Boeing 767-3S1
Service difficulty reports · 974
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 = '7673S1' 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 = '7673S1' 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 UIEA2012022900069Start Valve · failedLEFT ENGINE START VALVE WOULD NOT OPEN DURING START. R & R LEFT ENGINE START VALVE IAW AMM 80-11-02. OPS CHECKED GOOD.SDR UIEA2012022900072Electronic Unit · failedAIRTURN BACK, T/E FLAP DISAGREE, & L/E SLAT DISAGREE, PERFORMED FIM 27-51-00, FIG 114A. VISUAL INSPECTED FLAPS & AMP; SLATS. FIM 27-51-00, FIG 104, AMM 27-51-26/401 CHECKED RVDT'S M603/M604 FOUND OUT TOLERANCE. ADJUSTED SET IAW AMM 27-51-26. OPS CHECKED GOODSDR UIEA2012022700067Fseu · failedT/E FLAP DISAGREE, PERFORMED FIM 27-51-00 FIG 114A. VISUAL INSPECTED FLAPS AND SLATS. FIM 27-51-00 FIG 104, AMM 27-51-26/401 CHECKED RVDT'S M603/M604 FOUND M603 OUT OF TOLERANCE. ADJUSTED SET IAW BOEING AMM 27-51-26. OPS CHECKED GOOD. R & R FSEU IAW AMM 27-5SDR UIEA2012022700068Fseu · failedL/E SLAT DISAGREE. PERFORMED FIM 27-51-00 FIG 114A, VISUAL INSPECTED FLAPS AND SLATS FIM 27-51-00, FIG 104, AMM 27-51-26/401 CHECKED RVDT'S M603/M604 FOUND M603 OUT OF TOLERANCE. ADJUSTED SET IAW AMM 27-51-26. OPS CHECKED GOOD. R & R FSEU IAW AMM 27-51-01.SDR UIEA2012022700063Warning Message · illuminatedLEFT IGNITER 1 STATUS MESSAGE. PREFORMED FIM 74-00-00, FIG 108 HAD CODE ON PIMU 351-25B LT ADC CHANNEL FAIL.SDR UIEA2012022700064Warning Light · illuminatedLEFT ENGINE EEC MODE ON ROLLOUT.SDR UIEA2012022500061Engine · making metalAPU FAILED AT GATE. AUTO SHUTDOWN, ECU BITE SHOWS "APU SHUTDOWN FOR LOW OIL PRESSURE". APU CHIP DETECTOR SHOWS EXCESSIVE METAL.SDR UIEA2012021900054Warning Message · false activationRIGHT PACK MX MESSAGE TEMPERTURE CONTROL VALVE ON BITE CHECK. PERFORMED FIM FIM 21-51-00, FIG 103, TABLE B TEMPERTURE CONTROL VALVE, STEP 1E CONTROL VALVE OK.SDR UIEA2012021100043Warning Message · false activationSTATUS " CAB ALT AUTO 1", PERFORMED FIM 21-31-00 FIG 103, NO FAULTS FOUND. OK FOR CONTINUED SERVICE, GROUND CHECKS GOOD IAW AMM 21-31-00)SDR UIEA2012013000031Warning Message · illuminatedEICAS MESSAGE, LT PACK TEMP STANDBY SELECTED IAW QRH. MESSAGE CLEARED.SDR UIEA2012012800030Stator Vane · damagedLT ENGINE APROX 7 O'CLOCK POSITION STATOR VANE MISSING PIECE OF METAL FWD EDGE NO EROSION NOTED. ENGINE PN ;CF6-80C2B6F, SN 702522 (APPLIED SPEED TAPE IAW AMM 72-33-00)SDR UIEA2012012700029Panel · damagedDURING WALKAROUND, FOUND RT WING L/E PANEL LOWER SIDE WITH DAMAGE, PANEL FAA 611CB. REMOVED DAMAGED PANEL IAW SRM; INSTALLED SERVICEABLE PANEL IAW SRM 51-40-02.SDR UIEA2012012300023Actuator · failedEICAS MESSAGE "LEFT PACK TEMP". TROUBLESHOT IAW FIM 21-51-00. FAULTED LT RAM AIR DOOR ACTUATOR, R & R LT ACTUATOR IAW AMM 21-53-01. OPS CHECKED NORMAL. EICAS MESSAGE AND FAULT CLEARED. ACFT RELEASED TO