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 98UAL900196Power Supply · inoperativeEMERGENCY EXIT FLOOR LIGHTS FLICKER ON AND OFF ON RIGHT SIDE BETWEEN ROWS 15 TO 20. *S/D* REPLACED EMERGENCY LIGHTS POWER SUPPLY, M1559.SDR 98UAL900179Retract Mech · malfunctionedINITIAL LANDING GEAR EXTENSION RENDERED AMBER TAIL SKID AND GEAR LIGHTS AND EICAS GEAR DISAGREE MESSAGE. DID GO-AROUND, RECYCLED GEAR. SUBSEQUENT GEAR EXTENSION NORMAL.SDR 98UAL900154Indication · malfunctionedAFTER LANDING GEAR EXTENSION, EICAS GEAR DISAGREE AND TAIL SKID WARNINGS. GEAR AND TAIL SKID WARNING LIGHTS ILLUMINATED ON LANDING GEAR INDICATION PANEL BUT HAD ALL GEAR DOWN LIGHTS GREEN. RECYCLED LANDING GEAR AND GOT ALL NORMAL INDICATIONS WITH NO ABNORMALSDR 98UAL900144Sensor · out of adjustTAKEOFF ABORTED AT 110 KNOTS. *S/D* E AND E COMPARTMENT DOOR WARNING ILLUMINATED. REPLACED AND ADJUSTED E AND E DOOR CLOSED SENSOR S201 PER MM, GROUND OPS CHECKS OK.SDR 99UAL900193Sensor · malfunctionedRIGHT WING SLIDE EICAS MSG DISPLAYED. ALSO, EMERGENCY DOOR LIGHT ILLUMINATED. DIVERTED TO BOS. *S/D* ACCOMPLISHED BITE CHECK OF PSEU AND FOUND SENSOR S199 FAULTED. REPLACED S199 PER MM5 AND ADJUSTED SENSOR PER MM, OPS CHECKS NORMAL.SDR 98UAL900135Connector · looseEEL FLOOR PATH LIGHTS ARE INOP ON RIGHT HAND SIDE FROM DOOR 1 RIGHT TO SEAT 6E. PROBLEM ORIGINATES AT CONNECTOR AT SEAT 1E. REPLACED EEL FEEDER STRIP FROM WALL AT 1 E AND F.SDR 98UAL900102Actuator · failedLEFT MAIN LANDING GEAR REMAINED DOWN AFTER TAKEOFF. RETURNED TO FIELD. *S/D* MLG DRAG BRACE LOCK ACTUATOR FAILED. INTERNAL PISTON RETENTION NUT WAS NOT INSTALLED CORRECTLY. REPLACED ACTUATOR.SDR 98UAL900101Idg · disconnectedRIGHT GENERATOR EICAS MESSAGE DISPLAYED. GENERATOR DRIVE LIGHT ILLUMINATED. GENERATOR DRIVE DISCONNECTED. *S/D* MECHANICS PERFORMED BPCU BIT TEST, INLET TEMP SENSOR-WIRING RIGHT IDG MESSAGE WAS DISPLAYED. DURING IDG INSPECTION FOUND T2 POWER CABLE TERMINSDR 99UAL900121Compressor · stalledNR 2 COMPRESSOR STALL SHORTLY AFTER TAKEOFF. FLAMES REPORTED, FIRE BOTTLES DISCHARGED, ENGINE SHUTDOWN. EMERGENCY DECLARED. RETURNED TO FIELD, OVERWEIGHT LANDING WITHOUT INCIDENT. *S/D* THIS ENGINE EXPERIENCED A GROUP 3 SURGE EVENT. GROUP 3 SURGES ARE THSDR 98UAL900014Control Valve · failedTRAILING EDGE LIGHT ON DURING APPROACH AT POSITION 20. EXECUTED MISSED APPROACH. NEXT APPROACH FLAPS WORKED NORMALLY. *S/D* AN INTERMITTENT INTERNAL FAILURE