# SDR

REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM UPPER FLANGE SCREW HOLE CORROSION AT BS 294, LBL 25.  REPLACED T-CAP PERBOEING SRM AND TI 253-008.


REMARKS:
DURING SCHEDULED B-CHECK, FOUND BELTFRAME CRACKED AT BS 639 AND S17R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORROSION AT BS 907, RBL 5.5, WL 165.  REPLACED CORRODED SECTION PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE RT HORIZONTAL STRAPS CRACKED AT BS 1138, S12L AND 12R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSE LT HORZIZONTAL STRAP CRACKED AT BS 1138, S5.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGE AT BS 787, S16R.  REPAIRED PER BOEING SRM.


REMARKS:
CLT - FL 2127 - AT CRUISE, PRIOR TO DESCENT, THE NR 2 ENG OILPRESSURE INDICATED ZERO.  ALL OTHER INDICATIONS WERE NORMAL.  THE NR 2 ENGOIL PRESSURE SHOWED ZERO FOR ABOUT 60 SECONDS BEFORE IT WAS PLACED AT IDLE.THREE MINUTES LATER, SHUTDOWNTHE NR 2 ENGINE FOR CAUTION REASONS.  ANEMERGENCY WAS DECLARED AND THE FLT LANDED SAFELY WITH NO FURTHER INCIDENT.TOTALSINGLE ENGINE TIME WAS TWENTY-FIVE MINUTES.  MX REPLACED THE NR 2ENGINE OIL PRESSURE SWITCH AND OIL PRESSURE TRANSMITTER.  OPS CHECK WASNORMAL.  INSPECTION OF ENGINE AFTER SHUTDOWN SHOWED NO DEFECTS.  ALL ENGPARAMETERS CHECKED NORMAL. REFERENCE USAASB96123


REMARKS:
PIT - DURING Q-2/C-5 CHECK, FOUND .5 INCH BY 4 INCH CORRODED AREA,STATION 1322 LONGERON 30 BELTFRAME.  SPLICED IN NEW BELTFRAME PER SRM53-14-3, CORROSION TASK NR C57-53300.  CORROSION LEVEL 1.(M)


REMARKS:
PIT - DURING Q-1/C-3 CHECK, FOUND CORROSION IN BELTFRAME 1 INCH WIDEBY 2 INCH LONG AT BELTFRAME 996 AT LONGERON 18 LT.CUT OUT CORRODEDBELTFRAME, INSTALLED FILLER AND DOUBLERS 7075 T6 PER SRM 53-30 FIG 14 AND53-05 FIG 93.  CORROSION TASK NR C58-53300, CORROSION LEVEL 1.(M)


REMARKS:
PIT - DURING AFT PRESS BULKHEAD MOD, FOUND 4 INCH LONG CRACK AT AFTPRESS BULKHEAD STATION 996 UPPER RT CORNER OF REAR PAX DOORWAY, DOUBLER5910130-11.  REPLACED UPPER HALF OF DOUBLER 5910130-11 PER EA 32891A ANDDACO DWG J060088.  (M)


REMARKS:
ROA - DURING BX-CHECK, VISUAL INSPECTION FOUND .75 INCH CRACKSTRINGER 18 A RIGHT SHEAR BEAM AT BS 706.  INSTALLED REPAIR KIT, REPAIREDPER EO 5393G256 PART 3 STEP 4.  (M)


