Boeing 757-232

Service difficulty reports · 15,843

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '757232'
  ORDER BY difficulty_date DESC"

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SDR DL757060952Skin · damagedLIGHTNING STRIKE DAMAGE AT A FASTENER LOCATION AND ADJACENT SKIN WAS FOUND AT FS 395 BETWEEN S-2L AND S-3L. THE DAMAGE WAS CUT OUT IAW MFG APPROVED INSTRUCTIONS, AND IS DOCUMENTED IN ERA 456266-14.Nov 15, 2006 · N633DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006678Frame · dentedDENT ON FRAME UPPER CAP ON AFT PIT BS 1400 BETWEEN S-25L TO S-26L. CUT OUT DENTED AREA, FABRICATED AND INSTALLED FRAME SUPPORT REPAIR 8.2" BY 2.4" FROM 2075-T6 .071" IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.Nov 15, 2006 · N681DA · Boeing 757232 · Fuselage Main, FrameSDR DL757060962Fitting · gougedTHE LT WING INBOARD NACELLE SIDE LOAD FITTING WAS FOUND WITH A GOUGE. DAMAGE WAS BLENDED, INSPECTED, AND TREATED.Nov 14, 2006 · N629DL · Boeing 757232 · Wing, Nacelle/Pylon Attach FittingsSDR DL757060950Unknown · odorELEC ODOR IN CABIN IN FLT ROWS 37A - F AND 38A-F, ODOR DISSIPATED WHEN CEILING LIGHTS TURNED OFF, HAS NOT REOCCURRED. OPERATED CEILING LIGHTS FOR EXTENDED PERIOD. OPS NORMAL, NO ODOR, OPERATED IFE AND PACKS. ALL NORMAL. ACFT OK FOR SERV.Nov 14, 2006 · N6712B · Boeing 757232 · Air Distribution SystemSDR DL757060945Stringer · corrodedCORROSION WAS FOUND IN SEVERAL LOCATIONS IN THE STRINGER 29R A BOEING APPROVED REPAIR WAS INSTALLED PER 455767-14.Nov 14, 2006 · N629DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757060942Skin · gougedA DAMAGED FASTENER WAS FOUND UNDERNEATH THE SKY RADIO ANTENNA DOUBLER. THE SKIN SURROUNDING THE DAMAGE HOLE WAS TRIMMED OUT AND REPAIRED WITH A BOEING APPROVED REPAIR PER ERA 455640-14Nov 14, 2006 · N629DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757060941Support Fitting · wornTHE SUPPORT FITTING BORE OF THE OUTBOARD FLAP TRACK WAS FOUND WORN AND ELONGATED. THE BORE WAS REAMED TO A TRUE DIAMETER AND A BEARING WAS INSTALLED PER BOEING INSTRUCTIONS AS CONTAINED IN 455361-14.Nov 14, 2006 · N629DL · Boeing 757232 · Trailing Edge FlapsSDR DL757060940Sill · corrodedCORROSION WAS FOUND IN THE LOWER SILL OUTBOARD CHORD OF THE FORWARD CARGO DOOR CUTOUT. THE CORROSION WAS BLENDED, AND A BOEING APPROVED REPAIR ANGLE INSTALLED PER ERA 455360-14.Nov 14, 2006 · N629DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757060939Skin · misrepairedEXISTING DISCREPANCIES WERE FOUND ON THE DOUBLER WHICH REQUIRED REMOVAL AND REPLACEMENT PER BOEING INSTRUCTIONS AS CONTAINED IN 220717-14 REVISION A.Nov 14, 2006 · N629DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006683Shear Tie · corrodedCORROSION (HEAVY) ON AFT PIT FRAME SHEAR TIE AT FS 1480 BETWEEN S-29L AND S-30. FABRICATED AND INSTALLED SHEAR TIE 4-3/4" BY 1" BY 3-1/2" FROM 7075-T6 .050" AT FS 1480 BETWEEN S-29L AND S-30 IAW BOEING DRAWING 140N2002 AND 51-20-01.Nov 13, 2006 · N681DA · Boeing 757232 · Fuselage Internal Mounting StructureSDR DL757060963Bushing · migratedTHE NR 1 PYLON DIAGONAL BRACE WING FITTING OUTBOARD BUSHING