Boeing 767-375
Service difficulty reports · 1,386
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 = '767375' 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 = '767375' 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 CA101222003Adc · failed(CAN) AFTER T/O, CAPT LOST AIRSPEED AND ALTITUDE INSTRUMENTS. RECOVERED INSTRUMENTS BY CHANGING TO ALTERNATE AIR DATA SYSTEM. CAPT FELT FLIGHT DIRECTOR SYSTEM WAS UNRELIABLE AND ELECTED TO FLY AIRCRAFT MANUALLY. CAPT AIR DATA INFO RETURNED WHEN ALTN AIR DSDR CA101108008Printer · odor(CAN) ON GROUND, MAINTENANCE NOTICED A VERY STRONG BURNING SMELL IN FLT DECK. ACARS PRINTER FOUND TO BE AT FAULT. PRINTER REPLACED.SDR CA101105002Fuel Line · cut(CAN) AIRCRAFT HAD REPEAT REPORTS OF LT WING FUEL IMBALANCES. MULTIPLE TANK ENTRIES DURING TROUBLESHOOTING LEAD TO ROOT CAUSE FINDING OF THE FUEL PRESSURE LINE COMING FROM THE LT CENER TANK OVERRIDE PUMP WAS FOUND SHAFFED (CUT). PLEASE REFER TO ATTACHMENT. NSDR CA101101001Insulation · cracked(CAN) FROM AN INSPECTION ON AIRCRAFT 685 AND PHOTO’S OF THE ISSUE IN QUESTION IN ATTACHMENT. THERE ARE SEVEN WIRE BUNDLES THAT ALL HAVE ONE BLUE WIRE IN EACH. IN EACH BUNDLE THE BLUE WIRE ONLY, HAS CRACKED SHIELDING DOWN TO THE CORE FOR A TOTAL OF 15 CRACKS.SDR CA101027012Module · failed(CAN) ON DEPARTURE, CREW RECEIVED 2 MOMENTARY EICAS STAB TRIM FAULTS, THEY ALSO REPORTED NO STAB MOVEMENT. FOUND R STCM FIM BALL YELLOW IN VIEW AT R SAM RESET OK, MCDP NO LAST FAULT. MCDP 65 GRD TEST COMPLETED MAN & A/P STAB OPERATION CHECKED OK. REF FIM 2SDR CA101111003Seat Back · cracked(CAN) CONTOUR J-CLASS SEATBACK PNS231010-001-001 FAILED AND REQUIRED REPLACEMENT. SEATBACK HAD ALREADY BEEN MODIFIED BY CONTOUR SB25-3379 INSTALLATION OF DOUBLERS TO SEATBACK SUPPORT ARMS. AIR CANADA SAFETY REPORT NR 12892 RAISED.SDR CA101004006Hose · leakingTHE ACFT DEVELOPED LOW CTR HYD PRESSURE AFTER TAKEOFF. WITH NO INDICATIONS OF IMPROVEMENT, THE FLIGHT DIVERTED. AS A PRECAUTION, CFR WAS CALLED OUT TO MEET THE FLIGHT, HOWEVER THE ACFT WAS ABLE TO TAXI INTO THE GATE WITHOUT ASSISTANCE. THERE WAS NO ADVERSE PSDR CA100922008Motor · seizedBOTH WEATHER RADAR SYS FAILED AFTER TAKEOFF, ENROUTE. FLIGHT DIVERTED AND DURING TROUBLESHOOTING IT WAS IDENTIFIED THAT THE WEATHER ANTENNA SWEEP MOTOR, COMMON TO BOTH SYS, WAS SEIZED. THE ANTENNA WAS REPLACED AND BOTH SYSTEMS WERE GROUND FUNCTIONED SERVICEASDR CA100719004Brake Assy · fireON THE TAXI INBD TO THE GATE, THE CREW REPORTED THAT THEY HAD HOT BRAKES. WHEN THE ACFT ARRIVED ON THE GATE, AN ATTENDANT NOTICED SMOKE COMING FROM THE RT MAIN OTBD GEAR FOLLOWED BY A SMALL FLAME. ATTENDANT EXTINGUISHED THE FLAME