REMARKS:
ROA - DURING 'BX CHECK' VISUAL, CONFIRMED WITH HFEC INSPECTIONFOUND 1 INCH FUSELAGE SKIN CRACK BS 747 STRINGER 18R.  REMOVED CRACK ANDINSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCHBY 1 INCH FRAME STATION 990 WL 208.  INSTALLED FRAME REPAIR AND REPLACED 'Z'ANGLE, REPAIRED PER SRM 51-40-03, 51-10-2.  CORROSION TASK NR 53-107-02,CORROSION LEVEL 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH INDENTEDAREA STABILIZER SKIN STATION 111.1 APPROX 12 INCHES FORWARD OF AFT SPAR.INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCHCORRODED AREA ON TOP OF FLOOR BEAM BS 1016 LBL 16 LBL 5.  INSTALLED FLOORBEAM REPAIR, REPAIRED PER SRM 53-10-9.  CORROSION TASK NR C53-017-02,CORROSION LEVEL 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 10 INCHESCHAFFING STATION 720 RHS KEEL BEAM LOWER CORD OUTBOARD FLANGE. INSTALLEDREPAIR STRAP, REPAIRED PER EA 41322.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCHCORRODED AREA AT INBOARD SIDE STRINGER BS 960-967 STRINGER 26R.  INSTALLEDSTRINGER SPLICE/REPAIR.  REPAIRED PER SRM 53-10-3 PAGE 10 FIG 1.  CORROSIONTASK NR C53-202-01, CORROSION LEVEL 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 90INCHES AT STATION 986 FLOOR BEAM UPPER CHORD.  INSTALLED NEW SECTION WITHREPAIR ANGLES AND STRAPS, REPAIRED EA 41317.  CORROSION TASK NR C53-107-02,CORROSION LEVEL 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CRACK .375 INCHSTATION 917 BETWEEN STRINGERS 21L AND 22L SKIN.  INSTALLED DOUBLER, REPAIREDPER SRM 53-30-3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .75 INCH SCRATCHAFT PRESSURE BULKHEAD SKIN 5 O'CLOCK POSITION.  INSTALLED DOUBLER, REPAIREDPER SRM 53-10-4 FIG 3.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO GOUGES 1 INCHAND .625 INCH SKIN STABILIZER STATION 226 15 INCHES AND 20 INCHES AFT OFFRONT SPAR.  INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND TWO GOUGES .75INCH AND .625 INCH SKIN STABILIZER STATION 92.7 APPROXIMATELY 17 INCHES FROMAFT SPAR.  INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCHCORRODED AREA FLOOR BEAM BS 360 RBL 54.  INSTALLED REPAIR ANGLE, REPAIREDPER TR 53-10-05 C.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 1.(M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY1 INCH CORRODED AREAS ON FLOOR BEAM BS 328 RBL 12 INCHTO RBL 45 INCH.INSTALLED NEW T-CAP WITH REPAIR ANGLES, REPAIRED PER TR 53-10-13.  CORROSIONTASK NR C53-107-02, CORROSION LEVEL 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CORRODEDAREAS FLOOR BEAM BS 967.  INSTALLED DOUBLER REPAIRED PERSRM 53-10-9.CORROSION TASK NR C53-107-02, CORROSION LEVEL 1 (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SPOTS OFCORROSION ALONG SIDES OF STRINGER BS 947-995 S-27L.  REMOVED STRINGERSECTION, FABRICATED NEW SECTION AND INSTALLED, REPAIRED PER SRM 53-10-3.CORROSION TASK NR C53-202-01 CORROSION LEVEL 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .33 INCH CORRODEDAREA FLOOR BEAM BS 947.5 RBL 10 TO LBL 36.  INSTALLED REPLACEMENT T-CAP,REPAIRED PER TR 53-10-05C.  CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 3INCHES AT FLOOR BEAM STATION 1006 LBL 8.  CUT OFF T-CAP THATWAS OUT OFLIMITS, FABRICATED REPLACEMENT AND INSTALLED PER SRM 53-10-9 FIG 2.CORROSION TASK NR C53-107-02, CORROSION LEVEL 1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 3INCH CORRODED AREAS AT NUT PLATE HOLES T-CAP, BS 312 FLOOR BEAM BBL 0, RBL8.  INSTALLED T-CAP REPAIR AND REPAIRED PER SRM 53-10-9.  CORROSION TASK NRC53-107-02, CORROSION LEVEL1.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCHCORROSION FLOOR BEAM F/S 1016 BL 0 TO RBL 12.  SPLICED IN FLOOR BEAM T-CAPAND DOUBLERS REPAIRED PER SRM 53-10-9 EA 41313.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETERCORRODED AREA PLUS 4 KEEL BEAM RBL 6.4 FS 727 TO FS 710.  SPOT FACED HOLESINSTALLED, INSTALLED REPAIR STRAP.  REPAIRED PER EA 41303.  (M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1INCH CRACK IN 178 BULKHEAD TWO PLACES LEFT SIDE AT LOWERLEFT MOUNT FORRADAR.  INSTALLED DOUBLERS, REPAIRED PER TR 53-10-11.(M)


REMARKS:
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCHCRACK IN 178 BULKHEAD 2 PLACES RIGHT SIDE AT LOWER RIGHT MOUNT FOR RADAR.INSTALLED DOUBLER AND FILLERS, REPAIRED PER TR 53-10-11.(M)


REMARKS:
BOS - DURING UNSCHEDULED MAINTENANCE, FOUND 2.4 INCH CRACK LTSIDE OF FUSELAGE S16L AT STATION 520, CONFIRMED BY EDDY CURRENT.  INSTALLEDDOUBLER PER SRM 53-30-3 FIG6 AS PERMANENT REPAIR.  (M)