IS MIGRATED. THE BUSHING WAS REMOVED AND THE HOLE INSPECTED. BUSHING WAS REINSTALLED.Nov 13, 2006 · N629DL · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DU4R2006682Frame · dentedDENT ON FRAME UPPER CAP ON AFT PIT AT BS 1260 BETWEEN S-25R - 26R. FABRICATED AND INSTALLED DOUBLER 8" BY 7" BY 2-1/2" BY 1" FROM CALS 7075-T6 .080" IAW B757 SRM 51-40-02, 51-20-01 AND 51-70-01 FIG 2.Nov 12, 2006 · N681DA · Boeing 757232 · Fuselage Main, FrameSDR DU4R2006677Skin · dentedS/O NR 291026, N/R 21232 FUSELAGE SKIN BS 1430 BETWEEN S-30R AND S-29R SKIN HAS 2 EA. DENTS. FABRICATED AND INSTALLED REPAIR DOUBLER 13.5 X 12.5 FROM 2024-T3 .100 IAW SRM 53-00-01 FIG. 201 REPAIR 3, AS DIRECTED BY RFTS NR 60014. NOTE: THIS IS A CATEGORY B RNov 10, 2006 · N681DA · Boeing 757232 · Fuselage Main, Plate/SkinSDR DALA1133790682Gear · unknownTRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME04.Nov 8, 2006 · N682DA · Boeing 757232 · Trailing Edge Flap Control SystemSDR DALA1133760682Link · damagedNACELLE STRUT UPPER LINK WING AND STRUT FITTING BUSHING REPLACED IAW EA 06-075079-03, ME01, ME02.Nov 8, 2006 · N682DA · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DU4R2006685Floorbeam · corrodedCORROSION ON MAIN CABIN FLOORBEAM UPPER CAP AT BS 377.7 THRU FASTENER HOLES (2 EA.) AT RBL 1 AND 5 (ON TOP SIDE). CUT OUT UPPER CAP AT BS 377.7. FABRICATED AND INSTALLED FLOORBEAM REPAIR 102.5" BY 7" FROM BAC1505-100617 IAW B757 SRM 53-10-51D, 51-40-05 AND 5Nov 7, 2006 · N681DA · Boeing 757232 · Fuselage Main, Floor BeamSDR DL757060926B-Nut · brokenLT HYDRAULIC QUANTITY ZERO WITH ASSOCIATED LIGHTS AND MESSAGES FOUND LINE TO LT SYS HYD PRES RELIEF VALVE BROKEN AT B-NUT RT HYD LINE AT PRESS RELIEF VALVE. NO PRESS EDP REPLACED EDP A CHANGED CASE DRAIN PRESS FILTERS IAW AMM.Nov 7, 2006 · N6711M · Boeing 757232 · Hydraulic System, MainSDR DU4R2006686Floorbeam · corrodedCORROSION ON MAIN CABIN FLOORBEAM UPPER CAP AT BS 365 FROM BL 0 TO RBL 24. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED FLOORBEAM REPAIR 130-3/4" BY 36-1/4" FROM 7075T73 .125" "T", 7-1/2" BY 1" FROM 7075-T6 .090", 11" BY 3/4" BY 1-7/8" FROM 7075-T6 .050",Nov 6, 2006 · N681DA · Boeing 757232 · Fuselage Main, Floor BeamSDR DU4R2006687Floorbeam · corrodedHEAVY CORROSION ON MAIN CABIN FLOORBEAM UPPER CAP AT BS 720 LBL 4. FABRICATED AND INSTALLED FLOORBEAM REPAIR 12" BY 1.6" FROM BAC1505-100617, 9" BY .7" FROM 7075-T6 .125", 11.25" BY .9" FROM 7075-T6 .063", 11.25" BY .9" FROM 7075-T6 .090", AND 9" BY 1/2" FROMNov 4, 2006 · N681DA · Boeing 757232 · Fuselage Main, Floor BeamSDR DU4R2006688Floorbeam · corrodedHEAVY CORROSION ON MAIN CABIN FLOORBEAM UPPER CAP FWD EDGE OF FASTENER HOLE AT BS 740 LBL 4. FABRICATED AND INSTALLED REPAIR SECTION 12 FROM BAC1505-100617, REINFORCEMENT STRAPS 1 14-1/2 BY 7/8 FROM 7075-T6 .063 AND 1 14-1/2 BY 7/8 FROM 7075-T6 .090 AND RADIUNov 3, 2006 · N681DA · Boeing 757232 · Fuselage Main, Floor BeamSDR DU4R2006675Skin · corrodedS/O 291025 N/R 25256 CORROSION ON FUSELAGE SKIN BS 1681 AND S-26R TO S-29R. COMMON TO AFT LAVE DRAIN PAN FWD FLANGE MOUNT. FABRICATED AND INSTALLED