USING THE PCA (AIR CONDITIONSDR CA100701003Engine · failedRIGHT ENGINE SURGE AFTER T/O. ENGINE NOISE, VIBRATION AND N1 INDICATION WAS ALSO SURGING. EGT WAS CONTROLLABLE WITH THRUST LOWER N1. REDUCED ENGINE POWER TO 75 PERCENT N1 AND RETURNED TO THE DEPARTURE AIRPORT. THE ENGINE APPEARS TO HAVE HAD A FAILURE AND LSDR CA100604003Nut · wrong part(CAN) AN ANOMALY DETECTED DURING A RECENT ENGINE CHANGE WHEN DIFFICULTY WAS ENCOUNTERED IN APPLYING TORQUE TO 4 EACH FORWARD MOUNT BOLTS. NUTS, WHICH ARE CAPTIVE TO MOUNT AS RECEIVED WITH ENGINE, WERE SUBSEQUENTLY REJECTED AND NEW NUTS INSTALLED. ENGINE CHANGSDR CA100126002Duct · damaged(CAN) UPON ARRIVAL, MX DISCOVERED THAT THE L/E SLAT NR 4 (LT WING) OVERPRESSURE PANEL WAS OPEN. FURTHER INSP REVEALED THAT THE THERMAL ANTI-ICE INSTERSTITIAL DUCT WAS DAMAGED AND HAD IN FACT SEPARATED AT THE JOINT WITH THE ADJOINING SLAT ANTI-ICE DUCT WHILE ISDR CA090818003Lug · damaged90 MINUTES AFTER TAKEOFF, AT 34,000 FT, RED CABIN ALTITUDE WARNING AND BELL SOUNDED. CABIN ALT SHOWED 10,000 FT WITH CABIN ALTITUDE CLIMBING AT 800-1000 FT/MIN. PRESS CHECK LIST ACCOMPLISHED, MASKS DEPLOYED AND CREW DECLARED A PAN PAN. FLIGHT DESCENDED TO 8,0SDR CA090702001Duct · ruptured(CAN) AFTER TAKEOFF, F/A REPORTED EXCESSIVE HEAT IN AFT CABIN THAT COULD NOT BE CONTROLLED. ACFT RETURNED TO DEPARTURE WHERE MX FOUND THAT AFT CARGO HEAT DUCT RUPTURED BETWEEN THE SUPPLY AND THE SHUT-OFF VALVE. DUCT HAD A 4 INCH LONGITUDINAL CRACK. DUCT IS LSDR CA060918002Circuit Card · malfunctioned(CAN) CAPTAIN REJECTED TAKEOFF ROLL AT 155KTS BECAUSE OF A (TAKEOFF CONFIGURATION SAFETY WARNING) MESSAGE, 4 MAIN LANDING GEAR TIRES REPLACED DUE TO HIGH ENERGY BRAKING AND FUSE PLUGS MELTING. NEW LANDING CONFIGURATION CARD INSTALLED AND TESTED. (TC NR 2006091SDR CA060526003Duct · ruptured(CAN) L GEN CONT MSG ILLUMINATED, IN FLIGHT CHECKLIST C/O, L GENERATOR CONTROL REMAINED OFF. ON CLIMB OUT, L OIL PRESS EICAS FLASHED RED NUMBERS DECREASING WENT BLANK - OIL TEMP INCREASING -QRH FOLLOWED ENGINE SHUT DOWN. FOUND CB FOR LEFT ENGINE OIL PRESSURE SDR CA060307001Control Panel · malfunctionedON CLIMB-OUT YVR, NO A/T, NO CMD BARS, NO A/P L AND C. NO L NAV, (ACFT RETURNED TO YVR). REPLACED MCP PER AMM 22-11-02 PB 201.SDR CA051221006Cooling Fan · seizedCREW REPORTED SLIGHT SMOKE AND PLASTIC BURNING ODOR IN COCKPIT. ACFT DIVERTED TO SNN. MX CARRIED OUT INSPECTION, FOUND EQUIP COOL EXHAUST FAN FAILED AND TRIPPED THE CB, AREA INSP. NO FURTHER DAMAGE FOUND, FAN PLACED ON MEL ACFT DISPATCHED.SDR CA051031002Striker · burned(CAN) FAULT: STRONG RUBBER BURNING SMELL FIRST NOTICED IN FWD GALLEY THEN IN COCKPIT. AUTH NR175945 FOUND