Boeing 767-238
Service difficulty reports · 109
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 = '767238' 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 = '767238' 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 2PSASDR7670901Failsafe · crackedON 5-13-09 AT 1600 HRS. NOTIFIED THAT WHILE COMPLYING WITH SB 767-53A0100 IAW AD 2004-19-06: ULTRASONIC TESTING OF THE LT AND RT STA 955 REAR BULKHEAD SIDE FITTING FAIL-SAFE STRAPS SHOWED POSSIBLE CRACKING OF BOTH FAIL-SAFE STRAPS AND RECEIVING THE NDT REPORT SDR 2009F00008Windshield · delaminatedRT NR1 WINDSHIELD FAILURE.SDR 7A7B20091192Slide · unwanted deployUNCOMANDED DEPLOYMENT OF OFF WING EVACUATION SLIDE.SDR 2009F00015Wire · misinstalledWHILE ACFT WAS ON GROUND, WITH JUST APU RUNNING, THE LT OVERWING SLIDE DEPLOYED. THE ESCAPE HATCH WAS NOT DISTURBED. THIS TOOK PLACE IN LFPB. THE ONLY THING DONE PRIOR TO DEPLOYMENT WAS THAT THE LEAD F/A PUSHED THE EMERGENCY LIGHTING TEST SWITCH AT THE L1 CONTSDR 2008FA0000850Pin · installedA SLIDE DEPLOYMENT OF THE RT AFT ENTRY DOOR OF THE ACFT WAS ATTEMPTED IN CONJUNCTION WITH A DITCHING DEMONSTRATION IN SUPPORT OF OUR FAR PART 125 CONFORMITY ASSESSMENT BY FSDO - 25. THE SLIDE DID NOT EXTRACT FROM THE DOOR BUSTLE AS THE DOOR WAS OPENED. UPON SDR 05212008001Clamp · failedTHE CREW REPORTED THAT AFTER A NORMAL TAKEOFF AND CLIMB, AND AFTER GOING INTO CRUISE THE LEFT ENGINE WOULD NOT PRODUCE GREATER THAN 70 PERCENT N1, 80 PERCENT N2 AND 1.00 EPR. THEY ALSO REPORTED THAT EICAS REPORTED A LEFT ENGINE OVERTEMP OF 451 DEGREES. THE CSDR 05290701Liner · departedDURING TAKEOFF FROM EGSS EN ROUTE TO KIAD MUCH OF THE FAN EXIT OUTER CASE LINER SEGMENT AFT OF THE FAN EXIT GUIDE VANES SEPARATED FROM THE NR 1 ENGINE ESN 716801. THE BRITISH AIRPORT AUTHORITY NOTIFIED MAXJET MAINTENANCE THAT THE DEPARTED LINER HAD BEEN FOUNDSDR L43A12170601Spar · corrodedA/C IS IN "C" CHECK, VISUAL INSPECTION POINTED TO POSSIBLE CORROSION IN RT INB MAIN FLAP. AFTER DISASSEMBLY OF FLAP THE AFT SPAR CHORD WAS FOUND TO HAVE CORROSION IN NUMEROUS PLACES. A REPLACEMENT MAIN FLAP HAS BEEN PURCHASED FOR INSTALLATION. DISCREPANCY ESDR STN121305Slide · detachedL1 DOOR SLIDE DETACHED FROM DOOR.SDR AUS20040349Cabin Pressure · malfunctioned(AUS) CABIN DIFFERENTIAL PRESSURE STUCK AT 8.6 PSI.SDR AUS20031211Water Heater · faulty(AUS) AFT GALLEY NR 1 WATER BOILER FAULTY.SDR AUS20031099Symbol Generator · failed(AUS) LT AND RT EFIS SYMBOL GENERATORS FAILED.SDR AUS20030841Link · sheared(AUS) RT INBOARD TRAILING EDGE FLAP LINK SHEARED ON OUTBOARD HINGE. LINK IS LOCATED BETWEEN AFT FLAP AND SLAVE DRIVE BELLCRANK.SDR AUS20030772Wire · shorted(AUS) RT ENGINE GENERATOR A' PHASE FEEDER CABLE CHAFED AND SHORT CIRCUITING TO ENGINE COWL.SDR AUS20030642Shutoff Valve · faulty(AUS) FLAP/SLAT HYDRAULIC SHUTOFF VALVE FAULTY.SDR AUS20030643Computer · faulty(AUS) LT FLIGHT CONTROL COMPUTER (FCC) FAULTY.SDR AUS20030472Solenoid · faulty(AUS) FLIGHT DECK DOORLOCK SOLENOID FAULTY.SDR AUS20021354Fan · failed(AUS) GASPER FAN FAILED.SDR AUS20021197Torque Tube · corroded(AUS) RH INBOARD FLAP TORQUE TUBE AND COLLAR FITTING CORRODED BEYONDLIMITS. FOUND DURING INSPECTION IAW AD/B767/108.SDR AUS20021002Pipe · cracked(AUS) LH HYDRAULIC SYSTEM HYDRAULIC PIPE TO HEAT EXCHANGER LOCATEDUNDER THE SAILBAOT FAIRING CRACKED. LOSS OF LH HYDRAULIC SYSTEM FLUID. LH HYDRAULIC CASE DRAIN FILTER CONTAMINATED.SDR AUS20021001Fuse · failed(AUS) RH MAIN LANDING GEAR