Boeing 767-233
Service difficulty reports · 154
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 = '767233' 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 = '767233' 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 CA020121003Transducer · failed(CAN) EICAS MESSAGE FOR FLAP / SLAT ELEC. DISPLAYED.REPLACED THE ROTARY DIFFERENTIAL TRANSDUCER M603 AND ADJUSTED AS PER AMM 27-51-26-424-020. FOUND SERVICEABLE.SDR CA020104008Sensor · failed(CAN) EICAS MSG AIR/GRND DISAGREE DISPLAYED IN FLIGHT AFTER TAKE OFF FROM TORONTO. RIGHT GEAR SYST. 1 TILTED PROX. SENSOR S246 REPLACED. SYSTEM BITE CHECKED SERVICEABLE.SDR CA011019008Heat Exchanger · leaking(CAN) RIGHT HAND ENGINE SHUTDOWN AFTER START-UP DUE TO ENGINE FIRE. EMERGENCY EVACUATION ON LEFT END SIDE OF THE AIRCRAFT. ENGINE FIRE BOTTLES DISCHARGED.REPLACED RIGHT ENGINE, AFTER INVESTIGATION FOUND THAT THE CAUSE OF THE TAIL PIPE FIRE WAS A RESULT OF THE SDR CA010906014Fairing · damaged(CAN) ON ARRIVAL FOUND RT INBOARD LEADING FLAP HINGE FAIRING DAMAGED. DAMAGE APPEARED TO BE FROM MISSING MID SPAR FUSE PIN ACCESS PANEL LT SIDE OF RT ENGINE PYLON. LEADING EDGE FLAP HINGE FAIRING AND MID SPAR ACCESS PANEL REPLACED.SDR CA010727023Bushing · loose(CAN) BUFFETING FELT THROUGH THE FLIGHT AND INCREASE IN FREQUENCY DURING CLIMB OUT. THE LEFT ELEVATOR WAS INDICATING LOWER THAN THE RIGHT AND WOULD FLUCTUATE UPWARD. INVESTIGATION REVEALED LEFT END OUTBOARD POWER ACTUATOR (P.C.A.) EYE END BUSHING LOOSE AND SUPSDR CA010727029Actuator(CAN) BUFFETING FELT THROUGH THE FLIGHT AND INCREASED IN FREQUENCY DURING CLIMB OUT. FOUND TO BE THE APU DOOR ACTUATOR AT FAULT. HALF INCH PLAY IN ACTUATOR BEARING AND SEAL DAMAGE. REPLACED THE APU DOOR ACTUATOR.SDR CA010910007Spring · missing(CAN) ON WALK AROUND IN YYZ, FOUND RIGHT HAND NOSE WHEEL SPIN BRAKE SPRING MISSING. INSTALLED SPIN BRAKE SPRING.SDR CA010308003B-Nut · loose(CAN) ENROUTE LEFT ENGINE STARTED TO LOOSE OIL RAPIDLY. ENGINE THROTTLED BACK TO IDLE AND CREW DIVERTED. ENGINE WAS NOT SHUTDOWN. ENGINE RUN CARRIED OUT. ENGINE OIL LINE SUPPLY B NUT FOR 3/4 BEARING FOUND LOOSE, NOT LOCKWIRED PROPERLY AND LEAKING. B NUT TIGHTESDR CA010115004Actuator · failed(CAN) AILERON LOCKOUT IN CRUISE/LANDING/GATE.FOUND CIRCUIT BREAKER POPPED, RIGHT AND LEFT AILERON RESET, CARRIED OUT TEST. SPOILER AILERON MODULE FAULTED RIGHT HAND AILERON LOCKOUT. CIRCUIT BREAKER POPPED AGAIN. CHANGED RIGHT HAND AILERON LOCKOUT ACTUATOR.SDR CA001110009Motor · failed(CAN) ON APPROACH TO TORONTO, CENTRE HYDRAULIC LOSS. EXTENDED THE GEARS MANUALLY, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. HYDRAULIC FILTERS, AC MOTOR HYDRAULIC PUMP DRIVE, AND AIR DRIVEN PUMP UNIT WERE CHANGED. OPERATION CHECK CARRIED OUT, NORMAL.SDR CA001110007Panel · missing(CAN) ON AIRCRAFT ARRIVAL FOUND PANEL MISSING ON LEFT HAND WING ROOT TO FUSELAGE. PANEL 195CL INSTALLED NEW ANCHOR NUTS AND PANEL.SDR CA001110013Card · faulty(CAN) RIGHT HAND ENGINE OVERHEAT ON ENGINE CREW ALERT SYSTEM, AND MASTER CAUTION CAME ON ON CLIMB OUT. ENGINE SHUT DOWN AND DIVERTED INTO WINNIPEG. FOUND RIGHT HAND ENGINE LOGIC CARD M10274 AT FAULT. REPLACED M10274 CARD.SDR CA001019026Seat Back · collapsed(CAN) AFTER TAKEOFF, PASSENGER SEATS 22H & 22K BACKREST METAL FRAME COLLAPSED. BACKREST FELL ON THE PASSENGERS SEATED IN 23 H/K. NO REPORTED INJURY. SEAT ASSEMBLY REPLACED.SDR CA001019025Apu · failed(CAN) DURING PUSH BACK AND ENGINE START OF RIGHT HAND ENGINE, AUXILIARY POWER UNIT FAULT LIGHT AND SHUTDOWN. AUXILIARY POWER UNIT HAD INTERNAL SEIZURE, CAUSING TURBINE TO BE DISCHARGED. METAL PIECE WAS EJECTED OUT OF EXHAUST PORT. AUXILIARY POWER UNIT CHANGED SDR CA001019024Engine · surges(CAN) AT FLT390, 25NM FROM DOWNWIND OF A THUNDERSTORM, IN LIGHT CLOUD, LEFT HAND ENGINE EXPERIENCED A SURGE, CHECK LIST CARRIED OUT, THROTTLE RETURNED TO CRUISE POWER AND EXPERIENCED A SECOND SURGE. DESCENT TO FL350, ALL PARAMETERS NORMAL. CREW ELECTED TO DIVESDR CA001004016Panel · missing(CAN) ON WALKAROUND FOUND PANEL MISSING ON INBOARD SIDE OF RIGHT HAND ENGINE STRUT. NIL PART AVAILABLE, PLACED ON MEL 54-51-0100. NEW PANEL INSTALLED.SDR CA000830011Fan · failed(CAN) SMOKE IN COCKPIT IN FLIGHT WHILE EXITING AN INBOUND HOLD. AFTER INVESTIGATION, AN AFTER SMOKE DISSIPATED AN EICAS (ENGINE INDICATION AND CREW ALERT SYSTEM) MESSAGE APPEARED FOR A TRIPPED OFF LINEOF THE FORWARD ELECTRICAL SUPPLY FAN. REPLACED AIR COOLING SDR CA000721005Control Unit · failed(CAN) DURING FLAP EXTENSION ON GROUND EICAS WARNING MESSAGE LE SLAT DISAGREE ON FLAPS LEVER AND THE LEADING EDGE ALTERNATE SWITCH CYCLED AND MESSAGE CLEARED. AFTER TAKE OFF SAME MESSAGE APPEARED AND CLEARED ITSELF AFTER FLAP RETRACTION. FOUND LEADING EDGE AND SDR CA000721003Warning System · activated(CAN) DURING TAKE-OFF ROLL AT 50 KNOTS TAKE-OFF CONFIG WARNING CAME ON EICAS. TAKE-OFF REJECTED MAINTENANCE RERACKED CONFIG CARDS. ON SECOND TAKE-OFF CONFIG MESSAGE APPEARED AT 120 KNOTS TAKE-OFF REJECTED A SECOND TIME.TAKE-OFF WARNING CARD REPLACED AND OPERASDR CA000721004Panel · dislodged(CAN) PANEL CEILING TRIM OVER SEAT 19-20-21 CABIN RIGHT SIDE, FELL OFF SHORTLY AFTER TAKE OFF. MINOR INJURY TO PASSENGER. FACIA PANEL VELCRO REPLACED, AND PANEL TRIM INSTALLED. CHECKED CABIN PANELS OK.SDR CA000530071Fan · failed(CAN) ELECTRICAL BURNING SMELL IN COCKPIT DURING APPROACH, ELECTRICAL COOLING SWITCH SELECTED TO OVERIDE SMELL DISSIPATED. NR 1 EQUIPMENT COOLING VAN SOURCE OF SMELL AND GRINDING DURING ROTATION. CHANGED.SDR CA000530073Line · ruptured(CAN) ON LANDING CENTER