FLT DECK DOOR ELEC LOCK ACT BURNNED. LOCK ACT ELECT CONNECTORS REMOVED AND STOWED, C/B PULLED AND COLLARED. (RUNOUT DATE10/31/2005).SDR CA050909003Wire Harness · failed(CAN) FAULT: FLT DEP.YYZ WITH LT FUEL DENSIOMETER UNDER MEL. FLT CREW CONFIRMS LT IND DID BLANK OUT ON OCCASION DURING THE FLT AND HAD BEEN CALCULATING THE FUEL REMAINING THROUGHOUT THE FLT. AT FL370 AND 50NM FROM TOP OF DESCENT, THE LT ENG FLAMED OUT, ENG RSDR CA050517002Light · smoke(CAN) ON FINAL TO 24R, IN CHARGE F/A REPORTED SMOKE FROM UTILITY LIGHT FWD GALLEY AFTER COMPLETING QRH AND CUTTING UTILITY BUSSES SMOKE SUBSIDED. TRANSFORMER REPLACED AND OPS TESTED OK.SDR CA050510002Wire · burned(CAN) FAULT: REF L1523271 AFT CHILLER POPS CB, FOUND UPPER CHILLER WIRING BURNED AND ARCED TO BOTTOM OF FLOORBEAM . FLOORBEAM AT STN 1540 , 26 INCHES RT OF CENTER LINE. HAS HOLE BURNED THROUGH LOWER CHORD APROX .8750 INCHES WIDE , .5 INCH ACROSS LOWER CHORD,SDR CA050510008Throttle Cable · misaligned(CAN) ON CLIMB OUT THRU FL 130 EICAS (L PRV) QRH COMPLETED - THRU FL 200 LT THROTTLE VERY HARD TO ADVANCE OR MOVE TO IDLE. A/T ARM OFF NO IMPROVEMENT. RETURN TO LHR. NO LT REVERSE ON LANDING. FOR T/S AND INFO ON PRV REFER TO L1425969. LT ENG PUSH PULL CABLE RSDR CA050111003Oven · fire(CAN) FAULT: JUST PRIOR TO DESCENT, SOMETHING WAS BEING COOKED IN THE MID CABIN GALLEY. AS THE F/A WAS ABOUT TO REMOVE IT, A FIRE WAS FOUND AT THE BACK OF THE OVEN. 3 FIRE EXT. WERE USED TO DOUSE THE FIRE. NO EMERGENCY WAS DECLARED, NO ADVERSE PAX REACTION.SDR CA041230002Bleed Air Sys · leaking(CAN) R' BLEED DUCT LEAK''EICAS MSG',QRH COMPLETED. LIGHT DUCT LEAK STAYED ON FOR 90 MINUTES, WENT OUT FOR 30 MINUTES, THEN CAME ON AGAIN. NOTICED THAT RT BLEED PRESSURE STAYED AT 5 PSI, NOT ZERO. VISUAL INSPECTION OF PNEUMATIC DUCTS, CLAMPS AND OVERHEAT DETSDR CA041126010Axle · broken(CAN) ACFT 684 ON LANDING, DISCOVERED RT ML GEAR AFT AXLE BROKEN, IT SEEMS THAT HAPPEN DURING TAKEOFF IN XXX, BECAUSE FLIGHT CREW REPORT ANTI- SKID LIGHT WAS ON DURING WHOLE FLIGHT. MORE INFO AND PICTURES WILL FOLLOW AS IT BECOME AVAILABLE.SDR CA041123003Wire · burnedFOUND WIRE BUNDLE INSIDE TOILET SHROUD BURNING AND SMOKING, C/B SYST 2 WATERLINE HEATER (LAV LIGHTS) POPPED IN AVIONICS BAY. FURTHER T/S ON WIRING BURNED, FOUND WIRES IDENTIFIED AS H75C20,H75A20, AND H75A20N (GRN) ALL BROKEN FROM SPLICES. ALSO, HEATER TAPE RSDR CA040813003Windshield · cracked(CAN) WHILE IN CRUISE CAPT'S WINDSHIELD CRACKED.SDR CA040812010Transmitter · leaking(CAN) NR 1 ENGINE FUEL PRESSURE TRANSMITTER FOUND LEAKING TOTAL TIME ON PART 20349.7HRS TOTAL TIME SINCE INSTALL 3445.2 HRSSDR CA040513003Computer · failed(CAN) AFTER