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 I5PA20200327605Controller · leakingRH ENG BLEED FLUCTUATED IN FLIGHT. MX FOUND AND REPLACED A LEAKING RFCC WITHOUT FURTHER DEFECTSSDR I5PA20200327604Pressure Switch · faultyRH ENG LOW OIL PRESSURE LIGHT AND EICAS MESSAGE INTERMITTENT. MX FOUND AND REPLACED FAULTY LOW OIL PRESSURE SWITCHSDR I5PA20200327203Ignition Lead · shortedRH ENG IGNITION SYS 1 CIRCUIT BREAKER EXTENDED DURING START. ISSUE WAS ISOLATED TO A SHORTED IGNITION LEAD AND REPLACED WITHOUT FURTHER ISSUESSDR I5PA2020031675702Starter · wornAPU ABORTED START. TROUBLE SHOT AND FOUND STARTER BRUSHES WORN. REPLACED STARTER, PERFORMED OPERATIONAL CHECKS AND NUMEROUS STARTS WITH NO ISSUES. APU OK FOR SERVICE.SDR I5PA2020030875701Eec · intermittentRH ENGINE HUNG START AFTER PUSHBACK. ASSOCIATED WITH EICAS MESSAGE R ENG SEC CONT. PROBLEM ISOLATED TO EEC REPLACEMENT. REPLACED RIGHT EEC -ENGINE IDLE RUN NORMAL.SDR I5PA2020022075703Fmc · inoperativeRH FLIGHT MANAGEMENT COMPUTER FAILED PRIOR TO PUSHBACK. PART WAS REPLACED AND CONFIRMED OPERATIONALSDR I5PA2020021547702Starter · damagedRH ENG STARTER HAD ABNORMAL FINDINGS DURING ROUTINE SERVICING. PART WAS REPLACED WITHOUT FURTHER DEFECTSSDR I5PA2020020375701Hose · leakingRH ENGINE BLEED FLUCTUATES IN FLIGHT. ISSUE WAS ISOLATED TO A LEAKING PNEUMATIC LINE AT THE HP LIOT WHICH WAS REPLACEDSDR I5PA2020012807702Starter · making metalRIGHT ENG STARTER WAS REPLACED DUE TO OUT OF LIMIT CHIP DETECTOR FINDINGS DURING ROUTINE SERVICING OF THE STARTER.SDR I5PA2020012405701Controller · faultyL1 WINDOW ARCING IN FLIGHT. PROBLEM WAS ISOLATED TO A FAULTY WINDOW HEAT CONTROLLERSDR I5PA2020010675703Probe · unserviceableETOPS SIGNIFICANT ITEM: REF. MEL FOR F/O PITOT PROBE EICAS MSG. REMOVED AND REPLACED F/O PITOT PROBE AND OPS CHECKED NORMAL PER AMM 30-31-00. CLEARED DMI PLACARD REMOVED.SDR I5PA2020010675702Controller · unserviceableETOPS SIGNIFICANT ITEM: REF. MEL FOR CABIN ALT AUTO 2 STATUS MESSAGE, REMOVED AND REPLACED CABIN PRESSURE CONTROLLER 2 PER AMM 21-31-02. OPS CHECK NORMAL, NO FURTHER FAULT STATUS MESSAGE NOTED. CLEARED DMI PLACARD REMOVED.SDR I5PA2020010675701Pilot Valve · unserviceableMGE301 FLIGHT INTO PNI, CREW EXPERIENCED RIGHT ENGINE BLEED FAILURE ALONG WITH RIGHT PACK INOP. CREW FOLLOWED QRH AND LANDED SAFELY IN PNI. MAINTENANCE CREW REPLACED RH 14TH STAGE PILOT VALVE AND PERFORMED OPERATIONAL CHECK WITH NO ABNORMALITIES. AIRCRAFT PSDR I5PA2019090475702Cone · dentedDURING HEAVY MAINTENANCE PHASE "C" CHECK, FOUND DENT ON #1 ENGINE EXHAUST CONE REQUIRING REPAIR.SDR I5PA2019090300000Skin · corrodedDURING HEAVY MAINTENANCE PHASE "C" CHECK, FOUND UPPER SKIN SURFACE CORROSION ON HORIZONTAL STABILIZER REQUIRING MAJOR REPAIR.SDR I5PA2019062937572Relay · intermittentDISCREPANCY - TAT PROBE CAUTION MSG ASSOCIATED WITH LOTS OF AP, AT, VNAV, LNAV, EPR GAGE, SOME OF THE PERFORMANCE DATA. REMOVED AND REPLACED