REMARKS:
FLT 1240 - PIT-BGM - IN CRUISE, RIGHT HYDRAULIC SYSTEM LOW PRESSURELIGHT AND RUDDER CONTROL MANUAL LIGHT ILLUMINATED.  NO QUANTITY LOSS.RETURNED TO PIT.  REPLACED NR 2 ENGINE DRIVEN PUMP.  (M)


REMARKS:
FLT 1448 - PIT-PHL - AFTER TAKEOFF, EXPERIENCED SEVERE NOSE GEARVIBRATION AND UNSAFE INDICATION ON NOSE GEAR.  CYCLED GEAR, NO CHANGE.AFTER RETRACTING MAIN GEAR DOORS, GOT DOWN AND LOCKED INDICATION ON NOSEGEAR.  RETURNED TO FIELD.  REPLACED LEFT AND RIGHT NOSE GEAR FORWARD DOORACTUATOR LINKS.  (M)


REMARKS:
FLT 647 - LGA-PBI - UNABLE TO HOLD CABIN ALTITUDE AT FL 350.  CABINCLIMBING AT 500-600 FEET PER MINUTE.  STILL UNABLE TO CONTROL IN MANUAL.DIVERTED TO CHS.  FOUND LOOSE CLAMP ON RIGHT PACK DUCT WORK.  RESECUREDDUCT.  (M)


REMARKS:
FLT 845 - CLT-SDF - NOSE GEAR UNSAFE LIGHT ON WITH GEAR RETRACTION.RECYCLED GEAR WITH SAME RESULT.  RETURNED TO FIELD.REPLACED R2-28 RELAY.GEAR SWING CHECKS GOOD.(M)


REMARKS:
FLT 790 - CLT-IND - ON APPROACH, RIGHT HYDRAULIC SYSTEM QUANTITYBEGAN DROPPING.  MAIN GEAR LOCKED, BUT HAD TO USE EMERGENCY EXTENSION TO GETNOSE GEAR LOCKED.  REPLACED RIGHT HYDRAULIC FILTER HOUSING ASSY.  (M)


REMARKS:
PIT - FL 1601 - AFTER TAKEOFF, CREW RECEIVED 'NO AUTOLAND'MESSAGE.  NEITHER AUTOPILOT WOULD TURN ON.  FLIGHT RETURNED TO PIT ANDLANDED WITH NO FURTHER INCIDENT.  MAINTENANCE REPLACED THE NR 1 FCC.(M)


REMARKS:
CLT - FL 2127 - AT CRUISE, PRIOR TO DESCENT, THE NR 2 ENG OILPRESSURE INDICATED ZERO.  ALL OTHER INDICATIONS WERE NORMAL.  THE NR 2 ENGOIL PRESSURE SHOWED ZERO FOR ABOUT 60 SECONDS BEFORE IT WAS PLACED AT IDLE.THREE MINUTES LATER, SHUTDOWNTHE NR 2 ENGINE FOR CAUTION REASONS.  ANEMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY WITH NO FURTHERINCIDENT.  TOTAL SINGLE ENGINE TIME WAS TWENTY-FIVE MINUTES.  MAINTENANCEREPLACED THE NR 2 ENGINE OIL PRESSURE SWITCH AND OIL PRESSURE TRANSMITTER.OPS CHECK WAS NORMAL.  INSPECTION OF ENGINE AFTER SHUTDOWN SHOWED NODEFECTS.  ALL ENGINE PARAMETERS CHECKED NORMAL.  (M)


REMARKS:
LAS - FL 623 - FLOOR TRACK EMERGENCY LIGHTS INOP AT ROW 22 DEF.MAINTENANCE REPLACED THE EMERGENCY LIGHT LENSE P/N 07912AND BULB P/N0L3071BPEGPL AT ROW 22 DEF.  OPS CHECK GOOD.(M)


REMARKS:
BWI - FLT 262 - AFTER TAKEOFF FROM BWI, CAPTAIN WAS UNABLE TOPRESSURIZE AIRCRAFT.  FLIGHT RETURNED TO FIELD AT BWI.  NOEMERGENCY WASDECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  MX CLEANED WATERDRAIN LINES ON BOTH PACKS AND LINES TO LEFT AND RIGHT STANDBY TEMPERATURECONTROL VALVES.  PACK FLOW CHECKED NORMAL AT MIXING CHAMBER.  ALSO, FOUNDLARGE AIR LEAK AT REAR PRESURE BULKHEAD.  SEAL WAS FOUND OUT OF THE TRACKWHERE APU DUCT ENTERS THE PRESSURIZED AREA.  REPAIREDSAME.  ENGINE RUNACCOMPLISHED AT ALL POWER SETTINGS.  DUCT PRESSURE, PACK OPERATION ANDPRESSURIZATION OK.  (M)