T/O EICAS MSGS (RUDDER RATIO,AILERON LOCKOUT) ALTIMETER, AIRSPEED, IVSI OUTSIDE LIMITS BETWEEN CAPT AND F/O, AUTO PILOTS WOULD NOT ENGAGE. NOTE: MOC REQUESTED F/O ALT ADC BE SELECTED, FAULT CLEARED. FLT CREW ELECTED TO RTN TO YVR. RT ADC FAULT BUSDR CA040225012Actuator · stuck(CAN) EICAS MESAGE AILERON LOCKOUT, FOUND RT AILERON LOCK OUT ACTUATOR STUCK IN THE EXTEND POSITION, ACTUATOR REPLACED.SDR CA040122005Wire · chafed(CAN) FAULT: LT ENGINE HYD. ALT. CURRENT MOTOR DRIVEN PUMP (ACMP)POWER FEEDER WIRES FOUND CHAFFING AND ARCHING ON STRUT STRUCTURE. STRUC. DAMAGE WAS ALSO NOTED DUE TO ARCHING.SDR CA030919003Control Panel · malfunctioned(CAN) A/C HAD A DUAL ATC FAILURE AFTER DEPARTURE LHR. UK ATC WOULD NOT LET THE A/C PROCEED SO RETURNED TO LHR. OVERWEIGHT LANDING CHECK CARRIED OUT. ATC CONTROL PANEL CHANGED AND NO FURTHER FAULTSDR CA030226001Compressor · stalled(CAN) REJECTED TAKE OFF AFTER COMPRESSOR STALL ON THE LT ENGINE AND RISE IN TEMP AT 155 KNOTS, ALL 8 TIRES WENT FLAT (FUSES BLOWED OUT).SDR CA020916009Coffeemaker · failed(CAN) ON DECENT CREW REPORTED SMOKE IN AFT GALLEY AND LOUD POPPING SOUND, GALLEY COVERED IN WHITE DUST. NOTIFIED ATC/MAINT/DISPATCH. MTCE SUSPECTED COFFEEMAKER HOT WATER BLEW PLUG, AIRCRAFT LEFT WITH UTILITY BUSES OFF/REAR GALLEY CB'S PULLED. AREA INSPECTEDSDR CA020830011Light · miswired(CAN) SECOND OBSERVERS UTILITY LIGHT FOUND MISWIRED AT TERMINAL BLOCK. THIS FINDING WAS RESULT OF A CAMPAIGN TO CHECK FOR SIMILAR PROBLEM ON 767 FLEET. LIGHT SOCKET PRODUCES SPARKS IF INADVERTENTLY TOUCHED BY A GROUNDING OBJECT. TERMINAL BLOCK REWIRED CORRSDR CA020801003Actuator · failed(CAN) RT AILERON LOCKED OUT DURING FLIGHT AFTER LEAVING YVR. RT LOCK OUT ACTUATOR REPLACED PER AMM 27-11-44 PG 1-12 OPERATION CHECKED SERVICEABLESDR CA020530012Stator · destroyed(CAN) AFTER LANDING BRAKE TEMP LIGHT ON RIGHT FOREWARD INNER MAIN. TEMP WENT TO 9 WITH AUTOBRAKE SETTING AT 2 FOR LANDING. NR 3 MAIN WHEEL AND BRAKE REMOVED. BRAKE INNER STATOR DISINTEGRATED AND CAUSED JAMMING OF BRAKE. TIRE DEFLATED DUE FUSE PLUG OVERHEAT. SDR CA020509003Valve · leaking(CAN) DURING A M01 CHECK THE LEFT AND RIGHT HYDRAULIC SYSTEM EMPENNAGE FLIGHT CONTROL SHUTOFF VALVES WERE FOUND LEAKING.AFTER INVEASTIGATION , ONE OF THE L/H BOLT WAS SHEARED WHILE OTHERS WERE ENGAGED ONLY WITH A COUPLE OF THREADS. SIMILAR FINDINGS WERE FOUND SDR CA020502011Actuator · leaking(CAN) CENTRE SYSTEM HYDRAULIC QUANTITY MESSAGE ON EICAS ON TOP OF DESCENT. QUANTITY CONTINUED TO DROP SLOWLY DURING DESCENT AND FLAP/GEAR EXTENSION FOUND TO BE A LEAK FROM THE INBOARD RT ELEVATOR POWER CONTROL ACTUATOR (PCA). REPLACED ACTUATOR.SDR