TAT CURRENT SENSING RELAY.SDR I5PA201906227571Probe · inoperativeTAT PROBE CAUTION MESSAGE ASSOCIATED WITH LOTS OF OF AP, AT, VNAV, LNAV, EPR GAGE, SOME OF THE PERFORMANCE DATA. REMOVED AND REPLACED TAT PROBE.SDR I5PA2018101600001Apu · unserviceableAPU REMOVED AND REPLACED DUE TO HIGH EGT HISTORY DURING OPERATION.SDR I5PA2018F00128Transceiver · intermittentETOPS SIGNIFICANT ITEM (NON-EVENT). WX RADAR ONLY WORKS INTERMITTENTLY.SDR I5PA2018F00129Anti-Ice Valve · inoperativeETOPS SIGNIFICANT ITEM (NON-EVENT). NR 1 ENG ANTI-ICE VALVE INOP.SDR I5PA201808220001Module · inoperativeAPU DUCT PRESSURE LOW.SDR I5PA201807090001Regulator · inoperativeRT ENG BLEED OFF LITE, R PACK OFF LITE ON DURING CLIMB OUT.SDR I5PA201806080001Transceiver · inoperativeHF RADIO DOES NOT TRANSMIT OR RECEIVE.SDR I5PA2018021675702Not Reported · multiple failDURING CLIMB OUT, CAPTAIN`S AIRSPEED, VERTICAL SPEED, AND ALTIMETER FAILED. CREW AIR RETURNED TO DEPARTURE AIRPORT AND THE PROBLEM WAS ADDRESSED BY MX.SDR I5PA2018020475701Windshield · cracked2 HOURS PRIOR TO LANDING, THE CAPT WINDSHIELD SHATTERED. THE FLIGHT CREW DECLARED AN EMERGENCY, DESCENDED IN ALTITUDE AND LANDED SAFELY AT 0846Z.SDR I5PA201801270001Windshield · crackedCAPT WINDSHIELD SHATTERED 1 HOURS AFTER TAKE OFF, PRIOR TO THE WINDSHIELD SHATTER, CREW NOTICED ARCING IN FIGHT. WINDSHIELD AND WINDOW HEAT CONTROLLER WAS REPLACED PER APPLICABLE AMM, ALL TEST VERIFIED SATISFACTORY PER OPS CHECK IN APPLICABLE AMM.SDR I5PA2017032802Discharge Tube · brokenAFT CARGO FIRE BOTTLE NR 2 DISCHARGE LINE BROKEN. REPLACED DISCHARGE LINE TUBE PER AMM 26-23-02. WORK ACCOMPLISHED ON ATS JOB 722361 NRC 00348.SDR I5PA2017032818Support · chafedNR 2 PYLON FWD SUPPORT FOR PNL NR 445AR CHAFED FWD SUPPORT (CHORD). REMOVED AND REPLACED PER SRM 51-40-05, 51-40-08 DWG 313N3052 AND 313N3018 AND SRM 51-40-02 WORK ACCOMPLISHED ON ATS JOB 722361 NRC 00279.SDR I5PA2017032817Hinge · corrodedLVL 2 CORROSION ON MAIN CARGO DOOR HINGES 3-6. REMOVED AND REPLACED HINGES PER ER 17-01722 REV 1R DTD 3/21/2017 WITH 8110-0 DTD MARCH 20 2017. WORK DOCUMENTED ON JOB 722361 CARD 00118SDR I5PA2017032816Winglet · corrodedLT WINGLET LWR AFT CORNER HAS AREA OF CORROSION BLENDED AND REFINISHED PER ER-17-01606 REV 1R, CORROSION LVL 1, MAJOR REPAIR. WORK ACCOMPLISHED ON JOB 722361 CARD 00294.SDR I5PA2017032815Attach Bracket · gougedLT WING ATTACH BRACKET ABOVE FWD END OF TRUNNION LINK IS GOUGED. REMOVED AND REPLACED ATTACH BRACKET PER SRM 51-40-02 AND GOOD FUNCTIONAL CHECK OF BONDING WIRE PER SWPM 20-20-10. WORK ACCOMPLISHED ON JOB 722361 NRC 00150.SDR I5PA2017032814Plate · chafedLT PYLON CUTOUT FOR PNL 434BL, AFT FLANGE IS CHAFED. REMOVED, FABRICATED AND REPLACED AFT FLANGE (PLATE) PER SRM 54-51-71, 51-40-02 AND DWG 313N3022. WORK PERFORMED ON JOB 722361 NRC 00282.SDR I5PA2017032813Skin · corrodedFORWARD ACCESS DOOR 113AL CORRODED AT AFT EDGE AND NEAR DRAIN VALVE, CORROSION