Boeing 757-24APF
Service difficulty reports · 16,054
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 = '75724APF' 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 = '75724APF' 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 IPXA2025100857342Skin · damagedRIGHT EXTERNAL UPPER FUSELAGE, STA 540-560 BETWEEN STR 7R-8R HAS (1EA) HOLE CAUSED BY LIGHTNING STRIKE AT SKIN.PERFORMED HFEC SURFACE INSPECTION ON EXTERNAL SKIN ONLY AT STA 540-560 BTW STR 7R-8R IAW. NTM 51-00-19 PART6.INSTALLED FASTENER ON. RH EXTERNAL UPPERSDR IPXA2025092908881Latch · gougedCREW ENTRY DOOR LOWER CAM LATCH HAS A GOUGE APPROVED.SDR IPXA2055092908712Latch · gougedCREW ENTRY DOOR UPPER CAM LATCH HAS A GOUGE APPROVED.SDR IPXA2025093038715Scavenge Pump · malfunctioned30 MIN OF FLIGHT, 0.5 OF FUEL FROM RIGHT TANK TRANSFERRING TO CENTER TANK. NO CROSSFEED WAS USED. LT TANK SCAVENGE PUMP BEGAN PULLING CTR TANK FUEL AT 60% WHICH CAUSED 1500 LB IMBALANCE AT 1HR MARK. RT DEFUEL VALVE BODY OPS CHECK GOOD IAW AMM 28-26-01-790-80SDR IPXA2025092638715Fuel Sys · malfunctionedAT 30 MIN OF FLIGHT, 0.5 OF FUEL FROM RIGHT TANK. NO CROSSFEED WAS USED. LT TANK SCAVENGE PUMP BEGAN PULLING CTR TANK FUEL AT 60% WHICH CAUSED 1500 LB IMBALANCE AT THE1 HR MARK.SDR IPXA2025092531819Adc · malfunctionedATB, LOSS L AIR DATA DURING CLIMB-OUT AROUND 400FT. REMOVED AND REPLACED LEFT ADC PER AMM 34-12-01. OPS CHECK NORMAL.SDR IPXA2025100722583Strap · corrodedAPU DOOR SUPPORT STRUCTURE AFT STRAP SHOWS SIGNS OF CORROSION. REMOVED OUTER STRAP, REPAIR DOUBLER (-1), FILLER (-3), STRAP (-2) AND FILLER (-4) FROM APU DOOR SUPPORT STRUCTURE IAW SRM 51-40-02-0G-0. INSTALLED -1 DOUBLER, -2 STRAP, -3 FILLER AND -4 FILLER ANSDR IPXA2025102197638Cam · damagedCREW ENTRY DOOR FWD FRAME UPPER & LOWER LATCH CAM HAS GOUGED. REMOVED LATCH, CREW ENTRY DOOR UPPER CAM IN REFERENCE TO B757 CMM 52-11-08 AND SRM 51-40-02-0G-0. INSTALLED LATCH, CREW ENTRY DOOR UPPER CAM IAW CMM 52-11-08 AND SRM 51-40-02-0G-0. INSTALLED LATCSDR IPXA2025101592752Frame · corrodedRIGHT FWD FUSELAGE WASTE PANEL ACCESS HAS CORROSION INSIDE FRAME, FLL-011, ACCOMPLISHED REPAIR PER EO-95404-REQ1 AND VT-SAA EA 757-5249-01-B0574, REV. IR.SDR IPXA2025092497638Cam · gougedCREW ENTRY DOOR FWD FRAME UPPER & LOWER LATCH CAM HAS GOUGED.SDR IPXA2025100676445Strap · corrodedAPU INLET DOOR SUPPORT STRUCTURE FWD STRAP SHOWS SIGNS OF CORROSION. REMOVED FWD STRAP PN: 148N3138-20 AND UPPER MIDDLE ANGLE PN:148N3152-2 AT APU INLET DOOR STRUCTURE IAW SRM 51-40-02-0G-0. REMOVED LOWER MIDDLE ANGLE AND FWD LOWER ANGLE AT APU INLET DOOR STRUSDR IPXA2025092269443Valve · faultedATB, CLIMB OUT PASSING 24000€™ L OIL TEMP WAS IN THE AMBER RANGE (165°) QRH COMPLETED ACCOMPLISHED AIR TURNBACK. REMOVED AND REPLACED L/H ENG AIR/OIL HEAT EXCHANGER VALVE IAW AMM 79-21-08. OPS AND LEAK CHECKS PERFORMED IAW AMM 71-00-00 NO LEAKS NOTED AND OPSDR IPXA2025091851427Window · damagedNR 1 WINDSHIELD HAS MATERIAL STREAKING DOWN WHICH CANNOT BE REMOVED BY MX. SAFETY OF FLIGHT ISSUE. DUE TO OBSCURING FIELD OF VIEW. CLEANED CAPT 1L WINDOW PER SOPM-20-30-03. NO OBSCURING FIELD OF VIEW. OK FOR FLIGHT.SDR IPXA202509171427Windshield · damagedCA NR 1 WINDSHIELD HAS MATERIAL STREAKING DOWN WHICH CANNOT BE REMOVED BY MX. SAFETY OF FLIGHT ISSUE. DUE TO OBSCURING FIELD OF VIEW.SDR IPXA2025091632906Acm · odorLEFT PACK MODERATE BURNT ODOR RIGHT PACK MODERATE ODOR NOT BURNT SOME EYE IRRITATION AWARENESS BOTH CA AND F/O. R & R AIR CYCLE MACHINE I.A.W B757 MM 21-51-03. OPS CHECK, AND LEAK CHECK SATISFACTORY. NO CURRENT EVIDENCE OF BURNT ODOR PRESENT. OK FOR CONTINUESDR IPXA2025091962906A/C Pack · odorLEFT PACK MODERATE BURNT ODOR RIGHT PACK MODERATE ODOR NOT €ŒBURNT€? SOME EYE IRRITATION AWARENESS BOTH CA AND F/O T/S AND FOUND LEFT PACK TO BE CAUSE OF SMELL, SUSPECT ACM TO BE BURNING BEARINGS. DMI CONTINUES, PLACED ACM AND SEALS ON ORDER. IAW FIM 21-20-SDR IPXA2025100103715Skin · crackedUPON WORKING EO-88069-REQ047 REV1, TASK CARD T3F18E0054EL6, FOUND EVIDENCE OF POSSIBLE CRACK AT HOLE LOCATION NUMBER 10 L/W UPPR SKIN OF #1 ENG. PYLON. ATA-54-00.PERFORMED BLEND-OUT ON CORRODED AREAS LOCATED AT UPPER FACE SURFACES OF INBD AND OUTB DRAG FITTINSDR IPXA2025091629291Indication Sys · false indicationDESCENDING THRU 12,00 MSL, FLAPS 1, EICAS MESSAGE FOR GEAR NOT DOWN, DISPLAYED FOR APPROXIATELY 2 SECONDS. PERFORMED OPS CHECK OF RADIO ALT SYS IAW AMM 34-33-00-715-001 OPS CHECK GOOD WORK PERFORMED BY CAT 3 MECHANICSDR IPXA2025091129291Warning Message · illuminatedDESCENDING THRU 12,00 MSL, FLAPS 1, EICAS MESSAGE GEAR NOT DOWN DISPLAYED FOR APPROXIATELY 2 SECONDS. PERFORMED GPWS FAULT/BITE CHECK .BITE FAULT OF LEFT RADIO ALTIMETER SYSTEM EXTERNAL FAULT ,FLIGHT LEG 3.THIS IS THE LEG WITH LANDING GEAR NOT DOWN MSG.SDR IPXA2025091892090Angle · corrodedAFT UPPER FUSELAGE AT APU INLET AREA, STA 1787.45-1825, STR 6R, AFT LOWER ANGLE DELAMINATED. INSTALLED NEW AFT LOWER ANGLE IAW SRM 51-40-02-0G.SDR IPXA2025092198447Support Angle · crackedFWD CARGO COMPT BS 560 E5 EE RACK BULKHEAD DECOMPRESSION PANEL SUPPORT O/B ANGLE HAS A CRACK. INSTALLED NEW ANGLE FROM FWD CARGO COMPT BS 560 E5 EE RACK BULKHEAD DECOMPRESSION PANEL SUPPORT IAW SRM 51-40-02-0G.SDR IPXA2025092190774Floor Support · corrodedANGLE CORRODED AT STA 1716 RBL 33 UNDER AFT FLOOR DECK. INSTALLED NEW ANGLE FROM AT STA 1716 RBL 33 UNDER AFT FLOOR DECK IAW B757-200 SRM 51-40-02-0G.SDR IPXA2025092191420Cover · chafedNR 1 ENG UPPER PYLON GAP PANEL HAS LARGE CHAFE ON PREVIOUS METAL REPAIR DOT 55-104. INSTALLED NEW DOUBLER IAW B757-200 AMM 51-21-15. VERIFIED INSTALLATION OF DOUBLER. REVIEWEDSDR IPXA2025091762364Intercostal · corrodedRIGHT W/W STA 1040 - 1060, RBL 62 INTERCOSTAL T-CHORD CORRODED. INSTALLED NEW T-CHORD IAW B757-200PF SRM 51-40-02-0G-0.SDR