UP' HYDRAULIC FUSE FAILED. FUSE MAIN RESET SPRING BROKEN.SDR AUS20020666Engine · leaking(AUS) APU LEAKING OIL. OIL FUMES IN CABIN.SDR AUS20020517Engine · malfunctioned(AUS) LT ENGINE HARD TO START DURING INFLIGHT START ON TEST FLIGHT FOLLOWING HEAVY MAINTENANCE.SDR AUS20020282Module · faulty(AUS) HYDRAULIC FILTER MODULE FAULTY.SDR AUS20020135Relief Valve · failed(AUS) HYDRAULIC PUMP PRESSURE RELIEF VALVE FAULTY. VALVE WAS BYPASSING FLUID.SDR AUS20020107Wire · burned(AUS) APU GENERATOR FEEDER CABLE BADLY BURNED. THE CABLE WAS ALSO LOOSE WITH INSULATION MISSING.SDR AUS20020005Fuel Control · faulty(AUS) LT ENGINE FUEL CONTROL UNIT SUSPECT FAULTY.SDR AUS20011248Fan Blade · failed(AUS) LT ENGINE FAN BLADE FAILED. BLADE EXITED THROUGH COWL.SDR AUS20011285Skin · debonded(AUS) NR 8 RT LEADING EDGE SLAT DISBONDED. FOUND DURING INSPECTION IAW AD/B767/73.SDR AUS20011284Pulley · worn(AUS) RT ENGINE THRUST CONTROL CABLE PULLEYS (2OFF) LOCATED AT STA 240.0 WERE FOUND TO BE WORN. FOUND DURING INSPECTION IAW AD/B767/118(EI 762-76-003).SDR AUS20011172Actuator · faulty(AUS) APU DOOR ACTUATOR FAULTY.SDR AUS20011204Fitting · corroded(AUS) LT AND RT INBOARD FLAP TORQUE TUBE SPLINES AND COLLAR FITTINGS CORRODED. FOUND DURING INSPECTION IAW AD/B767/108.SDR AUS20011065Motor · faulty(AUS) APU STARTER FAULTY.SDR AUS20011027Starter · burned out(AUS) APU STARTER MOTOR BURNED OUT. STARTER MOTOR HAD REMAINED ENGAGED FOLLOWING APU START.SDR AUS20010968Acoustic Panel · missing(AUS) RT ENGINE COLD STREAM DUCT ACOUSTIC PANELS MISSING.SDR AUS20010956Lanyard · missing(AUS) OXYGEN MASKS LOCATED AT SEATS 26J/K HAD MISSING LANYARDS (3OFF).SDR AUS20010680Fseu · faulty(AUS) FLAP/SLAT ELECTRONIC UNIT (FSEU) SUSPECT FAULTY.SDR AUS20011199Hose · leaking(AUS) RH MAIN LANDING GEAR TILT ACTUATOR HYDRAULIC HOSE LEAKING.SDR AU010308Hose · leaking(AUS) RT MAIN LANDING GEAR TILT ACTUATOR HYDRAULIC HOSE LEAKING.SDR AUS20010630Switch · faulty(AUS) LH HYDRAULIC TAIL SHUTOFF VALVE SWITCH MODULE FAULTY.SDR AU010081Switch · faulty(AUS) LT HYDRAULIC TAIL SHUTOFF VALVE SWITCH MODULE FAULTY.SDR AU001256Cover · missing(AUS) BULK CARGO VENT COVER MISSING. AD/B767/65 AND FAA AD FAD 92-02-12 REQUIRE THE COVER TO BE FITTED FOLLOWING REMOVAL OF THE BULK CARGO VENTILATION VALVE IAW BOEING SB 767-21A0098.SDR AU001163Panel · separated(AUS) RT STRUT TRUNNION ACCESS PANEL SEPARATED FROM AIRCRAFT. THE PANEL CAUSED IMPACT DAMAGE TO THE RT HORIZONTAL STABILISER LEADING EDGE AND TOP SKIN. FOLLOWING REMOVAL OF THE REMAINS OF THE DEPARTEDPANEL THE HOLDING TORQUE ON THE ANCHOR NUTS WAS CHECKED WITHSDR AU000694Control Cable · worn(AUS) ENGINE THRUST CONTROL CABLES TLA-2 AND TRA-2 LOCATED IN THE RHFORWARD CARGO HOLD WERE WORN BEYOND LIMITS. FOUND DURING INSPECTION IAW AD/B767/118.SDR AU000643Control Cable · worn(AUS) ENGINE THRUST CONTROL CABLES PN TLA2 AND PN TRA2 WORN BEYOND LIMITS. FOUND DURING INSPECTION IAW AD/B767/118.SDR AU000852Bellcrank · faulty(AUS) PCA BELLCRANK SHEAR RIVETS FAILED. FOUND DURING INSPECTION IAW EI 767-027-0112 AND FAA AD 2000 17-05.SDR AU000549Pin · missing(AUS) LT INBOARD AILERON LOWER HALF PCA SUMMING LEVER/INPUT ROD PIVOT LINK PIN MISSING.SDR AU000233Wire · burned(AUS) CARGO HOLD FLOOR WIRING AND INSULATION BLANKET BURNT.SDR AU000069Switch · faulty(AUS) CABIN PRESSURE SELECTOR PANEL SWITCH FAULTY.SDR AU000029Spring · broken(AUS) ENTRY DOOR L1 COUNTER BALANCE SPRING BROKEN.
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