Boeing 757-232
Service difficulty reports · 15,843
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '757232' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '757232' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DL757071212Support Fitting · migratedBUSHINGS MIGRATED IN NR 1 PYLON WING AND STRUT SUPPORT FITTINGS FOR UPPER LINK. BUSHINGS REPLACED PER EA 06-075079-03 AND ERA 464036-14.SDR DU4R2007173Skin · damagedFOUND CHAFED NR 2 PYLON AFT WEB FITTING CHAFED AT BOTTOM LT CORNER. REPAIRED BY FABRICATING AND INSTALLED REPAIR HFEC NO RELEVANT INDICATIONS, FABRICATING AND INSTALLING REPAIR GUSSET 4.34" BY 2.88" BY 1.2" FROM 7050-T7451 IAW DELTA ERA 463490-14AD DATED 9-12SDR DU4R2007168Frame · crackedFOUND DENT/CRACK ON FRAME BS 1560 BETWEEN S-24L AND S-23L IN AFT PIT. REPAIRED BY CUTTING OUT DENT/CRACK SECTION OF FRAME, HFEC NO RELEVANT INDICATION. FABRICATED AND INSTALLED FRAME REPAIR 13.5" BY 3" FROM 7075-T6 .063 IAW B757 SRM 51-40-02, 51-20-01.SDR DU4R2007167Fitting · wornFOUND DEEPLY WORN CORNER FITTING OF NR 1 PYLON LT AFT LOWER CORNER AT AFT ENGINE MOUNTS. REPAIRED BY BLENDING, HFEC NO RELEVANT INDICATIONS, FABRICATING AND INSTALLING REPAIR GUSSET 4.34" BY 2.88" BY 1.2" FROM 7050-T7451 IAW DELTA EA NR 463490-14AD DATED 9/12SDR DU4R2007169Skin · damagedPERMANENT REPAIR TO NR 2 PYLON FWD SKIN REQUIRED. ACCOMPLISHED PERMANENT REPAIR IAW DELTA EA 06-074338-03 REV B DATED 01-30-2003 IAW DELTA ERA 362852-14 REV E DATED 9/5/07 APPROVED PER FAA FORM 8110-3 SIGNED BY DER NR SO-831 DATED 29 SEP 1997.
SDR DU4R2007166Floorbeam · corrodedFOUND FLOORBEAM CORRODED AT BS 1640 BL-0 RBL-4, W/L 208.1. REPAIRED BY CUTTING OUT CORRODED AREA. FABRICATED AND INSTALLED FLOORBEAM 29-3/4” FROM BAC1505-100617/7075-T73 AND 2 REPAIR ANGLES 35 BY 1/4 BY 2-1/4 FROM 7075-T6 .063 AND 2 ANGLES 41” BY 1-1/4 BY 2-SDR DL757071182Transceiver · odorDURING DESCENT ACRID ODOR DETECTED IN COCKPIT AND REPORTED BY FLT ATTENDANTS AS WELL IN CABIN. PRIOR TO ODOR THE CABIN AIRFLOW CHANGED TO A SIGNIFICANTLY LESS INTENSITY. RT RECIRC FAN WAS TURNED OFF. LT DME C/B ALSO WAS NOTED POPPED. THE ODOR DISSIPATED RASDR DU4R2007171Skin · damagedNR 1 PYLON I/B SKIN HAS TEMPORARY REPAIR. ACCOMPLISHED PERMANENT REPAIR TO NR 1 PYLON O/B SKIN IAW DELTA EA 06-074338-03 REV B DATED 01/30/2003 IAW DELTA ERA 454288-14 REV ORIG AND B757 SRM 51-00-00D PG 1 APPROVED PER 14 CFR 121.379(B).SDR DU4R2007172Skin · damagedTEMPORARY REPAIR TO NR 1 PYLON O/B SKIN. ACCOMPLISHED PERMANENT REPAIR TO NR 1 PYLON O/B SKIN REPAIR IAW DELTA EA 06-074338-03 REV B DATED 01/30/2003 IAW DELTA ERA 454258-14 REV ORIG APPROVED PER 14 CFR 121.379(B).SDR DU4R2007170Skin · damagedFOUND TEMPORARY REPAIR NR 1 PYLON I/B SKIN. ACCOMPLISHED PERMANENT REPAIR TO NR 1 PYLON I/B SKIN IAW DELTA EA 06-074338-03 REV B DATED 01/30/2003 IAW DELTA ERA 093016-14 REV A AND B757 SRM 51-00-00D PG 1 APPROVED PER 14 CFR 121.379(B).