ETOPS SERVICE IAW ETOPS MM FOR VERIFICATION FLIGHT DUESDR UIEA2012012100021Guide Vane · damagedLT ENGINE HAS 2 INLET GUIDE VANES DELAMINATED. NO DELAMINATION, FOUND MISSING METAL JACKET ON L/E & NBSP; APPLIED SPEED TAPE IAW AMM 72-33-00 PAGE 816 "F".SDR UIEA2012011500010Fire Detector · malfunctionedRT AFT LAV FIRE DETECTOR IS ACTIVATED. RESET FIRE DETECTOR; INSPECTED LAV TRASH RECEPTACLE, HEAT INDICATORS; INDICATORS ALL 4 WERE WHITE, NO SIGNS OF SMOKE OR FIRE.SDR UIEA201112272011Windshield · brokenCAPTAINS WINDSHIELD OUTER PANE BROKEN. R & R NR 1 WINDSHIELD IAW MM 56-11-01 AND R & R WINDOW HEAT CONTROL UNIT M191 IAW MM 30-41-01. PERFORMED TEST OF WINDOW HEATING SYSTEM AND OPS CHECKED WINDSHIELD WIPER IAW MM 30-41-00 AND 30-42-00. OPS CHECKED NORMAL.SDR CA030205004Windshield · cracked(CAN) ON CLIMB OUT OF YVR, RT WINSHIELD SHATTERED. ACFT CONTINUED TO YUL.SDR CA020801008Bolt · sheared(CAN) AT TRIP CHECK DAMAGE FOUND TO LT WING TO FLAP FAIRING, MLG SHOCK STRUT DOOR, AND JURY STRUT DOOR. INVESTIGATION FOUND SHOCK STRUT DOOR MID ATTACH BOLD HAD SHEARED ALLOWING SEPERATION OF DOOR FROM STRUT. NEW FAIRING PANEL FABRICATED, JURY STRUT DOOR TSDR CA020328004Outflow Valve · failed(CAN) AFTER TAKEOFF, EICAS MESSAGE "CABIN ALT AUTO 1 APPEARED. AIRCRAFT DIVERTED TO LONDON (HEATHROW) LHR FOR FIX. OUTFLOW VALVE AND ACTUATOR REPLACED AS PER AMM 21-31-02. SYSTEM CHECKED SERVICEABLE.OUTFLOW VALVE -606832-21 ACTUATOR -2022480-6SDR CA020110001Engine · failed(CAN) ON TAKEOFF ROLL, AFTER N1 SELECTED ON MCP, ENGINE ACCELERATE NORMALLY TO 50 PERCENT AT 50 PERCENT ENGINE DID NOT ACCELERATE ANY FURTHER. ALL PARAMATERS NORMAL FOR BOTH ENGINES. AN AIRFRAME VIBRATION COULD BE FELT AT 25 - 50 PERCENT ON LT ENGINE. TASDR CA011114004Motor · failed(CAN) AFTER TAKEOFF AT 14,000 FT. LOSS OF BOTH AUTO CABIN PRESSURE CONTROL SYSTEMS. AIRCRAFT RETURNED TO ZURICH. AC MOTOR 2 REPLACED AS PER AMM 21-31-03 AND CHECKED SERVICEABLE.SDR CA010301017Engine · failed(CAN) ON FINAL INTO YYZ, RIGHT ENGINE SHUTDOWN, 4 MINUTES TO LANDING. ENGINE SHUTDOWN CHECKLIST COMPLETED. LANDED WITHOUT INCIDENT. ON INSPECTION OF RT ENGINE METAL FOUND IN TAILPIPE. RT ENGINE REPLACED. OFF PART NUMBER 6-7200-9-0002, SERIAL NUMBER 2611.2001-0SDR CA000925009Indicator · failed(CAN) FIRST OFFICERS AIRSPEED FAILED AT 60 KNOTS ON TAKEOFF ROLL. REJECTED TAKEOFF AT 100 KNOTS. FIRST OFFICERS AIRSPEED INDICATOR REPLACED . WHEELS AND TIRES INSPECTED AS PER FLYAWAY MANUAL 2.02-05.02, DUE RTO, NO DAMAGE FOUND, BRAKE TEMP INDICATIONS NORMAL.SDR 96ZZZX2827Brake Assy · defectiveTHE BRAKE, PN 2608812-7, SN B4383, CAME FROM AVIALL ON FEBRUARY 5TH, AND INSTALLED THE NEXT DAY ON N769TA. DURING OPERTION OF FEBRUARY 6TH HERE AT THIS STATION, RECEIVED A FAX MESSAGE FORWARDED FROM AVIALL INFORMING THIS BRAKE HAS A FAILURE. FAILURE CONSISTE
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