REMARKS:
MCO - FL 1145 - ON DESCENT INTO MCO, LANDING GEAR WAS LOWERED,NOSE GEAR RED LIGHT FLICKERED ON.  CAPTAIN WENT THROUGH MANUAL GEAREXTENSION PROCEDURE.  NOSE GEAR SHOWED DOWN AND LOCKED IN VIEW FINDER.EMERGENCY EQUIPMENT WAS CALLED OUT.  ABOUT FOUR MINUTES FROM LANDING GEARLIGHT WENT TO GREEN.  FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCEREPLACED THE NOSE GEAR DOWNLOCK SENSOR.  SYSTEM CHECKS NORMAL.  (M)


REMARKS:
PIT - FL 1211 - ON APPROACH INTO PIT, CREW RECEIVED A REDINDICATION LIGHT WITH THE GEAR DOWN.  CAPTAIN REQUESTED A FLYBY OF THE TOWERAND RECEIVED CONFIRMATION OF THE GEAR BEING DOWN.  AFTER TALKING WITHMAINTENANCE AND FOLLOWING ABNORMAL PROCEDURES, THE CREW FOUND THAT A CIRCUITBREAKER WAS THE CAUSE OF THE LIGHT.  THE CIRCUIT BREAKER WAS RESTORED ANDTHE LIGHT WENT OUT AS THE FLIGHT WAS EN ROUTE TO A SECOND FLYBY.  THE SECONDFLYBY WAS CANCELLED AND THE FLIGHT LANDED SAFELY IN PIT.  RESTORED CIRCUITBREAKER.  (M)


REMARKS:
TPA - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP ON LEFT SEATAT EMERGENCY EXIT ROW.  MAINTENANCE FOUND BROKEN WIRE.  REPAIRED SAME.  OPSCHECK GOOD. (M)


REMARKS:
CLT - FLT 1979 - ON DESCENT INTO CLT, WHEN LANDING GEAR LOWERED,CREW RECEIVED THREE GEAR RED LIGHTS AND THREE GEAR GREEN LIGHTS.  THE GEARHORN SOUNDED AT FLAPS 15.  CREW RECYCLED GEAR AND RECEIVED THREE GEAR GREENLIGHTS ONLY.  THE FLIGHT LANDED WITH NO FURTHER INCIDENT.  MAINTENANCEJACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES.  UNABLE TO DUPLICATE.CLEANED AND LUBED GEAR HANDLE.  CYCLED GEAR SEVERAL MORE TIMES AND WAS STILLUNABLE TO DUPLICATE.  SYSTEM OPS CHECK GOOD.(M)


REMARKS:
NUMBER 2 WHEEL DAMAGED.  REMOVED AND REPLACED NUMBERS 1 AND 2 TIRE/WHEEL ASSEMBLIES PER BOEING M/M.


REMARKS:
INADVERTENT SLIDE DEPLOYMENT AT FWD SERVICE DOOR.  REPLACED SLIDE ASSEMBLY PER BOEING M/M.


REMARKS:
AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT.  AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING.  INSPECTED AIRCRAFT, REMOVED GEAR PINS.


REMARKS:
ON CLIMBOUT, APU FIRE WARNING LIGHT AND BELL SOUNDED, FIRE BOTTLE WAS DISCHARGED.  AIRCRAFT RETURNED TO LAS AND MADE ANUNEVENTFUL LANDING.  INSPECTED AIRCRAFT AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION.  DEFERRED FIRE DETECT/EXTINGUISHING SYSTEMS AND CONTINUED PER MEL.


REMARKS:
ON CLIMBOUT, NR 3 SLAT WOULD NOT FULLY RETRACT.  AIRCRAFT RETURNED TO MAF AND MADE AN UNEVENTFUL LANDING.  INSPECTED AND LUBED SLAT TRACKS, OPERATION CHECKED SLATS.  MX FERRIED TO DAL.  REMOVED AND REPLACED NR 3 SLAT ACTUATOR AND OP CHECKED PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND DOUBLER ON LT VERTICAL STAB AFT T-BEAM HAS A DEEP GOUGE, 10 INCHES FROM TOP OF BODY.  REPLACED DOUBLER PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 995, RBL 611, WL 226.  REPAIRED PER BOEING SRM.