SDR DL757071172Trigger · brokenDURING OPN 6T129 SLIDE/RAFT SAMPLING PROGRAM 2L DOOR SLIDE DID NOT DEPLOY. FOUND 2L DOOR TRIGGER BROKEN REPLACED SAME PER M/M. INSTALLATION ADJ GOOD (QC1503) C/W OPN 6T129, NO DEFECTS FOUND.SDR DL757071166Hose · leakingON FINAL APPROACH AFTER SELECTING LANDING FLAPS LEFT HYD QTY STATUS MSG AND QTY LEVEL ZERO. FOUND OUTBOARD NOSE STEERING FLEX HYD LINE LEAKING IN AFT RT SIDE OF NOSE WHEEL WELL. INSTALLED TEMP HYD LINE TO FOM. REMOVED TEMP HYD LINE AND INSTALLED NEW FLEX HYSDR DL757071165Control Panel · odorRECEIVED EICAS MSG RT RECIRC FAN WITH ELEC ODOR. ODOR DISSIPATED WITH FAN OFF FWD RT RECIRC FAN TO MCO AND PLAC PER MEL 21-25-01A. FOUND CABIN ALTITUDE CONTROL PANEL LOADING DOWN BACKGROUND LIGHTING FOR ABOVE MENTIONED SYSTEMS REPLACED CABIN ALTITUDE CONTROLSDR DL757071156Video Monitor · inoperativeDURING PREFLIGHT, ELECTRICAL ODOR IN FIRST CLASS CABIN. FOUND FIRST CLASS RETRACTABLE VIDEO MONITOR BURNT UP. REMOVED MONITOR PER ERA AND FWD TO MCO/PLACARD. INSTALLED FWD VIDEO MONT. OPS CK GOOD.SDR DL757071130Window · crackedON MECHANICS PREDEPARTURE CHECK, FOUND A CRACKED OUTER PANE ON PASSENGER WINDOW 31ABC. ON FURTHER INSPECTION, FOUND WINDOW AT 30 ABC ALSO CRACKED. REPLACED BOTH OUTER PANES.SDR DL757071061Fuel Control · malfunctionedON APPROACH INTO SNA, GOT THE FOLLOWING ORDER OF EVENTS, LT ENGINE OIL PRESSURE ON EICAS AND THE OIL PRESSURE DISCREET LIGHT CAME ON, FOLLOWED BY THE ENGINE ROLLING BACK TO OFF. FLIGHT CREW ELECTED TO DIVERT TO LAX AND NOT LAND IN SNA. REPLACED FUEL CONTROLSDR DL757071059Engine · making metalRT ENG IFSD DUE TO OIL PRESS GOING INTO THE RED POSITIVE OIL PRESS NOTED PER FLT CREW. NO INDICATION OF OIL LOSS AS OIL QTY INDICATED 18 PTS AT GATE. T/S OIL PRESS SYSTEM FOUND METAL ON MAIN CHIP DETECTOR. NO METAL ON ALL OTHER CHIP DETECTORS. AIR SPUN ENGSDR DU4R2007164Floorbeam · corrodedFOUND CORROSION AROUND FASTENER HOLE AT FLOORBEAM BS 1661 LBL 10. REPAIRED BY CUTTING OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR CHORD 16 LONG FROM BAC1505-100617, 2 EA. REPAIR ANGLES 24 LONG FROM BAC1490-2734 AND BAC1490-2865 AND TWO 24 REPAIR STRAPSDR DU4R2007162Skin · gougedFOUND GOUGE IN EXT SKIN AT AFT LWR CORNER OF FWD PIT DOOR. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 12 BY 12 FROM 2024-T3 .071 IAW B757 SRM 52-30-01, 51-20-01 AND B757 AMM 51-41-00-352-013.SDR DL757071044Skin · dentedDENTS IN FUSELAGE SKIN NEAR RADOME AT FS 220, LT SIDE, S-23L. CUTOUT DENTS AND INSTALLED DOUBLER.SDR DL757081686Structure · dentedMAJOR REPAIR ER/A 463313-14. THREE DENTS NEAR A/C NOSE REPAIRED.SDR DL757071024Unknown · smokeON TOP OF CLIMB-OUT FLT CREW REPORTED A SLIGHT SMOKE HAZE WITH A RUBBER SMELL LOC AROUND SEAT ROW 36. AFTER LANDING, FLT CREW TRIED TO DUPLICATE PROBLEM BY RUNNING ENGS/PACKS/BLEED SYS/LIGHTING/GALLEY EQUIP. UNABLE TO DUPLICATE PROBLEM. ALSO, PERFORMED AN OSDR DU4R2007163Floorbeam · corrodedFOUND CORROSION ON CABIN FLOORBEAM AT BS 1640, LBL 24 TO RBL 4. CUT OUT 30 INCH CORRODED SECTION OF T-CAP. FABRICATED AND INSTALLED T-CAP REPAIR 36-3/4" FROM BAC1505-100617, 2 EA. SPLICE PLATES 9" BY 1-1/2" BY 1" AND 2 EA. 6-1/2" BY 1-1/2"FROM 7075-T6 .050",SDR DL757071008Lanyard · brokenDURING OPERATION 58108 GIRT BAR INSPECTION, THE CABLE WAS NOT ATTACHED TO THE LANYARD. THE CABLE WAS BROKEN. REPLACED LANYARD ASSY. REPLACED LANYARD ASSY PART NUMBER 3961899-501.SDR DL757071004Attach Fitting · misalignedINSTALLATION OF NEW NR 1 AND NR 2 PYLON WING ATTACH TENSION CLIPS WOULD HAVE REQUIRED SPOTFACE GREATER THAN THE 0.005" ALLOWABLE PER EO 6-070332-03 WHICH PERTAINED TO S/B 757-54-0034 REV 1 FOR THE SIP MODIFICATION. TAPERED RADIUS FILLERS WERE FABRICATED AND ISDR DL757071003Attach Fitting · misalignedNUMBER 2 PYLON SIDE LINK ATTACH FITTING HOLE NR 3 WAS FOUND MISALIGNED WHILE ACCOMPLISHING DELTAS EO 6-70332-3 COVERING SB 757-54-0034. A TAPERED RADIUS FILLER WAS INSTALLED PER ANAMOC TO AD 2003-18-05.SDR DL757071002Bushing · migratedTHE DIAGONAL BRACE WING END FITTINGS OF BOTH THE NR 1 AND NR 2 PYLONS WERE FOUND WITH MIGRATED BUSHINGS DURING ACCOMPLISHMENT OF 6-75079-3. NEW BUSHINGS WERE INSTALLED AS AN AMOC TO AD 2003-18-05.SDR DL757070975Spar · damagedDURING REMOVAL OF A RT WING LOWER PANEL, A FASTENER HOLE WAS MISDRILLED AND OVERSIZED THROUGH THE PANEL EXTERIOR SKIN AND THE FRONT SPAR LOWER CHORD. PERMANENT REPAIR WAS ACCOMPLISHED BY ACTS IN VANCOUVER.SDR DL757070966Transmission · trippedT/E FLAP DISAGREE MESSAGE AND LIGHT ON APPROACH. COMPLETED NON-NORMAL CHECKLIST. FLAPS WENT TO 20 ELECTRICALLY. LIGHTS WENT OUT. T/S PER FIM. BITE CKD FSEU NR 1 FAULT MSG 305 FLAP DISAGREE. BITE CHECK OF FSEU 2 AND 3, NO FAULTS. FOUND LT INBD FLAP TRANSSDR DL757070956Duct · blownLEFT DUCT LEAK THEN RIGHT DUCT LEAK, LOST REMAINING RT PACK AUTO PRESS 1 AND 2 FAIL MSGS. LOST CABIN PRESS, EMERGENCY DESCENT TO 10,000 FT. FOUND DUCT IN RT SIDE BLOWN BLOWING HOT AIR INTO THE RT AND LT A/C BAYS GIVING DUCT LEAK MSGS. DUCT BLOWN