Boeing 767-322
Service difficulty reports · 11,768
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 = '767322' 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 = '767322' 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 2002UALA01313Compressor · stalledCOMPRESSOR STALL ON LEFT ENGINE AT TAKEOFF. ENGINE EXPERIENCED A GROUP 3 (TAKEOFF) SURGE. REMOVED ENGINE FOR HIGH COMPRESSOR OVERHAUL.SDR 2002UALA01295Pump · faultyINDICATION OF A LEFT CENTER BOOST PUMP FAILURE WITH POSSIBLE FUEL IMBALANCE. THE LEFT CENTER FUEL TANK OVERRIDE PUMP WAS REPLACED AND OPS CHECKED OK. SYSTEM OPERATION NORMAL THROUGH 8/25/2002. SHOP TEST OF THE REMOVED PUMP WAS PERFORMED WITH NO DEFECTS NOTESDR 2002UALA01289Bracket · loose'L WING SLIDE' EICAS MESSAGE DISPLAYED INTERMITTENTLY WITH EMERGENCY DOOR OVERHEAD LIGHTS FLICKERING. TARGET ASSY BRACKET FOUND LOOSE IN OFF WING SLIDE COMPARTMENT. SECURED BRACKET.SDR 2002UALA01350Pin · burnedPOWER LOST TO FIRST OFFICERS PRIMARY INSTRUMENT BUSS. FLAGS IN VIEW ON FO AIRSPEED INDICATOR, RDMI, VERTICAL SPEED INDICATOR, EHSI AND EADI BLANK. FOUND PIN 4 OF D6430P BURNT, REPLACED PIN. THIS IS 'A' PHASE FROM FIRST OFFICER'S INSTRUMENT BUS VOLTAGE SENSESDR 2002UALA01278Inverter · malfunctionedEICAS STATUS MESSAGE OF STANDBY INVERTER DISPLAYED. UNABLE TO CLEAR MESSAGE. SUPPLEMENTAL DATA UPDATE FOUND INVERTER POWER TRU CB OPEN, REPLACED STATIC INVERTER. OPS CHECK OK.SDR 2002UALA01405Circuit Card · faultyFORWARD CARGO DOOR EICAS MESSAGE AND OVERHEAD CAUTION LIGHT ILLUMINATED INTERMITTENTLY. REPLACED PROXIMITY SENSOR CARDSSDR 2002UALA01222Windshield · crackedELECTRICAL ARC OCCURRED AT THE BOTTOM OF THE LEFT FORWARD WINDOW DURING CRUISE. CREW TURNED OFF WINDOW HEAT. SUBSEQUENTLY WINDOW SHATTERED REMAINING IN ONE PIECE. REPLACED NUMBER 1 LEFT WINDSHIELD ASSEMBLY AS OUTLINED IN MM 56-11-01. ADDITIONALLY DUE TO WISDR 2002UALA01205Compressor · stalledNR 2 ENGINE COMPRESSOR STALL. ENGINE RECOVERED. NR 2 ENGINE HAD A GROUP 3 (TAKEOFF) SURGE. THE ENGINE SELF RECOVERED. ENGINE WAS REPLACED AT TERMINATION OF THE FLIGHT FOR COMPRESSOR REFURBISHMENT.SDR 2002UALA01144Generator · defectiveON CLIMB FROM SFO RIGHT HAND GENERATOR DROPPED OFFLINE AND WAS UNABLE TO BE RESET. SUPPLEMENTAL DATA UPDATE REPLACED RIGHT GENERATOR.DEFECTIVE PARTS - FOUND DIODE, ROTOR AND EXCITER FAILED.SDR 2002UALA01115Scavenge Pump · failedAPU TAILPIPE FIRE. FOUND TURBINE SCAVENGE PUMP FAILED WITH NO ROTATION DURING OPERATION. IN ADDITION, THE TIE SHAFT DRIVE INSERT WAS FOUND LOOSE. THE POWER SECTION WAS ROUTED FOR DISASSEMBLY.SDR 2002UALA01114Engine · flamed outFLAME-OUT OF NUMBER 2 ENGINE. INADEQUATE FUEL SUPPLY PROVIDED TO NR 2 ENGINE. CONDUCTED EXTENSIVE ENGINE AND FUEL SYSTEM DIAGNOSTIC TESTING. DISCOVERED NO INDICATION OF MECHANICAL OR ELECTRONIC SYSTEM FAULTS. CAREFULLY TRACKED AIRPLANE OPERATION AFTER INCISDR 2002UALA01113Pump · leakingLOSS OF HYDRAULIC FLUID FROM RIGHT SYSTEM. REPLACED RIGHT ENGINE HYD PUMP DUE TO LEAK BETWEEN MATING SEAM. ACP ENG RUN, NO LEAKS NOTED.SDR 2002UALA01059Warning System · activatedLEFT ENGINE CONTROL MESSAGE DISPLAYED ON EICAS IN FLIGHT AND ENGINE, REVERTED TO IDLE SPEED.SDR 2002UALA01048Isolation Valve · leakingISOLATION VALVE LEAKED AND LOST LEFT HYDRAULIC SYSTEM. LEFT HYD SYSTEM ISOLATION VALVE LEAKING AT LOWER PORT UNION. REF MM 29-22-05 PG 402 FIG 401. REPLACED DEFORMED O-RING, LEAK CHECKED WITH ALL HYD SYSTEMS RUNNING. NO LEAKS NOTED.SDR 2002UALA01023Floorbeam · corrodedAFT PIT T-CAP CORRODED BODY STATION 1207 AND RBL 40. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP.SDR 2002UALA01022Floorbeam · corrodedAFT PIT T-CAP CORRODED BODY STATION 1285, LBL 40. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP.SDR 2002UALA01021Floorbeam · corrodedAFT PIT T-CAP CORRODED AT BODY STATION 1175, BL 0 TO RBL 40. MAJOR REPAIR ACCOMPLISHED. REPAIRED AND INSTALLED FLOORBEAM T-CAP.SDR 2002UALA01020Floorbeam · corrodedCABIN STATION 825-850, RBL 34, TRANSVERSE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED BEAM.SDR 2002UALA01019Floorbeam · corrodedAFT PIT FLOORBEAM T-CAP CORRODED BODY STATION 1241, RBL 44. MAJOR REPAIR ACCOMPLISHED. REPAIRED AND INSTALLED T-CAP.SDR 2002UALA01000Transmitter · out of rigFLAP ASYMMETRY JUST BEFORE FINAL APPROACH. OUT OF RIG FLAP LEVER TRANSMITTER. SUBJECT TRANSMITTER WAS RIGGED PER APPLICABLE MAINTENANCE MANUAL. FLAP SYSTEM WAS OPS CHECKED PER APPLICABLE MAINTENANCE MANUAL AND ALL OPS CHECKS WERE GOOD. A BITE CHECK WAS ACCSDR 2002UALA00999Switch · malfunctionedNR 2 ENGINE BYPASS OIL LIGHT ILLUMINATED. FOUND OIL FILTER AND CHIP DETECTORS CLEAN. REPLACED OIL FILTER BYPASS SWITCH.SDR 2002UALA00996Floorbeam · gougedCABIN FLOORBEAM UPPER SURFACE GOUGED NEXT TO GALLEY FITTING AT BODY STATION 807, RBL 29. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FLOORBEAM SPLICE DOUBLER.SDR 2002UALA00990Floorbeam · corrodedCABIN FLOORBEAM UPPER SURFACE CORRODED AT BS 800-825, RBL 54. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM.SDR 2002UALA00988Spar · crackedNAC STA 221, NR 2 ENGINE PYLON, UPPER SPAR WEB, IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.SDR 2002UALA00987Floorbeam · corrodedBS 1300 LBL 40-44 T-CAP FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP REPAIRS.SDR 2002UALA00985Spar · crackedNAC STA 221, NR 2 ENGINE PYLON, AFT UPPER SPAR WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.SDR 2002UALA00982Skin · chafedBS 1809.5, LT FUSELAGE AT HORIZONTAL STABILIZER, LOWER SURFACE SKIN CHAFFED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND FILLER.SDR 2002UALA00981Skin · chafedBS 1809.5, RT EXTERIOR FUSELAGE, HAS EXCESSIVE CHAFFING AT LOWER BANANA FAIRING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER AND FILLER.SDR 2002UALA00980Floorbeam · corrodedBS 852, LBL 34, FLOORBEAM CORRODED, MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SECTION AND SPLICES.SDR 2002UALA00979Floorbeam · corrodedBS 830-870, RBL 11, WL 200, UPPER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM REPAIR.SDR 2002UALA00978Floorbeam · crackedBS 786, LBL 12, FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW FLOORBEAM SECTION.SDR 2002UALA00989Floorbeam · crackedBS 287 FLOORBEAM CRACKED, LEFT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.SDR 2002UALA00972Floorbeam · crackedBS 287 FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.SDR 2002UALA00971Skin · damagedBS 