CA020104011Duct · damaged(CAN) LT ENGINE FIRE INDICATION AT 11,000 FEET IN CLIMB. ENGINE SHUT DOWN. FIRE BOTTLES DISCHARGED. AIRCRAFT RETURNED TO SYDNEY. FOUND ENGINE PNEUMATIC DUCTING RUPTURED AND ALSO HARNESS DAMAGED. HARNESS TEMPORARY REPAIRED AS PER PRODUCTION PERMIT 6-77-20/SDR CA011121017Control Handle · failed(CAN) ON APPROACH TO ST-JOHN, NF, WHEN SELECTED FLAP TO 5 DEGREES, FLAP DISAGREE EICAS MSG. CHECKLIST COMPLETED. EMERGENCY CALLED OUT. FLAP LEVER RVDT AND OUTBOARD SLAT PDU RVDT RE-ADJUSTED. FSEU RESETED AND FLAPS OPERATED SEVERAL TIMES. SYSTEM SERVICEABLE.SDR CA010924003Rib · cracked(CAN) LT AND RT WING RIB WEB, INBOARD OF SLAT ANTI-ICE TELESCOPING DUCT CRACKED/BROKEN AT TOP SURFACE. 4 - 6 INCH CRACK FOUND IN RADIUS OF L/H AND RT NOSE FORMER ON WING FIXED LEADING EDGE COMMON TO NR 5 AND 8 LEADING EDGE SLAT.SDR CA010906008Controller · failed(CAN) SMELL AND SMOKE COMING OUT NR 2 GALLEY OVEN. OVEN CONTROLLER REPLACED. OPERATION CHECKED FOR ONE HOUR. NO SIGN OF VERHEATING, CONSIDER SERVICEABLE.SDR CA010622010Generator · failed(CAN) F/O'S FMC FAILED, F/O'S ADI & HSI FLICKERED CONTINIOUSLY. AUTO THROTTLE DROPPED OFF. SINGLE FMC MESSAGE & RESYNCHING OTHER FMC MESSAGE ALL COME ON. WHEN THE RIGHT GENERATOR BREAKER WAS OPENED & THE APU GENERATOR WAS PUT ON LINE, ALL SYSTEMS OPERATE NORMASDR CA010626038Acm · seized(CAN) DURING TAKEOFF, THE COCKPIT/CABIN FILLED WITH SMOKE. AIR CONDITIONING SUSPECTED. AIRCRAFT RETURNED. DEFFERRED AS PER MEL 21-51-07. RIGHT HAND ACM FOUND SEIZED.SDR CA010522009Fitting · cracked(CAN) DURING INSPECTION NR 2 PYLON INBOARD MIDSPAR FITTING WAS FOUND CRACKED AT UPPER AFT INBOARD FASTENER HOLE. NR 2 PYLON MIDSPAR FITTING REPLACED AS PER EVA 01-767-54-4058.SDR CA010301015Fseu · failed(CAN) ON TAKEOFF, WITH FLAPS SELECTED 5, FLAPS WOULD NOT MOVE. MOMENTARY TRAILING EDGE FLAP DISAGREE LIGHT. STATUS MESSAGE TE FLAP SHUTDOWN. WHEN AUTOPILOT DISENGAGED AIRCRAFT ROLLED TO THE RIGHT. AIRCRAFT RETURNED TO YYZ. MAINTENANCE ON ARRIVAL FOUND FLAPS/SLSDR CA010404011Fitting · cracked(CAN) DURING INSPECTION OF NR 2 RT PYLON, THE MIDSPAN FITTING FOUND CRACKED BETWEEN FASTENERS. NR 2 ENGINE REMOVED AS PER WORK CRD 71125-2. NR 2 PYLON REMOVED AS PER WORK CARD 54102-2 FROM AIRCRAFT FOR REPAIR. NR 2 MIDSPAN FITTING RELACED AS PER ENGINEERING VASDR CA010301018Warning Light · malfunctioned(CAN) ON LANDING, WHEN GEAR SELECTED DOWN, MAIN GEAR YELLOW WARNING LIGHT EMAINED ON. GEAR WAS RE-CYCLED ON FINAL APPROACH, WITHOUT SUCCESS. A GO-AROUND WAS INITIATED AND GEAR WAS RE-CYCLES 2 MORE TIMES WITHOUT SUCCESS. A FLY-BY THE TOWER WAS ACCOMPLISHED AND
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