WAS THE RESDR DL757070955Idg · inoperativeON TAKEOFF, AROUND 60 KTS RT ENG GEN DRIVE LIGHT ON WITH EICAS MSG. ABORTED T/O. REPLACED RT ENG IDG AND GCU. NO FAULTS ON BPCU.SDR DU4R2007156Floor Panel · corrodedFOUND AFT DECK PLATE BS 1713 TO BS 1717 RBL 6 TO RBL 26 CORRODED. REPAIRED BY FABRICATING AND INSTALLING DOUBLER REPAIR 7-3/8 BY 6-3/4 FROM 2024-T3 .063 IAW B757 SRM 53-30-51 FIG 201, 51-40-02 AND 51-20-01.SDR DU4R2007155Sill · corrodedFOUND AFT CARGO LWR DOOR SILL CORRODED FROM BS 1390 TO BS 1440 S-27R. REPAIRED BY REMOVING DOOR SILL AND INSTALLING P/N 146N8522-52 IAW B757 SRM 51-40-02, 53-60-15, 51-40-04 AND 51-40-06.SDR DU4R2007154Skin · gougedFOUND GOUGE IN FUSELAGE SKIN AT PREVIOUS REPAIR ON LT SIDE BS 660, S-17L. REPAIRED BY FABRICATING AND INSTALLING DOUBLER REPAIR 13 BY 10 BY 11-3/8 BY 8-1/2 AND TRIPLER 12 BY 8 BY 9-1/4 BY 7-3/4 FROM 2024-T3 .063, DOUBLER AND FILLER 11.25 BY 8 AND 21 BY 18.50”SDR DU4R2007153Torque Tube · corrodedFOUND RT I/B FLAP I/B TORQUE TUBE CORRODED. REPAIRED BY REMOVING AND REPLACING TUBE WITH P/N 113N2108-1 AND 113N2105-2 IAW B757 AMM 27-51-05 AND DELTA EA 06-097981-14 REV A.SDR DU4R2007152Torque Tube · corrodedFOUND LT I/B FLAP I/B TORQUE TUBE CORRODED. REPAIRED BY REMOVING AND REPLACING TUBE WITH P/N’S 113N2105-1 AND 113N2108-1 IAW B757 AMM 27-51-05 AND DELTA EA 06-097981-14 REV A.SDR DL757070941Skin · dentedDURING HMV, INSPECTION NOTED 2 DENTS AND AN EXISTING EXTERNAL DOUBLER ON THE FUSELAGE SKIN, LEFT SIDE. THE TWO DENTS WERE CUTOUT, AND THE EXISTING REPAIR WAS REMOVED. THE EXISTING REPAIR WAS ALSO CUT OUT, REMOVING ALL EXISTING HOLES, AND THREE BOEING APPROVESDR DL757070939Display · unserviceableAT 13000 FT GOT ODOR OF ELEC SMOKE THEN SAW SMOKE BILLOWING UP FROM COPILOTS LT LEG. RETURNED TO LAS. FOUND EVIDENCE OF F/O'S FMS MCDU BURNT. ASSOCIATED FMC MSG MCDU BLANK. INSPECTED AREA AND ASSOCIATED HARNESSES FROM FWD E AND E COMPT AND PEDESTAL. REPLASDR DU4R2007161Fitting · corrodedFOUND FITTING AT C-2 DOOR CORRODED (AT NUTPLATES) THRESHOLD BS 1440 S-27R. REPAIRED BY REMOVING FITTING AND INSTALLING P/N 69-45578-7 IAW B757 SRM 51-40-02 AND 51-10-02.SDR DU4R2007160Rib · crackedFOUND LT INBB FLAP MAIN FLAP RIB (3RD FROM I/B END) CRACKED. REPAIRED BY REMOVING RIB AND INSTALLING RIB FABRICATED (ON N/R 25000)16.780 BY 8.550 FROM 7050-T7457 IAW B757 SRM 51-40-02, BOEING DWG NR 113N2352 REV C, AND B757 SRM 51-20-01.SDR DU4R2007151Frame · corrodedFOUND CORROSION IN AFT PIT ON MAIN FRAME BS 1480 UPPER