HYD SYSTEM FLUID DROPPED TO ZERO. PRESSURE LINE FROM CENTER HYD SYS PUMP RUPTURED. LINE REPLACED, SYS SERVICED AND LEAK CHECK OK.SDR CA000501030Generator · failed(CAN) LT ENGINE GENERATOR FAULT DURING FLIGHT BUT RUGHT HAND GEN COULD NOT POWER LT BUSS. APU USED TO POWER LT BUSS. LT INTRIGATED DRIVE GEN REPLACED, SYS SERVICEABLE.SDR CA000410031Seat Back · broken(CAN) SEATBACK 24H BROKE DURING DEPARTURE. CENTER HINGE PIN BOLT BROKE.SDR CA000328016Windshield · cracked(CAN) FIRST OFFICER SIDE WINDOW CRACKED IN FLIGHT. AT 350 FT RT TOP CORNER STARTED TO CRACK, BUBBLE AND ARC. EICAS MESSAGE APPEARED. WINDOW HEAT TURNED OFF AS PER QRH. WINDSHIELD REPLACED.SDR CA000328015Computer · failed(CAN) CARGO FIRE WARNING ON EICAS AP 410 FT AND SMOKE IN CABIN AFTER FIRE DRILL WITH NR 1 FIRE BOTTLE DISCHARGED IN CARGO BAY. SUSPECT DISCHARGE INTO BAY WAS SMOKE IN CABIN. REPLACED EICAS COMPUTER.SDR CA000222019Regulator · failed(CAN) SLIDE/RAFT HAD A 10 SECOND HUNG TIME ON TEST. CMM INDICATES 6 SEC MAX TIME DELAY. REGULATER REPAIRED AS PER CMM.SDR CA000222020Bearing · corroded(CAN) ELEVATOR HINGE NO 6 BEARING NOISE WHEN IN OPERATION. BEARING GREASE CONTAMINARED AND BEARING CORRODED. REPLACED.SDR CA000222018Regulator · failed(CAN) SLIDE/RAFT DAH A 10 SECOND HUNG TIME ON TEST. CMM INDICATES 6 SEC MAX TIME. REGULATOR REPAIRED IN ACC WITH CMM.SDR CA000209040Tire · failed(CAN) A/C ARRIVED WITH NR 3 WHEEL TIRE CAP MISSING REPLACED.SDR CA000209039Fuse · failed(CAN) RT GEAR FAILED TO RETRACT AFTER TAKEOFF, A/C RETURNED TO BLOCKS. HYD FUSE AND TRUCK TILT REPLACED.SDR CA000209038Chiller · failed(CAN) ON PREFLIGHT SMOKE COMING FROM REAR GALLEY AND BEGAN TO FILL CABIN PASS DEPLANED. DEACTIVATED BOTH CHILLERS AND REPLACED.SDR CA000110093Transmitter · failed(CAN) AFTER TAKEOFF, RT ENGINE OIL PRESSURE INDICATION IN AMBER AND DECREASING WITH THROTTLE MOVEMENT. A/C RETURNED, AFTER LANDING IDLE 57,58 PSI 13,14 OIL QTY, TEMP NORMAL. OIL PRESS TRANSMITTER REPLACED.SDR CA000110095Wire · overheated(CAN) AIRCRAFT HAD A HISTORY OF RT HYD INDICATION FLUCTUATIONS. TWO RT GEN FEEDER CABLES BADLY OVERHEATED CAUSING SOME OF ITS INSULATION TO MELT AND ALSO INSULATION ON ADJACENT WIRE BUNDLES. ALL DAMAGED CABLES REPAIRED.SDR CA000110089Computer · failed(CAN) ON CLIMB OUT, FIRST OFFICER LOST FLIGHT DIRECTOR INDICATIONS, CAPTAIN''S FD ALREADY ON DEVIATION, SELECTED CENTER SOURCE, FD RETURNED BUT THEN AUTOPILOT DISCONNECTED. A/C DIVERTED. LEFT FLIGHT CONTROL COMPUTER REPLACED, SEVICEABLSE.SDR CA991231031Line · leaking(CAN) RT HYD QTY DROPPED STEADILY ABOUT 30-40 PERCENT PER MINUTE. STOPPED AT .43 WHEN PUMPS TURNED OFF. FOUND RT ENG HYD PUMP FLEX LINE WORN THROUGH. REPLACED.SDR CA991231030Windshield · failed(CAN) FIRST OFFICERS WINDSHIELD SHATTERED