LEVEL 2. REPAIRED PER ER 17-01609 REV 1R WORK DOCUMENTED ON JOB 722361 CARD 00124.SDR I5PA2017032812Skin · dentedFUSELAGE SKIN DENT BS 1400 3" BELOW STR 25L. REPAIRED PER ER 17-01586 ON JOB 722361.SDR I5PA2017032875711Floorbeam · damagedDAMAGED FLOOR SUPPORT BS1016 WL208.10 LBL 25-LBL 45. REMOVED AND REPLACED PER SRM 51-40-02 AS DOCUMENTED ON ATS JOB 722361 CARD 00274.SDR I5PA2017032810Splice Plate · crackedMAIN CARGO BAY FLOOR SPLICE BS 1020 IS CRACKED AT CARGO HANDLING SIDE RAIL ATTACH POINT LBL50. DOCUMENTED ON ATS JOB 722361 CARD 00019. REMOVED AND FABRICATED, INSTALLED NEW SPLICE PLATE PER DWG 144N5020 AND SRM 51-40-02.SDR I5PA2017032809Floor Panel · puncturedPUNCTURE IN FLOOR PNL FWD CARGO COMPARTMENT BS 688. REMOVED, FABRICATED AND INSTALLED FLOOR PNL PER SRM 51-40-05, 51-40-02, 51-40-03, 51-40-06, 51-20-01 AND DWG 453N1805 AS DOCUMENTED ON ATS JOB 722361 CARD 00056.SDR I5PA2017032808Attach Angle · crackedFIRE BOTTLE ATTACH ANGLE CRACKED AT BULKHEAD 1180 LBL 5 WL188. REMOVED, FABRICATED AND INSTALLED ANGLE IAW SRM 51-40-02, SRM 51-40-05, SRM 51-20-01 AND DWG 453N2700 AS DOCUMENTED ON ATS JOB 722361 CARD 00318.SDR I5PA2017032807Light · inoperativeFWD ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED LIGHT AND PERFORMED SATISFACTORY LIGHT TEST PER AMM 33-51-06. DOCUMENTED ON ATS JOB 722361 CARD 00061.SDR I5PA2017032806Support Angle · crackedCARGO FIRE BOTTLE SUPPORT ANGLE CRACKED AT BS 1188 WL 16 161 LBL 5. REMOVED, FABRICATED AND REPLACED IAW SRM 51-40-02, 51-20-01 AND DWG 453N2800 AS DOCUMENTED ON ATS JOB 722361 CARD 00300.SDR I5PA2017032805Support · corrodedBS 1640 BULKHEAD UPPER SUPPORT LBL8 HAS CORROSION ON AFT SIDE(LVL 2). REMOVED, FABRICATED AND REPLACED SUPPORT (MAJOR REPAIR) PER SRM 51-21-14, 51-21-15, 51-40-02, 53-60-53 AND DWG PL 453N1010. WORK ACCOMPLISHED ON ATS JOB 722361 CARD 00304.SDR I5PA2016050275701Window · crackedON DESCENT INBOUND, AIRCRAFT EXPERIENCED R1 WINDOW OUTER PANE HAD CRACKED. EMERGENCY PROCEDURES WERE FOLLOWED AND ACFT LANDED IN THE NEAREST SUITABLE AIRPORT, SAFTELY.SDR ASMF200512005Starter · damagedAIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE RT ENGINE WAS REJECTED WITH N1 FALLING AND EGT INCREASING. THE RT STARTER AND VALVE WERE REPLACED IAW MM 80-11-01 AND MM 80-11-02 RESPECTIVELY, TESTED CORRECT.SDR ASMF200510010Igniter Box · failedCAPTAIN REPORTED THAT DURING RIGHT ENGINE START WITH IGNITION SELECTOR IN POSITION ONE, THE RIGHT ENGINE EGT DID NOT INCREASE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING MAINTENANCE REVISION WAS DETECTED THE CABLE OF THE SYSTEM TWO DAMAGED. THE EXCITER IGNITSDR FE5F200300004Skin · crackedDURING SC12 CHECK, A 4.6250 INCHES LONG SPAN WISE CRACK IS REVEALED BETWEEN OSS 831.5 AND OSS 836 ON LT WING LEADING EDGE LOWER SURFACE SKIN. ACTION: REQUEST MFG ASSISTANCE AND IAW MFG'S RESPONSE, REPAIR THE CRACK.
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