REMARKS:
EXPERIENCED BIRD STRIKE TO NUMBER 1 ENGINE ON TAKEOFF ACCOMPANIED BY VIBRATION.  AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING.  PERFORMED BIRD STRIKE AND BORESCOPE INSPECTIONS, REPLACED 8 ENGINE FAN BLADES AND PERFORMED ENGINE RUN PER BOEING M/M.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND CRACK INDICATION UNDER VERTICAL STRAP AT BS 178, LBL 5, WL 196.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION ON FORWARD EDGE OF BEAM, BS 1016, RBL 4.5.  REPAIRED PER SWA RA1-253-1476.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND WEB IN FORWARD CARGO BIN CRACKED APPROX 1.75 INCH AT BS 468, RBL 23.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 16R CRACKED BETWEEN 500A AND 500B.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND LT WING NR 3 OUTBOARD AUXILIARY TRACK CUTOUT CRACKED APPROXIMATELY .25 INCH.  REPAIRED PER SWA RA 1-257-167.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND RT SIDE FUSELAGE SKIN CRACKED AT BS 907.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND AFT GALLEY LOWER LOBE STRINGER 27L CORRODED AT BS 1006, AND AT BS 986.5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 294, RBL 21, AT BS 294, RBL 39, AT BS 294, RBL 27.  REPAIRED PER SWA RA TI 253-08 AND BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5 AT AFT FLANGE AND AT LBL 4.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 312 ON UPPER SURFACE AND AROUND SCREW HOLES, LBL 12 TO RBL 3.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 294 ON UPPER SURFACE AND AROUND SCREW HOLES, RBL 1.  REPLACED T-CAP PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, AT S22L, JUST AFT AND ABOVE EXIT LIGHT.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 INCHES AT BS 790, AT S24L, BOTTOM SIDE OF S24L.  REPAIRED PER BOEING SRM.


REMARKS:
AT FL 350, ALTIMETER WARNING HORN SOUNDED.  CREW PERFORMED RAPID DESCENT TO 16,000 FEET.  LEFT PNEUMATIC DUCT PRESS INDICATED 45 PSI AND RT, 13 PSI.  MAIN OUTFLOW INDICATED FULLY CLOSED AT ALL TIMES.  FLIGHT LANDED NORMALLY.  REMOVED AND REPLACED PRSOV PNEUMATIC CONTROL TUBE, AND OPS CHECKED PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 380, S21L AND S22L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 947.5, AT S22R.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 22R CRACKED AT BS 495.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 480, S22L.  INSTALLED DOUBLER PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 379-384, BETWEN S22 AND 23R.  INSTALLED DOUBLER REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE TIE STRAP CORRODED AT NUTPLATE HOLES, BS 436-455, RBL 27.  INSTALLED REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 460 BETWEEN S19 AND 20L.  REPLACED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME DENTED AND GOUGED AT BS 420, LBL 62.  REPLACED FRAME PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FORWARD CARGO FRAMES CRACKED IN UPPER FLANGE AT BS 492, RBL 36, WL 167, AT BS 440, RBL 35 AND AT RBL 39.  INSTALLED DOUBLER REPAIRS PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAMES CRACKED AT BS 500B, LBL 34-50, WL 160-169, AND AT BS 500, LBL 35-38, WL 161-168. INSTALLED DOUBLER REPAIRS PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 402.5 BETWEEN S24 AND 25R AND AT BS 357 AND BS 358, BETWEEN S24 AND 25R. INSTALLED DOUBLER REPAIRS PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INBOARD CHORD CRACKED AT BS 638 AND BS 639, LBL 63, WL 208.  INSTALLED REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 1138, S5L.  INSTALLED REPAIR PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FOWARD GALLEY DOOR AFT FRAME CRACKED ON FRAME LOWER STOP PIN FITTING AND AT NR 4 STOP FITTING.  INSTALLED REPAIR PER BOEING SRM.


REMARKS:
AT GATE, FOUND FLOOR EMERGENCY TRACK LIGHTS INOPERATIVE AT MID-CABIN AREA.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DIVERTED TO PHX DUE TO RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATING IN-FLIGHT.  AIRCRAFT LANDED WITHOUT INCIDENT.  INSPECTED AND REPLACED RIGHT GEAR UPLOCK SENSOR PER BOEING M/M.


REMARKS:
AIR RETURN TO PHX DUE TO TAKEOFF WARNING INDICATION SOUNDING IN-FLIGHT.  AIRCRAFT LANDED WITHOUT INCIDENT.  INSPECTED AND ADJUSTED GROUND SHIFT SENSOR AND OPS CHECKED PER BOEING M/M.


