND METAL PARTICLES IN TAILPIPE.  REPLACED ENGINE,  ENGINE OPERATION THEN CHECKED NORMAL.  ENGINE TOTAL TIME:  35,307 HOURS; 32,872 CYCLES.  CHECK C-12 - 3-20-96 - STL.  INVESTIGATION OF NR 2 ENGINE, S/N 1722, SHUTDOWNREVEALED ONE EACH VANE CRACKED AT INNER SHROUD AND RELEASED, PRODUCING DAMAGE TO THE HIGH PRESSURE COMPRESSOR AND TURBINE.  THE ENGINE WAS REPAIRED AND RETURNED TO SERVICE.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR BEAM CORROSION AT BS 203 WL 208 RBL 12 TO 18.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 727A PLUS 16 TO 19 AT S20L.  INSTALLED DOUBLER REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACK IN SIDE CHORD FROM WL 194 TO 195, BS 178, LEFT.  REPLACED CHORD PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME WEB DAMAGED AT BS 616 RBL 170, WL 221.  INSTALLED DOUBLER REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM STRAP CORRODED AT BS 328 RBL 5 WL 208.  INSTALLED NEW STRAP PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 294 RBL 15, 27, 39, 44.5 AND 46.5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, LBL 7 AND AT BL 0, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND MOP SILL FLOOR STIFFENER ANGLE BS 967 TO 987.5 RBL 46, WL 207.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOP SILL FLOOR CORRODED AT BS 967 TO 992.5, RBL 49 TO 47, WL 208 AND 209.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 987,5, LBL 40, WL 208 AT RBL 40, WL 208.  REPAIRED PER BOEINGSRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318, BETWEEN S2L AND S3L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT S16 AT WING ICE LIGHT CUTOUT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER END SPLICE CRACKED AT BS 359, S14L, UPPER AND LOWER FASTENER HOLES.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, JUST BELOW S16L.  REPLACED WEB PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DAMAGE AT BS 847, RBL 12, S26 TO 25R.  INSTALLED REPAIR DOUBLER PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1016, BETWEEN 18 AND 19R.  INSTALLED REPAIR DOUBLER PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY WEB UPPER ANGLE CRACKED BS 328, RBL 32.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, ON LOWER SURFACE OF SCREW HOLES, LBL 25 TO 38.  REPLACED T-CAP PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM UPPER FLANGE CORRODED AT BS 344 LBL 4 TO 22.  REPLACED T-CAP PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT SERVICE EMERGENCY EXIT LIGHT INOP.  REPLACED BATTERY PER BOEING M/M.


