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 CA001201007Sensor · dirty(CAN) FLIGHT RETURNED TO FCO, DUE LANDING GEAR DOOR CAUTION LIGHT AND STATUS MESSAGE LG MONITOR. GEAR CYCLED IN FLIGHT, BUT SNAG STILL REMAINED. LANDING WEIGHT WAS 380,000 LBS. BITE FUNCTION OF PSEU INDICATED TARGETS S234, S235 AND S257, WERE THE PROBLEM. SENSSDR CA001012007Actuator · failed(CAN) DURING APPROACH , GEAR DOWN, FLAPS 20, AUTOPILOT ON. VIBRATION, FELT LIKE SPOILERS UP. CONTROL WHEEL SHOWED 1/2 TO 3/4 (TOTAL) WHEEL MOVEMENT ROLL TO RIGHT. DISCONNECTED AUTOPILOT & AUTO THROTTLE, A AIRCRAFT, THEN ROLLED HARD TO LEFT, REQUIRED LARGE AMOSDR CA000925010Door · damaged(CAN) AIRCRAFT DEPARTED, CDL32-12A APPLIED PIOR TO DEPARTURE DUE R/H GEAR TRUNNION DOOR DAMAGE. CDL INDICATED A MINOR AIRCRAFT WEIGHT PENALTY. VMO/MMO SWITCH PLACED IN ALTERNATE POSITION DUE CDL. ON AKEOFF, (APPROX 250 KTS) OVERSPEED AURAL WARNING AND BARBER PSDR CA000925025Control Unit · faulty(CAN) A/C 641, AUG 20/2000, FLT 30, LOG SEQUENCE 0225444. AT APPROXIMATELY 14,000 FEET, LEADING EDGE SLAT ASYMMETRY WARNING ILLUMINATED ON EICAS, FLAP POSITION NEEDLE INDICATED BETWEEN 1 UNIT AND UP. RETURNED TO PEK. BITE CHECK COMPLETED ON PSEU, NIL FAULTS INSDR CA000731008Control Unit · failed(CAN) A/C 640, JULY 22/2000, FLT 51, YYZ, LOG SEQUENCE 0272985, ON LANDING YYZ, CAPTAIN DECLARED AN EMERGENCY, DUE TRAILING EDGE FLAP ASYMMETRY OCCURRED WITH FLAPS BEYOND 20 DEGREES. LANDED WITHOUT INCIDENT. SYSTEM RESET AS PER FAULT ISOLATION MANUAL 27-51-00SDR CA000731007Harness · chafed(CAN) RIGHT GENERATOR OFF LIGHT ILLUMINATED IN CRUISE. EICAS MASTER CAUTION FOR RIGHT AC BUS OFF. GENERATOR RESET, APU STARTED, BUT TIE BUS WOULD NOT RESET. AFTER 5 MINUTES GENERATOR TRIPPED, BUS TIE RESET, RIGHT AC BUS TRIPPED OFF AGAIN. DUE PREVIOUS SNAGS, ASDR CA000706003O-Ring · leaking(CAN) CREW REPORTED CENTER SYSTEM HYDRAULIC LOW QUANTITY LIGHT ON. TURNED OFF ALL CENTER HYDRAULIC PUMPS. FLIGHT DIVERTED, DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. ON INSPECTION FOUND LEAK AT DELTA P FITTING ON CENTER SYSTEM CASE DRAIN FILTER MODULE. O-SDR CA000518003Fan · failed(CAN) DURING GROUND CHECK LOUD NOISE AND VIBRATION IN J CLASS CABIN UNDER FLOOR. STRONG BURNING SMELL IN AVIONICS BAY. REPLACED NR1 EQUIPMENT COOLING FAN. DUCT, ELECTRICAL CONNECTORS AND WIRING INSPECTED, FOUND SERVICEABLE.SDR CA000518002Light · inoperative(CAN) 10 MINUTES PRIOR TO DEPARTURE CREW REPORTED SMELL OF SMOKE IN FORWARD GALLEY AREA. PASS DEPLANED. REACED TO THE LIGHT ASSY ON COCKPIT OVERHEAD PANEL. REPLACED.SDR CA000410004Apu · failed(CAN) APPROX 15 MINS PRIOR TO DEPARTURE APU FAILED AND