REMARKS:
AT GATE, FOUND BOTH AFT EMERGENCY EXIT LIGHTS REMAINING ILLUMINATED AT ALL TIMES.  REMOVED AFT GALLEY AND REPAIRED BROKEN WIRE.  OPS CHECKED OK PER BOEING M/M.


REMARKS:
AT GATE, FOUND AFT ENTRYWAY EMERGENCY EXIT LIGHTS DIM.  REPLACED LIGHT ASSEMBLY PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT AT AFT ENTRY DOOR INOPERATIVE.  REPLACED BATTERY PACK  PER BOEING M/M.


REMARKS:
DURING SCHEDULED A1 CHECK, FOUND BOTH AFT EMERGENCY EXTERIOR LIGHTS REMAINING ILLUMINATED WITH SWITCH IN ARM POSITION.REPAIRED BROKEN WIRE AT BATTERY PACK  PER BOEING M/M.


REMARKS:
DURING SCHEDULED T-CHECK, FOUND  AFT ENTRY DOOR AND AFT SERVICE DOOR EXTERIOR EXIT LIGHTS INOPERATIVE.  REPLACED BATTERY PER BOEING M/M.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND OVERWING EXIT EXTERIOR EXIT LIGHTS INOPERATIVE.   REPLACED BATTERY PER BOEING M/M.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND STRINGER CORRODED AROUND FASTENER HOLES FROM BS 360 TO BS 420, WL 305.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND STRINGER CRACKED AT BS 767, S10R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, WL 236, LBL 68.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED B1 CHECK, FOUND FORWARD ENTRY DOORWAY UPPER FORWARD RADIUS HAS A .5 INCH CRACK FROM RIVET TOWARD DOORWAY CUT-OUT ON FUSELAGE SKIN.  REPAIRED PER SWA RA 1-253-1483.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND 2 CRACKS ALONG S24L AND BETWEEN BS 781-800.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND WEB AT BS 470 CRACKED UNDER FORWARD CARGO DOOR THRESHOLD.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED 1/2 D-CHECK, FOUND PRESSURE BULKHEAD CRACKED AT FLOOR LEVEL FORWARD AT BS 1020, RBL 37.  REPAIRED PER BOEING SRM.


REMARKS:
DURING FINAL APPROACH, FLIGHT ATTENDANT NOTED A BURNING SMELL IN FORWARD CABIN AREA.  INSPECTED AND FOUND MAIN A/C BATTERY CELLS SHORTED.  REPLACED AND OPS CHECKED BATTERY AND CHARGER PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM UPPER T-CHORD CORRODED AT BS 294.5, BBL ZERO TO LBL 8.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR TO SIDEWALL SUPPORTS CORRODED AT BS 400A TO BS 520, RBL 23, WL 156, AT BS 492, RBL 32, WL 160, AND AT BS 420 TO BS 440, RBL 23, WL 156.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 398, S24-25R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 960, S21L.  REPAIRED PER TRAMCO EWO 96-0406.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND DOOR FRAME CRACKED AT BS 440, RBL 36.5, WL 162.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB GOUGED AT BS 178, RBL 12, WL 239.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 225, S25R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 947, RBL 46 TO 43, WL 208.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 616, WL 202, LBL 65, AT BS 294, RBL 54, WL 274, AND AT BS639, WL 202, LBL 65.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM WEB CRACKED TWO PLACES, BS 710 AND BS 712, RBL 25, WL 203.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND T-ANGLE CRACK ON AFT SIDE OF BS 178 BULKHEAD, LBL 5.5, WL 183.5.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED FROM BS 947 TO BS 1012.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD CHORD CRACK AT BS 178, WL 208.5, TO WL 207, LBL 29.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND FRAME SHEAR TIE CORRODED AT BS 967, S25L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SV CHECK, FOUND AFT CABIN EMERGENCY TRACK LIGHTING INOPERABLE.  REPLACED BATTERY PACK PER BOEING M/M.


REMARKS:
DURING SCHEDULED TERM CHECK, FOUND A 3.5 INCH CRACK ON OUTER SKIN RT SIDE OF FUSELAGE, BETWEEN BS 747 AND BS 727R, AT S18R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH FUSELGE SKIN CRACK FORWARD OF WATER SERV PANEL.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERM  CHECK, FOUND A 2 INCH FUSELAGE  SKIN CRACK AT BS 877, JUST AFT OF EMERGENCY LIGHT.  REPAIRED PERBOEING SRM.