IN THE TRAILING EDGE FLAP POWER DRIVE UNIT HYDRAULIC CONTROL VALVE MODULE ACTIVATED THE T/E FLAP FASDR 98UAL900009Warning Syst · malfunctionedUPON EVACUATION OF AIRCRAFT, AURAL WARNING SIGNAL FAILED TO OPERATE MID CABIN TO AFT CABIN. *S/D* THIS PROBLEM WAS NOT DUPLICATED. AFTER POWER WAS RESTORED, THE SYSTEM OPERATIONALLY CHECKED NORMAL. THE SYSTEM HAS ONLY ONE POWER SOURCE FOR THE FORWARD, CENTSDR 98UAL900008Wire · chafedSHORT CIRCUIT IN FRONT OF P39 PANEL RESULTED IN LOCALIZED FIRE AFT OF FORWARD GALLEY CHILLER. THE I/B WIRE BUNDLE WAS FOUND WITH SEVERE DAMAGE. DIVERTED TO LHR. *S/D* ALL WIRES REPAIRED PER BOEING STANDARD WIRING PRACTICES MANUAL CH 20. BECAUSE OF THE SEVSDR 97UAL900860Battery · dischargedEMERGENCY EXIT FLOOR LIGHTING IN RIGHT SIDE OF CABIN ROWS 21 TO 29 COMES ON INTERMITTENTLY. *S/D* THE CAUSE OF THE INTERMITTENT EEL WAS FOUND TO BE A BAD BATTERY ASSEMBLY. UAL CORRECTED THE PROBLEM BY REPLACING THE BATTERY ASSEMBLY WITH AN OVERHAULED, RECHASDR 97UAL900859Eicas Message · malfunctionedLEFT WING SLIDE EICAS MESSAGE CAME ON INTERMITTENTLY ON TAXI OUT. *S/D* ACCOMPLISHED LT OFF-WING ESCAPE SYSTEM CHECK OF ADJUSTMENT OF SLIDE COMPARTMENT DOOR PROXIMITY SENSOR. THE SENSOR WAS FOUND WITHIN LIMITS. ACCOMPLISHED CHECK OF DOOR ADJUSTMENT AND DOOSDR 97UAL900851Comprssor · deterioratedRIGHT ENGINE COMPRESSOR STALL. RETURN TO FIELD. ENGINE WAS NOT SHUT DOWN, OVERWEIGHT LANDING. *S/D* ENGINE SURGED ON TAKEOFF DUE TO GENERAL DETERIORATION OF THE HIGH PRESSURE COMPRESSOR AND EXCESSIVE BLADE TIP CLEARANCES. ENGINE WAS REPLACED.SDR 97UAL900827Slide · will not testLEFT OVERWING SLIDE SYSTEM WILL NOT TEST IN EITHER SYSTEM 1 OR 2. *S/D* ACCOMPLISHED CHECK PER MEL 25 360. GROUND CHECK GOOD. SYSTEM RETURNED TO NORMAL. REPLACED RELAYS K1, K5.SDR 97UAL900783Fire Card · failedRIGHT ENGINE NR 1 FIRE LOOP STATUS MESSAGE DISPLAYS CONTINUOUSLY. *S/D* PROBLEM CAUSED BY A FAULTY AUTOMATIC FAULT AND LOGIC TEST CARD (AFOLTS). REPLACED CARD, SYSTEM OPS CHECKS GOOD.SDR 97UAL900764Fire Loop · intermittentRIGHT ENGINE FIRE LOOP 2 DISPLAYED INTERMITTENTLY DURING FLIGHT.SDR 97UAL900763Power Supply · inoperativeSECTION OF EMERGENCY TRACK LIGHTS FROM 6AB TO 13AB REMAIN ON WITH SWITCH ARMED AND OFF POSITIONS. REPLACED POWER SUPPLY. OPS CHECK OKAY.SDR 97UAL900755Airframe · vibrationCREW REPORTED VIBRATION AND RUMBLING AT RIGHT SIDE OF MID CABIN AREA. STARTED AROUND 320 KTS. RETURNED TO