COMPONENTS WERE OBSERVED EXITING TAILPIPE. APU NOT UNDER LOAD AT TIME OF FAILURE. APU AND TAILPIPE REPLACED.SDR CA991229014Seat · malfunctioned(CAN) SHORTLY AFTER TAKEOFF SEAT 3G RECLINED ON ITS OWN AND NO FURTHER CONTROL AVAILABLE. HOT PLASTIC SMELL THEN PERSISTED IN FORWARD CABIN. POWER TO ALL SEATS TURNED OFF, RECIRC FAN OFF ON FIX. A/C RETURNED FOR REPAIRS.SDR CA991027009Tire · failed(CAN) AFTER LANDING, MAINTENANCE REPORTED SEVERE AIRCRAFT DAMAGE DUE NR 6 TIRE TREAD BLOWN. SEVERE DAMAGE TO LEFT INBOARD FLAP, LEFT MAIN FLAP, AND NR 6 SPOILER. PARTS REPLACED.SDR CA990707023Fitting · broke(CAN) RT TRAILING EDGE FLAP OUTER DEFLECTION CONTROL TRACK SUPPORT FITTING BROKEN AT BOTTOM LUG. REPLACED.SDR CA990310062Wire · failed(CAN) DURING INSPECTION, FOUND WIRES SHORTED AND BROKEN AT RT OVERWING EXIT FORWARD HEATER BLANKET CONNECTOR, DUE TO PHYSICAL DOOR TO CONNECTOR INTERFERENCE. WIRES SEPARATED, BURNT AND MELTED, SURROUNDING AREA BLACKENED WITH SMOKE. REPAIRED AS REQUIRED.SDR CA990310061Angle · cracked(CAN) ZONAL INSPECTION REVEALED 8 FLOOR SUPPORT ANGLES CRACKED AT FLOORBEAM STA 246. ANGLES REPLACED.SDR CA981125014Light · failed(CAN) FLIGHT DIVERTED DUE TO SMOKE EMITTING FROM SPOT LIGHT IN FORWARD GALLEY. REPLACED LIGHT ASSY AND TRANSFORMER.SDR CA981125013Outflow Valve · failed(CAN) ON TAKEOFF, EICAS MESSAGE R PRV. REPLACED PRESSURE REGULATING VALVE. PART TC: 1,618.SDR CA980707028Hpsov · failed(CAN) TAKEOFF ABORTED AT 70 KNOTS DUE MASTER CAUTION SOUNDED AND EICAS MESSAGE R-HPSOV AND R-BLEED LT. A/C OPERATED PER MEL WITH R-HPSOV AND T/R LOCKED OUT. REPLACED HPSOV. A/C SERVICEABLE.SDR CA980325012Acm · seized(CAN) A/C RETURNED TO GATE DUE LT PACK TEMP EICAS MESSAGE AND LT PACK INOP LIGHT ON. LT ACM REPLACED.SDR CA980317028Idg · failed(CAN) ABORTED TAKEOFF DUE EICAS MESSAGE. RT GENERATOR DRIVE FOLLOWED BY RR GEN AND LT AND RT UTIL BUSSES. RT GENERATOR DRIVE MESSAGE DISSAPPEARED DURING TAXI IN. SERVICED IDG WITH 3 QUARTS OIL. A/C OPERATED MEL WITH RT IDG DISCONNECTED. IDG REPLACED.SDR CA970904012Sensor · intermittent(CAN) ON APPROACH WHEN GEAR SELECTED DOWN NOSE GEAR DID NOT EXTEND. GEAR LEVER CYCLED TO 'OFF' AND TO 'DOWN'. NOSE GEAR EXTENDED.SDR CA970815001Computer · defective(CAN) LEFT HAND EICAS DISAGREE MESSAGE ON TAXI. REPLACED.SDR CA970507008Sensor · failed(CAN) IN CRUISE STATUS MESSAGE DISPLAYED, AIR/GROUND DISAGREE, RH MAIN GEAR TILT SENSOR REPLACED.SDR CA970327008Brake · disintegrated(CAN) FOUND PIECES OF BRAKE ON GROUND DURING WALKAROUND. ON DISASSEMBLY ROTOR DRIVE KEY BRACKETS FOUND SEPARATED. SEPARATOR IN TWO PIECES WITH TORQUE TUBE SPLINES MISSING. TORQUE TUBE FULL OF GREASE. SEAL