DOUBLER 10 INCHES X 14 INCHES AND FILLER 11.7 INCHES X 11.10 INCHES FROM 2024-T3 .063 INCH IAW ERA 458474-14 DANov 3, 2006 · N683DA · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006674Housing · corrodedS/O 291025 N/R 24877 CORROSION ON FRAME ON TOP OF LAV SERVICING HOUSING BS 1681 TO BS 1701. FABRICATED AND INSTALLED FRAME 17.3 INCH X 3.3 AND BEAM 4 INCHES X 1 INCH X 1 INCH AND 2 BRACKETS 1.3 INCH X 1.8 INCH AND 2 BRACKETS 2.5 INCHES X 1.5 INCH FROM 2024-T3 Nov 3, 2006 · N683DA · Boeing 757232 · Fuselage Main, StructureSDR DL757060911Skin · corrodedDURING CURRENT HMV OF AIRCRAFT, CORROSION WAS FOUND ON THE FUSELAGE SKIN SURFACE AT FS 1682, S26R S29R, UNDER THE FORWARD FLANGE OF THE AFT LAV SERVICE PAN ASSEMBLY. THE CORROSION WAS BLENDED TO REMOVE THE DAMAGE, AND A BOEING APPROVED REPAIR WAS INSTALLED PENov 2, 2006 · N683DA · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006681Skin · corrodedHEAVY CORROSION ON EXTERIOR FUSELAGE SKIN AT AIRPHONE ANTENNAS MOUNT BETWEEN BS 1500 - BS 1520, S-28L - S-29L AND INSIDE DOUBLER. FABRICATED AND INSTALLED DOUBLER 11" BY 6.5" FROM 2024-T3 .050" AND FILLER 2.5" BY 1.8" FROM 2024-T3 .040" IAW B757 SRM 51-20-01,Oct 31, 2006 · N681DA · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757060902Windshield · failedON INITIAL CLIMB-OUT, CAPTS WINDSHIELD CRACKED AND BEGAN TO ARC. LEFT WINDOW HEAT WAS SHUT OFF. RETURNED TO JFK. REPLACED CAPTAIN'S WINDOW AND WINDOW HEAT CONTROLLER.Oct 30, 2006 · N618DL · Boeing 757232 · Flight Compartment WindowsSDR DL757060899Engine · malfunctionedON CLIMB-OUT AT APPROX 8000, LEFT ENG EGT INCREASE INTO RED RADIAL MAX EGT OF 789. LEFT THROTTLE RETARD TO IDLE AFTER APPROX 2 MINUTES EGT WITHIN NORMAL LIMITS. THROTTLE ADVANCE BACK TO CLIMB POWER AND ALL ENGINES INDICATION ARE NORMAL. REPLACED NR 1 ENG PEOct 29, 2006 · N601DL · Boeing 757232 · Engine (Turbine/Turboprop)SDR DU4R2006684Shear Plate · corrodedCORROSION ON SHEAR DECK BS 1716 BL 0 TO LBL 42. FABRICATED AND INSTALLED REPAIR DOUBLER 8.8" BY 6.5" FROM 2024-T3 .063" IAW B757 SRM 53-60-51 FIG 203 REPAIR 2 ALT I.Oct 25, 2006 · N681DA · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006653Support Beam · corrodedS/O 291025 N/R 25189 CORROSION IN SCREW HOLES AND DRILLED OFF SCREWS AT SUPPORT BEAM AFT PIT FLOOR LEVEL S-27R FROM BS 1380 TO 1440. OVERSIZED HOLE, INSTALLED FREEZE PLUG, FABRICATED AND INSTALLED REPAIR STRAP 2.50 INCHES X .90 INCHES FROM 7075-T6 .063 INCH IOct 21, 2006 · N683DA · Boeing 757232 · Fuselage Main, StructureSDR DL757060879Light · brokenEMERGENCY EXIT LIGHT ASSY DAMAGED L2 DOOR. REPLACED L2 DOOR EXIT LIGHT ASSY.Oct 21, 2006 · N621DL · Boeing 757232 · Emergency LightingSDR DU4R2006646Support · corrodedS/0 291025 N/R 24243 CORROSION ON WING TO BODY FAIRING SUPPORT FRAME AT FS 860 (LWR PANEL). CUT OUT CORRODED SECTION OF ANGLE. FABRICATED AND INSTALLED DOUBLER 23 INCH X 1INCH X 1INCH FRP, 775-T6 .050 INCH, 2 EA. DOUBLERS 23 INCH X 1INCH X 1 INCH AND 1 EA. 12Oct 20, 2006 · N683DA · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757060863Door · inoperativeFOUND THAT 4L OXYGEN PANEL DOOR DID