IPXA2025092164563Doubler · crackedRIGHT WING, PANEL 621PB, TRACK CUTOUT, BRACKET IS BENT AND HAS A CRACK. DOT 103-788. INSTALLED NEW DOUBLER (BRACKET) ON PANEL 621PB, IAW B757-200PF SRM 51-40-02-0G. REVIEWEDSDR IPXA2025092150063Support Angle · delaminatedAFT UPPER FUSELAGE AT APU INLET AREA, BS 1787.45, STR 6R, FWD LOWER ANGLE DELAMINATED. INSTALLED NEW FWD LOWER ANGLE IAW SRM 51-40-02-0G.SDR IPXA2025092248757Support Channel · crackedRIGHT WW FWD SEAL RETAINER SUPPORT FRAME O/B AREA HAS A CRACK. INSTALLED SUPPORT CHANNEL AT RT WW IAW SRM 51-40-02.SDR IPXA2025092341988Crank Assy · gougedCREW ENTRY DOOR FWD EDGE LOWER ROLLR CRANK FITTING GOUGED. VERIFIED ACCOMPLISHED SREO 14721-REQ001 REV 1.SDR IPXA2025092341857Crank Assy · gougedCREW ENTRY DOOR FWD EDGE UPPER ROLLER CRANK FITTING GOUGED AT BOTTOM SIDE. VERIFIED ACCOMPLISHED SREO 14721-REQ001 REV 1.SDR IPXA2025090841988Roller · gougedCREW ENTRY DOOR FWD EDGE LOWER ROLLR CRANK FITTING GOUGED.SDR IPXA2025090841857Fitting · gougedCREW ENTRY DOOR FWD EDGE UPPER ROLLER CRANK FITTING GOUGED AT BOTTOM SIDE.SDR IPXA2025090405528Seal · dirtyL1 DOOR IS VERY DIFFICULT TO OPEN. ADJUSTED AND CLEANED L1 DOOR SEAL AND DOOR LINING REF. AMM 52-12-00. DOOR OPS CHECKS NORMAL.SDR IPXA2025091690459Strap · corrodedAPU INLET SUPPORT STRUCTURE AFT STRAP SHOWS SIGNS OF CORROSION. INSTALLED 1EA REPAIR DOUBLER (1), 1EA STRAP (2), 1EA FILLER (3), 1EA FILLER (4) AND 9EA NUTPLATES ON APU AIR INLET SUPPORT STRUCTURE AT STA 1825 BETWEEN STGRS 3R AND 6R IAW B757-200PF SRM 53-80-15SDR IPXA2025090482863Window · damagedL2 WINDOW HEAVILY SCRATCHED AND IMPAIRS VIEW DURING TAXI IN WITH BRIGHT LIGHTS. REMOVED AND REPLACED L2 WINDOW IN REF TO AMM 56-11-02/401. LEAK CHECK GOOD. REF MM 05-51-24-201.SDR IPXA2025090382863Window · scratchedL2 WINDOW HEAVILY SCRATCHED AND IMPAIRS VIEW DURING TAXI IN WITH BRIGHT LIGHTS LEAK CHECK GOOD. REF MM 05-51-24-201.SDR IPXA2025091653930Support Angle · corrodedAPU INLET SUPPORT STRUCTURE FWD STRAP O/B END SHOWS SIGNS OF CORROSION , HAS 3 EA NUT PLATES PULLED THROUGH STRAP WHITH A LAYER OF WHITE POWDER. REMOVED AND REPLACED SUPPORT ANGLES IAW SRM 51 GUIDELINES, USING THE ORIGINAL PARTS AS SAMPLE IAW UPS GMM REV 12 SDR IPXA2025090211532Hose · failedLEFT HYD QTY ANNUNCIATED ON FINAL APPROACH. S HORTLY AFTER LT SYS PRESSURE WAS LOST, AFTER GO AROUND ACCOMPLISHED, QRH PROCEDURE AND RETURNED FOR LANDING. QTY DEPLETED BEFORE LT ENG. SERVICING HOSE WAS REPLACED AND LEAKED CHECK IAW AMM 29-18-01. BOTH HOSES SDR IPXA2025082811532Hydraulic System · leakingEMERGENCY DECLARED, LT HYD QTY (EICAS C) ANNUNCIATED ON FINAL APPROACH. SHORTLY AFTER LEFT SYSTEM PRESSURE WAS LOST, AFTER GO AROUND ACCOMPLISHED QRH PROCEDURE AND RETURNED FOR LANDING. QTY DEPLETED BEFORE L ENG PERFORMED OPS AND LEAK CHECK OF LT ENGINE DRIVESDR IPXA2025090390433Floor Panel · damagedMAJOR REPAIR, MC FLOOR PANEL DAMAGE INSTALLED FLOOR