DUS. ETOPS. *S/D* SEQ NR 3272003: CREW FELT AND HEARD NOISE; SUGGESTED LOOSE EXTERIOR PANEL. A/C CK'D FOR OPEN OR LOOSE PNL, DOOR AND LNDG GR DRS, FOSDR 97UAL900727Tr Unit · intermittentWEATHER RADAR FAIL ON HSI. DUMPED FUEL, RETURNED TO FIELD, OVERWEIGHT LANDING. *S/D* FOUND WEATHER RADAR TRANSCEIVER FAILED. REPLACED WEATHER RADAR TRANSCEIVER.SDR 97UAL900728Actuator · leakingCENTER HYD QUANTITY DROPPED TO .44. WITH PUMPS OFF, QUANTITY DROPPING SLOWLY. DIVERTETED TO GRU. FOUND RT MLG TRUCK POSITION ACTUATOR LEAKING. REPLACED ACTUATOR AND FILLED CTR SYSTEM.SDR 97UAL900707Bpcu · malfunctionedFLIGHT DECK EXPERIENCED A MOMENTARY ELECTRICAL POWER FAILURE. AUTO-PILOT DROPPED-OFF, POWER SELF RESTORED WITH NO EICAS MESSAGES. PASSENGER CABIN EXPERIENCED NO ELECTRICAL POWER LOSS. *S/D* BUS POWER CONTROL UNIT WAS REPLACED. NO FURTHER DISCREPANCY HAS OSDR 97UAL900702Compressor Vane · brokenAPU AUTO SHUTDOWN AT DEPARTURE TIME. *S/D* FOUND APU DRIVEN COMPRESSOR DEWHISTLER VANE BROKEN. IMPELLER FOD. APU REPLACED.SDR 97UAL900689Pneumatic Sys · inoperativeAPU PNEUMATIC PRESSURE AT 5 PSI, PNEUMATICS INOP.SDR 97UAL900671Fire Loop · malfunctionedRIGHT ENGINE FIRE LOOP 2 FAILS TEST. *S/D* ACFT EXPERIENCED A CHRONIC RIGHT ENGINE FIRE LOOP STATUS MESSAGE INFLIGHT, OK ON GROUND. SYSTEM WIRING WAS EXTENSIVELY CHECKED AND SEVERAL SYSTEM COMPONENTS WERE REPLACED. PROBLEM WAS ATTRIBUTED TO THE LWR AND/OR SDR 97UAL900652Lights · illuminatedAFTER LANDING ON TOUCHDOWN ROLL, EMERGENCY LIGHTS ILLUMINATED THROUGHOUT THE AIRCRAFT. *S/D* DEPOWERED ELECTRICAL POWER FROM AIRCRAFT. RESET EMERGENCY LIGHTS, OPS OK.SDR 97UAL900632Pin · sheared2.5 BLEED DISCONNECTED FROM BLEED VALVE. ENGINE CHANGE REQUIRED. *S/D* BELL CRANK PIVOT PIN SHEARED. REPAIRED 2.5 BLEED LINKAGE. REPLACED PIVOT PIN WITH IMPROVED PIN, (P/N 510264). REPLACED BLEED VALVE SLIDER BLOCKS WITH ROLLERS.SDR 97UAL900631Fire Panel · malfunctionedLEFT ENGINE OVERHEAT/FIRE TEST PANEL GAVE INDICATION INTERMITTENTLY. *S/D* FAULTY FIRE/OVERHEAT TEST PANEL GAVE INTERMITTENT INDICATON. REPLACED PANEL AND SYSTEM OPERATIONAL CHECKED NORMAL. PART IS NON-STOCK/NOT RECOVERABLE AND SPECIFIC COMPONENT FAILURE USDR 97UAL900595Oil · decreasedRIGHT ENGINE OIL QUANTITY DECREASED TO 1 QUART. AIRCRAFT DIVERTED TO YQX. ENGINE WAS NOT SHUT DOWN. *S/D* SUSPECT LEAK AT NR 3 BEARING OIL SCAVENGE TUBE UPPER B-NUT. NO DEFECTS WERE FOUND. POSSIBLE INSTALLATION OR TORQUING