REMARKS:
DURING SCHEDULED SERV  CHECK, FOUND A  2 INCH FUSELAGE SKIN CRACK APPROXIMATELY 10 INCHES FORWARD OF WATER SERV PANEL.REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C2  CHECK, FOUND FUSELAGE SKIN DENTED 6 INCHES AFT OF AFT CARGO DOOR  AT BS 847, AT S19R.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED TERM CHECK, FOUND AFT CENTER CEILING EMERGENCY EXIT SIGN INOPERATIVE.  REPLACED BATTERY AND OPS CHECKED PER BOEING M/M.


REMARKS:
DURING SCHEDULED BC1 CHECK, FOUND FUSELAGE SKIN DAMAGED 13 INCHES BELOW R1 WINDOW FRAME AT BS 224.  REPAIRED PER BOEINGSRM.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND FORWARD SERV DOOR OUTER SKIN CRACKED ABOVE SNUBBER AT L/E FORWARD SIDE.  REPAIRED PER SWA RA 1-352-0252.


REMARKS:
DURING SCHEDULED TERM CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT AFT ENTRY.  RELAMPED PER BOEING M/M.


REMARKS:
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN S27R AND S27L.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C1 CHECK, FOUND 2 FLOOR TRACK LIGHTS INOPERATIVE AT EMERGENCY EXIT ROW.  RELAMPED PER BOEING M/M.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FLOOR BEAM CRACKED AT BS 520, RBL 26.  REPAIRED PER BOEING SRM.


REMARKS:
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 727E, AT S23R, AT 500C, LBL 24.74.  REPAIRED PER BOEING SRM.


REMARKS:
STL - DURING OP-19, FOUND CORROSION ON LEFT INBOARD SEAT TRACK, STATION 200-206.  REPLACED SEAT TRACK PER SRM 53-03, PAGE 10G, SHEET 1, FIGURE 4F.  (M)


REMARKS:
STL - DURING SPECIAL CHECK, FOUND DENT ABOVE EXTERNAL POWER DOOR, STATION 89, LONGERON 17L.  CUT OUT DAMAGED SKIN AND REPAIRED PER SRM 53-04, FIGURE 12B.  TOTAL AIRCRAFT TIME 71,703, TOTAL CYCLES 77,896.


REMARKS:
STL - DURING CRUISE, NOSE GEAR UNSAFE LIGHT ILLUMINATED.  REMOVED AND REPLACED PROXIMITY ELECTRONICS UNIT.  OPERATIONALCHECK NORMAL.


REMARKS:
STL - DURING CRUISE, FLOOR EGRESS LIGHTING STRIP ILLUMINATED AT ROWS 14 TO 20.  DISCONNECTED, CLEANED AND RECONNECTED BATTERY PACK AT ROWS 14 TO 20.  OPERATIONAL CHECK OF EGRESS LIGHTING SYSTEM NORMAL.  (M)


REMARKS:
STL - DURING SPECIAL CHECK, FOUND A CRACK IN LONGERON 1L, STATION 756.  REPAIRED PER SRM 53-02, FIGURE 4, PAGE 5.  (M)


REMARKS:
STL - DURING OP-15, FOUND CRACK APPROXIMATELY ONE INCH LONG IN LONGERON 17R, STATION 1151, TOP AND BOTTOM LEGS.  REPAIRED PER SRM 53-02.  AIRCRAFT TOTAL TIME 41,764, TOTAL CYCLES 37,652.


REMARKS:
SFO - DURING GEAR EXTENSION RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE.  REMOVED AND REPLACED LIGHT BULB INLIGHT ASSEMBLY.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING LAYOVER MAINTENANCE, EMERGENCY LIGHTS WOULD NOT TEST.  REMOVED AND RE-SEATED BULBS IN SOCKETS.  OPERATIONAL TEST NORMAL.  (M)


REMARKS:
STL - DURING CLIMB, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON.  FLIGHT RETURNED TO STL.  REMOVED AND REPLACED DOWNLOCK SWITCH, MFG P/N H14-6.  OPERATIONAL CHECK NORMAL.


REMARKS:
STL - DURING CRUISE EGRESS LIGHTS AT ROWS 8-12 ILLUMINATED.  REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING CRUISE, EMERGENCY EGRESS LIGHT ILLUMINATED.  REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING CRUISE, COACH EMERGENCY LIGHTS ILLUMINATED.  REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING LAYOVER, MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE.  FEEDER CABLES WERE CHECKED FOR SECURITY AND BATTERY PACK, MFG P/N 5822-2, WAS CHANGED.  OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING CRUISE, EGRESS LIGHTING ILLUMINATED IN LAST THREE ROWS.  REMOVED AND REPLACD BATTERY PACK, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL.  (M)


REMARKS:
STL - DURING CRUISE, EMERGENCY LIGHTS FLASHED ON AND OFF.  REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2.  OPERATIONAL CHECK NORMAL.