PANEL AT POS. 7 REF. 25-55-07. STILL REQUIRES SEALANT AND ROLLER INSTALL. REF. ITEM 47 FOR COMPLETIONSDR IPXA2025902000433Floor Panel · not reportedMC FLOOR PANEL P/N 143N5457-26 DAMAGE INSTALLED FLOOR PANEL AT POS. 7 REF. 25-55-07. STILL REQUIRES SEALANT AND ROLLER INSTALL. REF. ITEM 47 FOR COMPLETIONSDR IPXA2025082506213Window · inoperativeLEFT FWD WINDOW HEAT INOPERATIVE. R & R L1 WINDOW IAW M/M 56-11-02.SDR IPXA2025090493586Bracket · corrodedAFT CARGO COMPARTMENT HAS CRACKED BRACKET AND STRUCTURE AT BS 1681.8. 03-094. REMOVED PLATE ASYY FROM AFT CARGO COMPARTMENT SAT 1681.8 TO FURTER EVALUATE IAW SRM 51-40-02-OG-0. REMOVED 1EA NUT PLATE FROM PLATE ASYY IAW SRM 51-40-02-OG-0. REMOVED 1 EA FLOOR SDR IPXA2025090597004Fitting · gougedRIGHT WING. FLAPS GUIDE ROLLER FITTING HAS CHAFING ON THE LOWER SURFACE.(DM08). ACCOMPLISHED REPAIR PER EO-94899-REQ1 AND VT-SAA EA 757-5750-01-B0560.SDR IPXA2025090495838Tee Angle · brokenR/H WING. I/B FLAP HAS BROKEN T-ANGLE SUPPORT LOCATED AT O/B SIDE OF THE FLAP.(DM09) ATA57. INSTALLED TEE-ANGLE SUPPORT AT R/H WING. I/B FLAP. LOCATED AT O/B SIDE OF THE FLAP I.A.W. B757-200PF SRM 51-40-02-0G-0 AND BOEING DWG NO.113N2605.SDR IPXA2025082287433Flap System · malfunctionedEMERGENCY DECLARED ON APPROACH, WHEN CONFIG., TE FLAP DISAGREE EICAS MSG. FLAPS @ BETWEEN 0 AND 1 REMOVED AND REPLACED RT FLAP TRANSMITTER PER AMM 27-58-03/401. PERFORMED ADJUSTMENT/TEST PER AMM 27-58-01/501. FLAPS/SLATS OPERATE NORMAL. ACFT OK FOR SERVICE.SDR IPXA2025091564404Tail Cone · damagedMAJOR REPAIR, DAMAGE ON TOP OF TAILCONE AREA BELOW RUDDER ALL STEPS OF EO-94785-REQ2 COMPLETED. THIS DEFERRAL IS NOW CLOSED.SDR IPXA2025082160238Engine · faultedDIVERSION, EMERGENCY DECLARED, DURING CLIMB PASSING APPROXIMATELY 20,000 FT WITH EPR'S MATCHED AT CLIMB POWER WE NOTICED RIGHT HAND ENGINE EGT AMBER AT 800 DEGREE AND CLIMBING. IN ADDITION, N1 AND FUEL FLOW WERE SEE ATTACHED PAGE. INSPECTED,CLEANED,PRESSURE TSDR IPXA2025082060238Engine · overtempDIVERSION, EMERGENCY DECLARED, DURING CLIMB PASSING APPROXIMATELY 20,000 FT WITH EPR'S MATCHED AT CLIMB POWER WE NOTICED RIGHT HAND ENGINE EGT AMBER AT 800 DEGREE AND CLIMBING. IN ADDITION, N1 AND FUEL FLOW WERE SEE ATTACHED PAGE. PERFORMED FIM TASK 73-21-00/SDR IPXA2025090630285Skin · dentedLEFT FWD SIDE OF FUSELAGE HAS 4EA DENTS AFT OF RADOME AT APPROX FS 211 L21L . REMOVED 2EA FASTENERS FOUND WITHIN 0.5" OF DENT PERIPHERY AT LT FUSELGE SKIN BETWEEN FRAMES 199.09/215.25 AND STGR 23L IAW SRM 51-40-02-0G-0. INSTALLED 2EA FASTENERS AT LT FUSELGE SSDR IPXA2025090530455Radome · dentedLEFT FWD SIDE OF FUSELAGE HAS A DENT AFT OF RAYDOME AT APPROX FS 205 L24L . 49-001 ATA 53-00. INSTALLED 1EA (-1) REPAIR DOUBLER AND 1EA (-2) FILLER ON L/H FWD SIDE OF FUSELAGE AFT OF RAYDOME AT APPROX FS L24L IAW E.A.#:757-5310-01-B0557 REV:P1, STEP 22 AND 2
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