ERROR. REVIEWED INSTALLATION ASDR 97UAL900588Battery Pack · dischargedEMERGENCY EXIT THRESHOLD LIGHT BY DOOR 2L AND 2R WILL NOT GO OUT. *S/D* REPLACED BATTERY PACK UNDER FLIGHT ATTENDANT JUMP SEAT AT SEAT 2R AND RECYCLED SYSTEM, OPS CHECK OK.SDR 97UAL900547Battery · failedAPU WILL NOT START. BATTERY VOLTAGE DROPS TO 15 VOLTS DURING OPERATIONAL CHECK. *S/D* APU BATTERY FAILED. REPLACED BATTERY.SDR 97UAL900546Prsov · cloggedWHILE DESCENDING ON APPROACH, THE RIGHT ENGINE BLEED AIR TRIPPED OFF. *S/D* PRSOV MALFUNCTION. SHOP FOUND PRSOV REMOVABLE ORIFICE CLOGGED AND SENSE LINE LOOSE.SDR 97UAL900518Brakes · smokingDURING TAXI, ANOTHER AIRCRAFT PILOT REPORTED SEEING SMOKE COMING FROM THE RIGHT MAIN LANDING GEAR. *S/D* UPON FURTHER INSPECTION IN THE LT AND RT GEAR AND WHEEL WELLS, FOUND NO EVIDENCE OF SMOKE OR DEFECTS. BRAKE TEMPS WERE WITHIN LIMITS.SDR 97UAL900502Filter · dirtyABORTED TAKEOFF AT LHR AT 90 KNOTS DUE TO RT ENGINE BLEED OFF LIGHT ILLUMINATED AND EICAS MESSAGE RIGHT ENGINE BLEED OFF. *S/D* REPLACED RH PRSOV 02 JULY. SHOP FOUND INLET FILTER COMPLETELY CLOGGED, PREVENTING VALVE FROM OPENING.SDR 97UAL900490Tailskid · strikeON LANDING, TAIL SKID LIGHT ILLUMINATED. *S/D* AIRCRAFT WAS OVERROTATED CAUSING TAILSKID DRAG. TAILSKID DRAG CHECK WAS ACCOMPLISHED PER MM 53-51-32 AND FOUND TO BE SATISFACTORY.SDR 97UAL900475Bypass Valve · failedWHEN RETRACTING FLAPS, TE DISAGREE MSG APPEARED WHEN FLAP HANDLE WAS MOVED FROM 5 DEG TO 1 DEG. RETURNED TO JFK. *S/D* A FAULTY TRAILING EDGE FLAP POWER DRIVE UNIT BYPASS VALVE PREVENTED AFT FLAPS FROM RETRACTING TO THE COMMANDED POSITION. THE FLAP/SLAT ELSDR 97UAL900393Actuator · failedAILERON LOCK LIGHT CAME ON DURING CLIMB AT 300 KNOTS IAS. EICAS SHOWED NO OUTBOARD AILERON MOVEMENT DURING TURN. LIGHT WENT OUT BY ITSELF AFTER 20 MINUTES AT 0.80 MACH. *S/D* AN INVALID POSITION INDICATION FROM THE LEFT AILERON LOCKOUT ACTUATOR CAUSED THE SDR 97UAL900391Start Syst · malfunctionedUNABLE TO START APU AT ARRIVAL. *S/D* RAN APU, OPERATIONS CHECK NORMAL. AN OIL QUANTITY INDICATION SYSTEM FALSE MESSAGE IS SOMETIMES REPORTED AND IS SUSPECT IN THIS DISCREPANCY. THIS CAN RESULT FROM SERVICING THE APU OIL WHEN IT IS RUNNING. NO OTHER INCIDSDR 97UAL900358Pitot Line · looseTAKEOFF ABORTED APPROXIMATELY 90 KNOTS DUE TO NO CAPTAIN'S AIR SPEED INDICATION. *S/D* FOUND LOOSE PITOT ON LEFT ADC. SECURED PITOT LINE, AIRSPEED OPS NORMAL.SDR 