CARRIER 'O' RING MISSING ALLOWING GREASE TO ENTER TORQUSDR CA970203002Lock Actuator · failed(CAN) AFTER TAKEOFF GOT EICAS MESSAGE 'GEAR DISAGREE' AND 'GEAR DOORS' ACCOMPANIED BY LANDING GEAR LIGHT INDICATIONS OF DOORS 'AMBER', GEAR 'AMBER' LEFT 'GREEN' GEAR INDICATION. RECYCLED LANDING GEAR SEVERAL TIMES WITH NO CHANGE. AIRCRAFT RETURNED.L/H MAIN GEASDR CA960801004Radome · hail damage(CAN) HAIL DAMAGE TO RADOME AND LH AND RH LEADING EDGE DEVICES.SDR CA960801003Radome · hail damage(CAN) BIRD STRIKE AND HAIL DAMAGE TO RADOME, WINDSHIELD REPLACED TEMPORARY REPAIR TO RADOME.SDR CA960725103Pressure Plate · missing(CAN) AIRCRAFT RETURNED TO GATE DUE TO MASSIVE HYDRAULIC LEAK #5 BRAKE DISINTEGRATED. PRESSURE PLATE MISSING, #1 STATOR HAD DISINTEGRATED. ALL PISTONS HAD HYPER EXTENDED. ONE PISTON BROKEN OUT OF BACK PLATE. REPLACED.SDR CA960626102Electronic Unit · failed(CAN) AFTER TAKEOFF FLAPS WOULD NOT RETRACT FROM 1 TO UP. TRIED UNSUCCESSFULLY SEVERAL TIMES, ALSO ALT FLAP, NO CHANGE. REPLACED FLAP/SLAT ELECTRONIC UNIT.SDR CA960612003Generator · failed(CAN) ON RAMP, AFTER START, INTERMITTENT STATUS APPEARED "LIDG TEMP SENS". STATUS WENT OUT AND DID NOT OCCUR AGAIN. ON CLIMB OUT "RIDG TEMP SENS" STATUS MESSAGE INTERMITTENTLY ILLUMINATED AND WENT OUT. FIVE HOURS LATER "RIDG TEMP SENS" REAPPEARED ALONG WITH EISDR CA960528102Coffee Maker · burnt(CAN)AFT GALLEY COFFEE MAKER SPARKING AND FLASH FOLLOWED BY SMOKE. CBS PULLED AND UNIT REPLACED.SDR CA960515102Panel · missing(CAN) DURING LAYOVER CHECK FOUND FAIRING ACCESS PANEL 195CL MISSING. FOUR ANCHOR NUTS FOUND DAMAGED. REPAIRED.SDR CA960423109Frames · damaged(CAN)ON LANDING THE TAIL SKID CONTACTED THE RUNWAY. THE IMPACT DROVE THE ACTUATOR UPWARD, SHEARING BOTH PIVOT BEARINGS, THE HYDRAULIC SUPPLY LINE & THE TWO 50 TON SAFETY RETAINER CABLES. THE TOP OF THE ACTUATOR CONTACTED THE LOWER END ON THE HORIZONTAL STAB JASDR CA960311102Valve · failed(CAN)AFTER TAKEOFF AFT CARGO OVERHEAT EICAS FOLLOWED AND RETURNED TO BLOCKS. REPLACED AFT CARGO HEAT VALVE WHICH WAS IN POOR CONDITION - TRYING TO DRIVE BEYOND ITS LIMITS.SDR CA951116002Outer Cylinder · corroded(CAN)THE RH MAIN LANDING GEAR INSPECTED AS PER AD 95-19-10, FOUND VISIBLE EVIDENCE OF CORROSION AT THE UPPER TRUNNION AFT BUSHING TO THE CYLINDER SURFACE. CORROSION CONFIRMED BY CHEMICAL SPOT TEST. CYLINDE R REPLACED.SDR CA951123110Tire · cap missing(CAN)ON ARRIVAL #7 MAIN WHEEL CAP WAS FOUND THROWN. DAMAGE TO 7 SPOILER RHS INBOARD MAIN FLAP, TWO UNDERWING PANELS, AND THE SPOILER SUPPORT BEAM LOWER CORD. #7 SPOILER REPLACED, FLAPS AND PANELS REPAIRED AND #7 AND #8 WHEELS REPLACED.
Back to Boeing 767-375