Boeing 757-29J
Service difficulty reports · 245
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 = '75729J' 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 = '75729J' 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 I5PA2026071575702Shutoff Valve · inoperativeFLIGHT 305, RT ENG BLEED ISSUES. R & R RT ENG HPSOV PER AMM OPS CHECK NORMAL.SDR I5PA2026071575701Pilot Valve · inoperativeFLIGHT 305, RT ENG BLEED ISSUES. R & R RT ENG HS PILOT IAW AMM, OPS CHKD NORMAL.SDR I5PA2026062975708Eec · faultedLEFT ENGINE HIGH EGT. R & R LT ENGINE EEC IAW AMM.SDR I5PA2026062675707Fmc · faultedRIGHT FMC INOPERATIVE. R & R RT FMC IAW AMM. OPS CHKD NORMAL.SDR I5PA2026062275706Pressure Switch · faultedFLIGHT MGE301, APU INFLIGHT START FAILED. FOUND APU DIFF PRESSURE SWITCH FAULTY. R & R DIFFERENTIAL PRESSURE SWITCH IAW AMM. OPS CHECK NORMAL, APU VERIFICATION FLIGHT SUCCESSFUL.SDR I5PA2026062275705Gcu · inoperativeRIGHT BUSS TIE LIGHT ILLUMINATED. R & R RT GCU IAW AMM OPS CHECK NORMAL.SDR I5PA2026062275704Idg · inoperativeRIGHT ENG IDG INOPERATIVE. (DEFERRED PER MEL 24-00-01). R & R RT ENG IDG IAW AMM, OPS CHKD NORMAL.SDR I5PA2026061375703Gcu · inoperativeRIGHT BUSS TIE TRIPS WHEN POWER TRANSFERED. R & R RT GCU IAW AMM, OPS CHECKED NORMAL.SDR I5PA2026061275702Fmc · inoperativeRIGHT FMC INOPERATIVE. R & R THE LT FMC IAW AMM. OPS CHECKED NORMAL.SDR I5PA2026061275701Fmc · inoperativeLEFT FMC INOPERATIVE. R & R LT FMC IAW AMM. OPS CHECKED NORMAL.SDR I5P2026F00000Apu · inoperativeAPU INOP. REPLACED APU PER TASK CARD.SDR I5PA2026042175704Eec · faultyFLIGHT MGE601. LT ENG LOW OIL PRESS AFTER LANDING. FOUND FAULTY EEC. R/R LH ENG EEC PER AMM, OPS CHECK NORMAL.SDR I5PA2026042175702Solenoid · failedPERFORMED APU BITE PER FIM. FOUND LOW OIL PRESS APU DE-OIL SOLENOID FAULTY. REPLACED SAME PER AMM. OPS AND LEAK CHECK OK. SUCCESSFUL APU INFLIGHT START PERFORMED.SDR I5PA2026041875703Flex Line · leakingFLIGHT MGE601, AIR RETURN DUE LOW LEFT HYD QTY. FOUND HYD. FLEX LINE LEAK AT R MLG TILT ACTUATOR. R/R FLEX LINE AND SERVICED HYD. SYSTEM PER AMM. NO LEAKS DETECTED. AIRCRAFT RETURNED TO SERVICE.SDR I5PA2026041775702Apu · faultedFLIGHT MGE301, APU INFLIGHT START FAILED. OPENSDR I5PA2026040875701Shaft · shearedLEFT ENG HYDRAULIC PUMP. LEFT ENG EDP SHAFT FOUND SHEARED. R/R LEFT ENG EDP PER AMM. OPS CHECK, LEAK CHECK OK.SDR I5PA2026033075711Drive Unit · failedFLIGHT MGE301, WXR FAILED. REPLACED WXR DRIVE UNIT PER AMM.SDR I5PA2026033075710Igniter · wornFLIGHT MGE301, RIGHT ENGINE HUNG START. FOUND UPPER IGNITER PLUG WORN TO LIMITS. REPLACED IGNITER PLUG PER AMM.SDR I5PA2026033075709Fuel Control · faultedFLIGHT MGE301, RIGHT ENGINE HUNG START. FOUND FCU/EEC EPCS MESSAGE, REPLACED FCU PER AMM.SDR I5PA2026031975708Starter · faultedRIGHT ENGINE SLOW TO START. REPLACED RT ENGINE STARTER IAW AMM.SDR I5PA2026031875707Warning Message · false activationFLIGHT MGE400 - AIR RETURN. LT & RT EICAS COMPUTER STATUS MESSAGE. PERFORMED EICAS BITE, FOUND NUISANCE FAULTS. CLEARED FAULTS PER FIM. SWAPPED LT & RT COMPUTERS IAW FIM. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.SDR I5PA2026031675706Transceiver · faultyFLIGHT MGE600, WXR FAIL. FOUND AND REPLACED FAULTY WXR TRANSCEIVER PER AMM.SDR I5PA2026031575705Converter · leakingFLIGHT MGE600 - ESI / (AIR RETURN) RIGHT ENGINE BLEED OFF MESSAGE ON T/O. NO DUCT PRESSURE ON RIGHT SIDE. PERFORMED FIM, FOUND RFCC LEAKING. REPLACED RFCC IAW AMM.SDR I5PA2026031375704Fmc · inoperativeFLT MGE502, RT FMC INOP. REPLACED RH FMC PER AMM.SDR I5PA2026031275703Controller · inoperativeRIGHT PACK TEMP EICAS MESSAGE. REPLACED PACK TEMP CONTROLLER PER AMM. NO DEFECTS NOTED.SDR I5PA2026031275702Drive Unit · inoperativeFLT. MGE502, WXR FAILED. PERFORMED OPS CHECK OF WEATHER RADAR SYSTEM. FOUND DRIVE UNIT FAILED. REPLACED DRIVE UNIT PER AMM. NO DEFECTS NOTED.SDR I5PA2026031075701Transmitter · intermittentRIGHT ENGINE FUEL FLOW INDICATION INTERMITTENT. REPLACED FUEL FLOW TRANSMITTER IAW AMM.SDR I5PA2025101375702Ecu · faultyAPU PNEUMATICS INOPERATIVE. R & R APU ECU PER AMM. OPS CHECKED NORMAL.SDR I5PA2025101375701Shutoff Valve · faultyFLT: MGE831, APU FUEL VAL EICAS. R & R APU FUEL SHUTOFF VALVE IAW AMM, OPS CHECK NORMAL.SDR I5PA2025070575701Skin · corrodedMAJOR REPAIR: LEVEL 2 CORROSION FOUND AT BSTA 680-700 BETWEEN STRINGERS 26R/28R. REPAIRED CORROSION PER EO APA-0043-001 REV 1 DTD 28JUN2025 AND PER SRM 53-00-01 REPAIR 28.SDR I5PA2025061675701Smoke Detector · faultedAIR RETURN DUE TO MAIN CARGO FIRE WARNING DURING CLIMBOUTFOLLOWED BY POPPED CB. QRH CONSULTED, ACFT RETURNED TO HNL. MX T/S PER PRECISION AMM AND FOUND FAULTY SMOKE DETECTOR. R/R SAME, OPS CHK NORMAL. ACFT BACK IN SERVICE.SDR I5PA2025053075702Blade · wornFLT: N/A (MX INSP.) ESI: RH ENG LPC 1ST STAGE BLADE #17 FOUND OUT OF LIMITS R/R #17 AND #35 FAN BLADES PER AMM NO DEFECTS NOTED.SDR I5PA2025050675701Controller · faultyFLIGHT DECK TEMP HOT. R & R STBY PACK TEMP CONTROLLER PER AMM.SDR I5PA2025042875701Exciter · faultedFLT: MGE301. LH ENG DID NOT START ON IGNITOR 1 STARTED NORMAL ON BOTH. R/R LH ENG EXCITER 1 PER AMM.SDR I5PA2025031575702Pilot Valve · faultyFLT NO: N/A (MX INSP). ESI - PERFORMED RH ENG PNEUMATIC HEALTH CHECK. FOUND HS PILOT FAULTY. R/R RH ENG HS PILOT PER AMM 36-11-08. OPS CHECK NORMAL.SDR I5PA2025031275701Pressure Sensor · faultedFLT NO: MGE 401. ESI - APU SHUTDOWN 2X WHILE ENG STARTING. PERFORMED ECU BITE CHECK FOUND REVERSE FLOW MSG. R/R PRESSURE SENSOR PER AMM 49-61-04. OPS CHECK GOOD.SDR I5PA2025012575705Display · inoperativeFLT NO: N/A (MX INSP) ESI - FO MCDU INOP. REMOVED AND REPLACED FO MCDU PER AMM.SDR I5PA2025011775704Autothrottle Sys · malfunctionedMGE 300, EVENT - AIR RETURN DUE TO NO LNAV/VNAV AND AUTO THROTTLE. DEFERRED LNAV / VNAV AND AUTO THROTTLE.SDR I5PA2025012175703Fmc · inoperativeFLT NO: N/A, MX INSP, ESI - DISCREPANCY: LEFT FMC FAULT. SWAPPED LT AND RT FMC, FAULT FOLLOWED. PLACED RT FMC ON MEL. REMOVE AND REPLACED RT FMC PER AMM 34-61-00.SDR I5PA2025011275702Autothrottle Sys · inoperativeMGE 300 (EVENT) - AIR RETURN DUE TO: NO LNAV/VNAV, NO AUTO THROTTLE NO TMC INFO.SDR I5PA2025010475701Fmc · faultedFLT NO. MGE 300 (EVENT). AIR RETURN DUE TO: NO INFO ON PROGRESS PAGE BURN, TIME WIND UNABLE TO MAINTAIN COURSE. TEMP SELECT FOR THROTTLES INOP. NO LNAV / VNAV. - SWAPPED FMC FOR TROUBLESHOOTING PER AMM 34-61-01, PERFORMED BITE TEST PER FIM 22-02 TASK 801 TEST SDR I5PA2024122375702Control Valve · faultedLH ENG STARTER VALVE DOESNT OPEN WHEN SWITCHED TO RUN. R/R LH ENG STARTER CONTROL VALVE IAW AMM 80-11-02-024-001-P001.SDR I5PA2024121975701Surge Valve · faultedAPU AUTO SHUTDOWN ON ENG START. REPLACED APU SURGE VALVE PER AMM 49-52-00SDR I5PA2024112275704Control Valve · faultedEPCS FAULT MESSAGE HCC/EEC. R/R ACTIVE CLEARANCE CONTROL VALVE IAW AMM 72-53-90/601.SDR I5PA2024112275703Control Valve · faultyLEFT ENG STARTER VALVE TAKES LONG TO CLOSE AFTER ENG START UP. R & R LH ENG STARTER CONTROL VALVE IAW AMM 80-11-02-024-001-P001.SDR I5PA2024111375702Ecu · inoperativeAPU ELECTRICAL LOAD FLUCTUATES. REPLACED APU ECU PER AMM. OPS CHECK GOOD.SDR I5PA2024110375701Computer · intermittentFLT NO: MGE305 - EVENT (ETOPS- AIR RETURN) MULTIPLE EICAS MESSAGES. PERFORMED FIM AND FOUND LEFT EICAS COMPUTER INTERMITTENT. REPLACED LEFT EICAS COMPUTER PER AMM.SDR I5PA2024102075704Skin · corrodedDURING C CHECK, CORROSION WAS FOUND ON THE RH WING LOWER SKIN AT WS 187-211. CORROSION WAS REPAIRED PER BOEING ENGINEERING INSTRUCTIONS.SDR I5PA2024102075703Skin · corrodedDURING C CHECK, CORROSION WAS FOUND ON THE LH WING LOWER SKIN AT WS 187-213. CORROSION WAS REPAIRED PER BOEING ENGINEERING INSTRUCTIONS.SDR I5PA2024102075702Structure · corrodedDURING C CHECK, CORROSION WAS FOUND ON THE RH HORIZONTAL STAB BETWEEN STA 116.25-122.428, 140.25-148.48,153.61-156.17,164.53-174.10,176.299-180.10, 183.30-189.80,227.70-232.91,234.94-241.52, 267.43-276.25 AND 286.80-288.38. ALL WERE ADDRESSED AND REPAIRED PER
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