97UAL900335Circuit Breaker · failedAIRCRAFT RETURNED TO SFO AFTER BOTH UTILITY BUS OFF LIGHTS CAME ON DURING TAKEOFF. *S/D* LEFT GENERATOR CONTROL BREAKER AUXILIARY CONTACT FAILED. REPLACED LEFT AND RIGHT GENERATOR CONTROL BREAKERS.SDR 97UAL900334Auto Throttle · malfunctionedABORTED TAKEOFF AT LOW SPEED WHEN AN AUTO THROTTLE DISC AMBER EICAS MESSAGE CAME ON. *S/D* FLIGHT CREW RE-ENGAGED AUTO THROTTLE AFTER TAKEOFF. ALL MODES FUNCTIONED NORMALLY. MCDP FLT FAULTS SHOWED TLA LT, TLA RT, AND MCDP-TMC TEST COMMAND FAIL MESSAGES. ASDR 97UAL900297Scavenge Pump · failedON TAXI TO THE GATE, EXCESSIVE BLUE COLORED SMOKE STARTED POURING OUT OF APU. *S/D* THE TURBINE SCAVENGE PUMP FAILED AND CAUSED THE SMOKE OUT OF THE APU TAILPIPE DUE TO OIL NOT BEING SCAVENGED BACK TO THE GEARBOX. REPLACED THE SCAVENGE PUMP.SDR 97UAL900278Wire · chafedRIGHT ENGINE BLEED OFF' EICAS AND BLEED OFF WARNING LIGHT DISPLAYED DURING CLIMBOUT. *S/D* MAINTENANCE FOUND WIRE CHAFED THROUGH AT PRESSURE REGULATING VALVE, CONTACTING ADJACENT METAL TUBING. REPAIRED WIRING AND SECURED.SDR 97UAL900264Press Valve · malfunctionedTAKEOFF ABORTED DUE TO AURAL SOUND AND WARNING MESSAGE RT ENG PRV (RIGHT ENGINE PRESSURE REGULATING VALVE). REPLACED PRV (PRESSURE REGULATING VALVE) AND PRV CONTROLLER.SDR 97UAL900325Gasket · wornLEFT HYDRAULIC EICAS MESSAGE AND QUANTITY LIGHT ON OVERHEAD CAME ON DURING TAKEOFF WITH HYDRAULIC QUANTITY INDICATION DROP. *S/D* REPLACED LEAKING STAB TRIM SERVO PLATE GASKET.SDR 97UAL900246Eec Message · illuminatedRIGHT ENGINE CONTROL EICAS MESSAGE APPEARED MOMENTARILY SHORTLY AFTER TAKEOFF. RIGHT ENGINE CONTROL AND RIGHT ENGINE EEC (ELECTRONIC ENGINE CONTROL UNIT) C1 MESSAGE REMAINED ON DISPLAY FOR ENTIRE FLIGHT. ENGINE OPERATION APPEARED NORMAL.SDR 97UAL900226Idg · failedRIGHT GENERATOR LIGHT CAME ON DURING APPROACH. *S/D* REPLACED RIGHT INTEGRATED DRIVE GENERATOR.SDR 97UAL900215Module · failedFORWARD LAVATORY WASTE TANK LOGIC CONTROL MODULE/CONTINUOUS LEVEL SENSOR REFLECTED FALSE FULL TANK INDICATION. CALIBRATION OF LOGIC CONTROL MODULE/CONTINUOUS LEVEL SENSOR LOST. REMOVED FOREIGN OBSTRUCTION AND RECALIBRATED LOGIC CONTROL MODULE.SDR 97UAL900156Prsov · failedRETURNED TO EZE, DUE TO RIGHT ENGINE BLEED VALVE FAILURE. SUPPLEMENTAL DATA UPDATE PRSOV (PRESSURE REGULATING AND SHUTOFF VALVE) FAILED DUE TO CLOGGED MAIN INLET FILTER. REPLACED PRSOV.
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