NOT OPEN AND DEPLOY, OXYGEN MASKS AT FLIGHT ATTENDANTS STATION WHEN AIRCRAFT LOST CABIN PRESSURE. ITEM LEFT OPEN IN LOGBOOK. A/C FERRY TO ATL FOR OXYGEN CYL. REPLACEMENT AND MAINTENANCE FOUND MTC LOCK INTERFERING WITH O2 Oct 17, 2006 · N611DL · Boeing 757232 · Fixed Inner DoorsSDR DL757060862Sensor · failedLEFT ENGINE BLEED ALERT WITH WING AND ENGINE ANTI-ICE SLECTED. WENT THROUGH QRH PROC. THEN LEFT AND RIGHT BLEED ALERTS, LOST CABIN PRESSURE. REPLACED LEFT FAN AIR TEMP SENSOR, LEFT AND RIGHT BLEEDS NOWCHECK NORMAL. AIRCRAFT DIVERTED INTO MCOOct 17, 2006 · N611DL · Boeing 757232 · Pneumatic Distribution SystemSDR DL757060856Coffeemaker · odorFLT ATT COMPLAIN OF BURNING SMELL FROM MID GALLEY COFFEE POTS. TURNED ON COFFEE MAKERS AND OVENS FOR 30 MIN. NO SIGNS OF BURNING SMELL OK FOR SERVICE.Oct 16, 2006 · N674DL · Boeing 757232 · Buffet/GalleysSDR DU4R2006652Intercostal · corrodedS/O 291025, NR 25180 CORROSION AT BS 1480 TO 1500 S-27R INTERCOSTAL UPPER AND INNER SURFACE.CUT OUT CORRODED INTERCOSTAL CAP. FABRICATED AND INSTALLED REPAIR INTERCOSTAL CAP 18.8750 INCH X 2 INCHES FROM 7075-T6 .050 INCH IAW SRM 51-30-01, 51-20-01 AND 51-40-02Oct 15, 2006 · N683DA · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006648Support Beam · corrodedS/O 291025 NR 24879, CORROSION ON L4 DOOR LOWER SILL SUPPORT BEAM AROUND FASTENER HOLES, CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER 40.0 INCH X 6 INCH FROM 7075-T6 .071 INCH IAW SRM 51-70-11.Oct 12, 2006 · N683DA · Boeing 757232 · Fuselage Main, StructureSDR DL757060840Packing · leakingA/C DIVERTED DUE TO FUEL LOSS. FOUND FUEL FILTER O-RING LEAKING.Oct 11, 2006 · N659DL · Boeing 757232 · Engine Fuel DistributionSDR DU4R2006651Floorbeam · corrodedS/O 291025, NR 25013 CORROSION ON UPPER T-CAP OF FLOORBEAM IN PASSENGER CABIN AT BS 720 B/L 3R. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED ANGLE REPAIR 11INCHES X 1 INCH X 2 INCH FROM BAC1490-2865 AND ANGLE DOUBLER 14 INCHES X 2 INCHES X 1INCH FROM BAC Oct 10, 2006 · N683DA · Boeing 757232 · Fuselage Main, Floor BeamSDR DU4R2006647Skin · corrodedS/O 291025, N/R 24770 CORROSION ON FUSELAGE SKIN AT BS 1510 BETWEEN S-28R AND S-29R.CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 7.0 INCHES X 12.75 INCHES X 6.6 INCHES FROM 2024-T3 .063 INCH IAW SRM 51-40-05, 53-00-01 FIG. 1, 51-20-02 AND 53-Oct 10, 2006 · N683DA · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757060841Skin · gougedTHE FUSELAGE SKIN HAS A GOUGE WHERE THE SKY RADIO ANTENNA WAS PREVIOUSLY INSTALLED AT STA 1338-1362 AND S1-2L. THE DAMAGED FUSELAGE SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED.Oct 10, 2006 · N680DA · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757060833Skin · delaminatedLTS FLAP, AFT MAIN FLAP, TRAILING EDGE LOWER SKIN WAS FOUND DELAMINATED. AREA OF DELAMINATION WAS REPAIRED IAW TABLE II OF SRM 51-70-17, WHICH WAS AUTHORIZED IAW ERA 456549-14.Oct 10, 2006 · N6701 · Boeing 757232 · Trailing Edge FlapsSDR DU4R2006650Shear Web · corrodedS/O 291025 NR 24959 CORROSION ON SHEAR DECK LOCATED NEAR RT AFT CORNER. FABRICATED AND INSTALLED REPAIR