AND FWD AREA BETWEEN S-26, S-27 RT. REPAIRED BY FABRICATING AND INSTALLING DOUBLER REPAIR 20 BY 4.0 FROM 7075-T6 .063 IAW B757 SRM 53-00-57, 53-60-07, 51-20-01 AND 51-40-02.SDR DL757070913Engine · damagedIRR:ON SELECTION OF TAKEOFF POWER, AT 31 DERATE-LEFT ENGINE EMITTED LOUD BANG. POWER-EPR/N1-DETERIORATED AND TAKEOFF WAS ABORTED-LESS THAN 10 KTS. MOMENTARY PUFF OF SMOKE. OTHER AIRCRAFT REPORTED FLASH AND SPARKS FROM TAILPIPE. ENGINE EGT AND OIL PRESSURE SDR DL757070917Unknown · odorFLT 597/13 JFK-SEA DIVERTED TO ORD FOR ELECTRICAL ODOR AND SLIGHT HAZE IN AFT CABIN NEAR THE AFT GALLEY. FLT CREW DECLARED AN EMERGENCY AND LANDED OVERWEIGHT. DURING DESCENT FLT CREW TURNED OFF BOTH UTILITY BUSSES, ODOR AND HAZE BEGAN TO DISSIPATE. MTC COMPSDR DL757070907Skin · dentedFUSELAGE SKIN HAS A DENT/GOUGE AT STA 528 BETWEEN S-26L AND S-27L. THE DAMAGED FUSELAGE SKIN WAS CUTOUT AND AN EXTERNAL DOUBLER WAS INSTALLED.SDR DL757070906Line · leakingJUST PRIOR TO LANDING, LOST LEFT HYDRAULIC FLUID. FOUND PRESS HYD LINE FOR RT GEAR DOWN LOCK ACTUATOR LEAKING. REPLACED LINE AND SERVICED HYD QTY .SDR DU4R2007159Floor Panel · corrodedFOUND CORRODED AFT DECK PLATE BS 1681.8 FROM LBL 14 TO LBL 29. REPAIRED BY CUTTING OUT CORRODED SHEAR SKIN AT B/L 25L AND SECTION OF FLOORBEAM. FABRICATED AND INSTALLED REPAIR DOUBLER 17 BY 4 FROM 2024-T3 .080, REPAIR STRAPS 24 BY 1 FROM 7075-T6 .040. REPAISDR DL757070900A/C Pack · malfunctionedIN FLIGHT, THE RIGHT PACK WAS UNABLE TO PRESSURIZE A/C. THE LT PACK WAS ON MCO. CHECKED NR 1 AND NR 2 CABIN PRESSURE CONTROLLER BOTH CK GOOD. CHECKED ALL DOOR SEALS AND OUTFLOW VALVE. AFTER LT ACM CHANGE PRESSURIZED A/C TO 5 PSID WITH APU NO LEAKS NOTED.SDR DU4R2007158Floor Panel · corrodedFOUND CORRODED AFT DECK PLATE BS 1681.8 FROM LBL 1 TO LBL 14. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 6-1/2 BY 14 FROM 2024-T3 .063 IAW B757 SRM 53-60-51 PG 201/204 AND 51-10-01.SDR DU4R2007157Floor Panel · corrodedFOUND CORRODED AFT DECK PLATE BS 1681.8 FROM LBL 1 TO LBL 14. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 6-1/2 BY 14 FROM 2024-T3 .063 IAW B757 SRM 53-60-51 PG 201/204 AND 51-10-01.SDR DL757070844Oven · overheatedSMOKEY SMELL IN MID GALLEY. LT BREAKER POPPED ON AFT SECTION OF MID GALLEY M301. VENT ON FWD PART OF MID GALLEY WAS WARM TO TOUCH EVEN AFTER TURNING OFF BOTH UTILITY BUSES. FOUND AFT OVEN MID GALLEY INOP. FWD TO MCO 25-20-01E. REPLACED OVEN IN MID, OVEN
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