REMARKS:
STL - DURING CRUISE, EGRESS LIGHTS AT SEAT ROW 15 TO 20 ILLUMINATED.  FOUND POWER SUPPLY, MFG P/N 5822-2, WEAK.  REPLACED POWER SUPPLY.  OPERATION THEN CHECKED NORMAL.


REMARKS:
LAX - AFTER GEAR RETRACTION, RIGHT REAR BRAKE OVERHEAT LIGHT ILLUMINATED.  LANDING GEAR WAS EXTENDED IN ORDER TO COOL THE BRAKE AND THEN RETRACTED.  NR 4 RIGHT TIRE, NR 4R, BRAKE ASSEMBLY, MFG P/N 2-1367-10PT-1, AND ANTI-SKID VALVE, MFG P/N 6000006, WERE REMOVED AND REPLACED.  OPERATIONAL CHECK NORMAL.


REMARKS:
HNL - DURING CLIMB, NOSE LANDING GEAR DOORS CAME OPEN WITH LANDING GEAR SELECTED TO UP.  CYCLED LANDING GEAR.  FOUND NOSE LANDING GEAR DOOR SEQUENCE VALVE.  NOSE GEAR DOOR OPERATION CHECKED NORMAL.


REMARKS:
STL - DURING CRUISE, SINGLE SERVING CART CONNECTOR EMITTED SMOKE AND CIRCUIT BREAKER POPPED.  TURNED OFF SERVICING CARTAND DISCONNECTED CONNECTOR.  FOUND INTERNAL MALFUNCTION IN SERVING CART, MFG P/N 88801-1, CONNECTOR.  REPLACED SERVING CARGO AND OPERATION THEN CHECKED NORMAL.


REMARKS:
STL - DURING OP-15, FOUND .25 INCH CRACK IN FORWARD LOWER DOOR BEAM FITTING RIVET HOLE.  REPAIRED PER SRM 51-00 AND TWASTANDARD PRACTICES.  AIRCRAFT TOTAL TIME 63,299, AIRCRAFT TOTAL CYCLES 77,392.


REMARKS:
OMA - DURING CRUISE NR 2 ENGINE, S/N 3225, WAS SHUTDOWN DUE TO TURBINE FAILURE.  ENGINE TOTAL TIME 34,212, CYCLES 17,878.


REMARKS:
STL - DURING DESCENT, SHUT DOWN NR 2 ENGINE, S/N 1213, DUE TO VIBRATION AND OIL FILTER BYPASS LIGHT ILLUMINATION.  FOUND METAL PARTICLES ON OIL SYSTEM CHIP DETECTORS.  REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL.  ENGINE TOTAL TIME 22,333, ENGINE TOTAL CYCLES 11,261.


REMARKS:
AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT PASS OFF POSITION WITHOUT USING OVERRIDE.  FLIGHT CONTINUED AND LANDED NORMALLY. REMOVED AND REPLACED LANDING GEAR LATCH LEVER AND PRESSURE WARNING CIRCUIT BREAKER ON P6-3 PANEL.  OPS CHECKED GOOD PER BOEING M/M.


REMARKS:
HNL - DURING CLIMB NR 2 ENGINE, S/N 4115, FIRE WARNING ILLUMINATED.  ENGINE WAS SHUTDOWN IN FLIGHT AND AIRCRAFT RETURNED TO HNL WHERE ENGINE WAS CHANGED.  ENGINE TOTAL TIME 78,187, CYCLES 14,251.


REMARKS:
CDG  - DURING CRUISE SHUT DOWN NR 4 ENGINE, S/N 4266, DUE TO LOW OIL PRESSURE.  FOUND ANGLE GEARBOX AND ACCESSORY GEARBOX CHIP DETECTORS WITH METAL PARTICLES.  REPLACED ENGINE AND THEN ENGINE OPERATION CHECKED NORMAL.  ENGINE TOTAL TIME 55,441, TOTAL CYCLES 13,504.


REMARKS:
STL - DURING OP-15, FOUND .25 INCH CRACK IN LONGERON 2R, STATION813, UNDER OUTBOARD BOLT.  REPAIRED PER SRM 53-02, FIGURE 2 AND TWA STANDARDPRACTICES.  AIRCRAFT TOTAL TIME 41,166, AIRCRAFT TOTAL CYCLES36,801.