DOUBLER 9.00 INCHES X 5.70 INCHES FROM 2024-T3 .063 INCHES IAW SRM 51-20-01, 51-10-02 AND 53-60-51, FIG. 101.Oct 7, 2006 · N683DA · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006649Shear Web · corrodedS/O 291025, NR 24881 CORROSION ON SHEAR DECK LEADING EDGE AROUND FASTENER HOLES. FABRICATED AND INSTALLED REPAIR DOUBLER 9.60 INCH X 4.60 INCH FROM 2024-T3 .063 INCH IAW SRM 51-20-01 AND 53-60-51, FIG 201.Oct 5, 2006 · N683DA · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757060826Control Box · malfunctioned19C AUDIO OUTLET OVERHEATS MELTS PLASTIC HEADSETS, OCCURRED DURING FLIGHT INOP SEAT AUDIO PER MEL 25-20-01I.. PLACARDED INOP DO NOT USE. CONFIRMED FAULT. RECONNECTED DJU/DCU HARNESS ALL VSEB AUDIO CONNECTORS NOW CHECKS GOOD ALL AUDIO OPERATES NORMALLY PER 4Oct 5, 2006 · N6715C · Boeing 757232 · Entertainment SystemSDR DL757060825Restraint · corrodedGIRT BAR RESTRAINT PLATE FOUND CORRODED BEYOND LIMITS, LEVEL 2. REPLACED RESTRAINT PLATE AND DOOR SLIDE/RAFT PER JIC 7809-2.Oct 5, 2006 · N680DA · Boeing 757232 · Escape SlideSDR DL757060822Hose · crackedON CLIMB OUT HEARD A POP AND HISSING SOUND UN VICINITY OF CAPT O2 MASK. ALSO NOTED A DROP IN CREW O2 QUANTITY TO ZERO. POSSIBLE LEAK UNDER CAPT O2 COMPARTMENT. FOUND FLEX LINE BROKEN UNDER CAPTS O2 MASK BOX. REPLACED SAM REPLACED O2 BOTTLE REF MM. LK CKS GOODOct 4, 2006 · N634DL · Boeing 757232 · Crew Oxygen SystemSDR DL757060821Controller · malfunctionedAC DID AN EMERGENCY DECENT DO TO LOSS OF CONTROL OF CABIN IN AUTO .5. NO FAULTS ON CABIN PRESS CONT 1 OR 2. ALL DOOR SEALS GOOD OVER PRESS VLVS NORMAL. REPLACED NR 1 CABIN PRESS CONTROLLER. PRESSURIZED SYS. PRESSURIZATION WAS GOOD DECAY RATE NORMALOct 4, 2006 · N630DL · Boeing 757232 · Cabin Pressure ControllerSDR DL75K060809Control Panel · smokeJUST PRIOR TO PUSHBACK, SMOKE BEGAN COMING FROM CAPTS SIDE VOR/DMA CONTROL PANEL. AFTER POWER REMOVED SMOKE STOPPED. REMOVED AND REPLACED VOR/DME CONTROL PNL IAW MM 34-51-02.Oct 2, 2006 · N608DA · Boeing 757232 · Automatic Direction Finder (ADF) SystemSDR DL757060807Stringer · damagedTHE AFT FUSELAGE STRINGERS WERE DAMAGED DURING A TAIL STRIKE AND NEW STRINGER ED FITTINGS REQUIRE FABRICATIONS WITH DEVIATIONS FROM THE ORIGINAL DRAWING. FABRICATED NEW STRINGER END FITTINGS FROM FORGED BLOCK INSTEAD OF ORIGINAL FORGED SHAPE.Oct 2, 2006 · N622DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757060930Skin · damagedPART REMOVED FROM AC 683. SENT TO SHOP FOR CSVE. WEDGE HAD HAIL DAMAGE AND IS A REQUIRED REPORTING ITEM IAW SRM 57-43-02D. WEDGE REPLACED IAW SRM57-43-02D. SLAT WAS RETURNED TO SERVICE AND SENT TO STOCK AS SPARE ON 11/08/06.Sep 23, 2006 · N683DA · Boeing 757232 · Leading Edge DevicesSDR DL757060774Mount · corrodedDURING THE CURRENT HMV3 CHECK, THE NR 2 PYLON P/N 311N3211 -1 FORWARD ENGINE MOUNT FITTING WAS FOUND WITH FRETTING CORROSION ON THE LOWER SURFACE AROUND THE MOUNT HOLES. PERMANENT REPAIR WAS ACCOMPLISHED PER PRODUCTION PERMIT B757-54-25940PA AND ERA 457245-14Sep 22, 2006 · N632DL · Boeing 757232 · Engine Mount Section
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