400-420, STRINGER 36R-30R SKIN DOUBLER HAS BLIND FASTENERS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER.SDR 2002UALA00970Floorbeam · corrodedBS 790, LBL 11, WL 200 TOP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS AND SPLICES.SDR 2002UALA00962Charger · intermittentESCAPE PATH LIGHTING IN BACK OF AIRCRAFT COME ON AND OFF DURING FLIGHT. EEL LIGHT COMES ON AND OFF FROM ROWS 29FG AFT TO ROW 35FG. REPLACED BATTERY CHARGER-POWER SUPPLY AND BATTERY AT SEAT 33FG SIDEWALL.SDR 2002UALA00953Cdu · failedRIGHT MULTIFUNCTION CONTROL DISPLAY UNIT FAILED. RIGHT FMC HMCDU FAIL. REPLACED THE RIGHT HMCDU.SDR 2002UALA00890Computer · malfunctionedR EICAS CMPTR EICAS MSG DISPLAYED. REPLACED EICAS COMPUTER AND LOADED CORRECT OPS AND OPC SOFTWARE. OPS OK. THERE WAS NO FAULT FOUND IN THE REMOVED EICAS COMPUTER.SDR 2002UALA00894Valve · failedEQUIPMENT FAILURE ASSOCIATED WITH EQUIPMENT COOLING PROBLEM. INTERMITTENT HSI/ADI/TCAS/WX RADAR OCCURRED RIGHT AFTER TAKEOFF. SYSTEMS SOMEWHAT RESTORED ONCE FAN SELECTED TO OVERRIDE. REF INBD LOG1 FOR LOSS OF VARIOUS CRT'S W SOME A-P PROBLEMS. AS PER LCL DSDR 2002UALA00885Warning System · malfunctionedAFTER TAKEOFF, CREW RECEIVED A FWD CARGO DOOR AND EQUIPMENT COOLING MESSAGE. FWD EQPT COOLING EICAS MSG DISPLAYED. PERFORMED OPERATION CHECK PER MM-21-58-00. NO FURTHER MSG DISPLAYED. NO FURTHER WRITE-UPS HAVE OCCURRED FOR EQUIPMENT COOLING SYSTEM. NO PARSDR 2002UALA00878Wire Harness · faultySECTION OF FLOOR EMERGENCY EXIT LIGHT BEGINNING AT RIGHT SIDE CLOSET AT MID GALLEY AND ENDING AT AFT EDGE OF MID LAV FORWARD OF ROW 15 IS INOPERATIVE. REPAIRED CABLE EMERGENCY ESCAPE PATH LIGHTING.SDR 2002UALA00843Stringer · puncturedSTATION 358 STRINGER 3 RT IS PUNCTURED, LIGHTNING STRIKE DAMAGE. MAJOR REPAIR ACCOMPLISHED. STRINGER REPAIRED.SDR 2002UALA00841Floorbeam · corrodedBODY STATION 852 LBL 55 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP.SDR 2002UALA00840Floorbeam · corrodedBODY STATION 1219 LBL 30 T-CAP CORRODED UNDER NUT PLATES. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP.SDR 2002UALA00839Stringer · corrodedBODY STATION 348 STRINGER 20R RBL 84 TOP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SECTION AND SPLICES.SDR 2002UALA00838Skin · chafedBODY STATION 1809.5 LT EXT FUSE SKIN HAS EXCESSIVE CHAFFING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR 2002UALA00820Skin · chafedBODY STATION 1809.5 RT EXTERNAL FUSELAGE SKIN HAS EXCESSIVE CHAFING WEAR. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLEDREPAIR DOUBLER.SDR 2002UALA00776Projector · failedFIRST CLASS PROJECTOR FAILED EMITTING SMOKE AND FUMES INTO PASSENGER COMPARTMENT. REPLACED FIRST CLASS PROJECTOR, SYSTEM TEST OK.SDR 2002UALA00787Stringer · crackedA/C FUSELAGE IS DENTED AT STATION 400 AND STRINGER 36L. STRINGER IS DEFLECTED .50 INCHES OVER 20 INCH LENGTH. ALSO, FWD CARGO PIT STRINGER 34L HAS 2 INCH CRACK AT STA 390. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW STRINGERS, THE DENT WITH STRING DOUBLER.SDR 2002UALA00760Stringer · crackedFORWARD CARGO PIT STRINGER 34L HAS A 2 INCH CRACK AT STATION 390. MAJOR REPAIR ACCOMPLISHED. INSTALLED U-CHANNEL.
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