ON APPROACH, WINDSHIELD REPLACED.SDR CA991210034Connector · chafed(CAN) DURING TAKEOFF, LT GENERATOR FAILED FOLLOWED BY BUS TRIP. NO INSTRUMENT ON CAPTAIN'SED 3 INCHES FROM CONNECTOR D414. REPAIRED SYS SERVICEABLE.SDR CA991008008Battery · failed(CAN) ON APPLICATION OF GROUND SERVICE POWER TO AIRCRAFT, BURNING SMELL REPORTED IN AIRCRAFT CABIN. TRUCKS CALLED. APU BATTERY FOUND TWO CELLS MELTED AND BATTERY SHOWING SIGNS OF OVERHEAT. REPLACED.SDR CA990715038Tire · failed(CAN) NR EIGHT MAIN WHEEL TIRE BLOWN ON LANDING. NR 7 AND NR 8 MAIN WHEEL ASSYS, ANTI-SKID CONTROL BOX, AUTO BRAKE CONTROL BOX, AND ANTI-SKID MODULE REPLACED.SDR CA990614082Fqic · faulty(CAN) AFTER FLIGHT LEVEL, FUEL CONFIGURATION EICAS MESSAGE ON. FUEL QTYS LT MAIN 8.6 AND RT MAIN 16.9. CROSS-FEEDING STARTED AND RETURNED TO BLOCKS. CARRIED OUT BIT TEST ON FUEL QTY INDICATION COMPUTER AND SHOWS A7 FAULT. FQIC REPLACED. SYSTEM SERVICEABLE.SDR CA990614090Switch · overheated(CAN) DURING FLT EQUIPMENT COOLING OVERHEAT ON IN ICAS, STANDBY SELECTED AND UNABLE TO CLEAR FAULT, OVERRIDE SELECTED AND FAULT CLEARED. SYSTEM RESET ANDS AME FAULTS. REPLACED OVERHEAT SWITCH S14 AND FLOW DETECTOR TS/04 IN FORWARD CARGO. SYSTEM SERVICEABLESDR CA990614091Fan · overheated(CAN) FORWARD EXHAUST EQUIPMENT COOLING FAN CIRCUIT BREAKER TRIPPED IN-FLIGHT, STRONG ELECTRICAL SMELL, SUBSIDED ONE MINUTE AFTER CIRCUIT BREAKER TRIPPED. REPLACED FORWARD EXHAUST FAN AND GROUND RUN SERVICEABLE.SDR CA990603026Cap · loose(CAN) LOST C-HYDRAULIC SYSTEM IN CLIMB-OUT. FOUND PLUG CAP LOOSE AT LEFT INBOARD AILERON INBOARD POWER CONTROL UNIT. PLUG TIGHTENED, SYSTEM SERVICED, AND LEAK CHECK CARRIED OUT SERVICEABLE.SDR CA990603023Yaw Damper · failed(CAN) LEFT YAW DAMPER EICAC MESSAGE DISPLAYED AFTER PUSHBACK, YAW PANEL AND LEFT YAW DAMPER SERVO REPLACED.SDR CA990603022Indicator · failed(CAN) TRAILING EDGE FLAPS DISAGREE MESSAGE CAME ON WHEN ATTEMPTING TO SELECT FLAPS AT 25 DEGREES, LANDING ACCOMPLISHED USING 20 DEGREE FLAPS. FLAP POSITION INDICATOR AND K353 AND K216 RELAYS REPLACED.SDR AU990420019Fcu · malfunctioned(AU) ON TAKEOFF, NR 2 ENGINE NEVER SPOOLED UP, BUT REMAINED AT IDLE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE NR 2 ENGINE FUEL CONTROL UNIT WAS REPLACED, LEAK CHECK AND CONTROL TRIM CHECKS WERE CARRIED OUT SERVICEABLE.SDR CA990603024Skin · damaged(CAN) LIGHTNING STRIKE ON ARRIVAL, DAMAGE FORWARD OF R1 DOOR AND STATIC WICK MISSING. REPAIRED DAMAGE AND REPLACED WICK.SDR CA990330078Servo · leaking(CAN) DURING FLIGHT, LEFT HYDRAULIC QUANTITY INDICATED .75. IT REDUCED STEADILY TILL LEFT SYSTEM PRESSURE, LEFT QUANTITY AND RUDDER RATIO MESSAGE APPEARED. AIRCRAFT DIVERTED. ON APPROACH, INOP LIGHT CAME ON. FOUND LEAK COMING FROM RUDDER POWERPACK AREA. SDR CA990330074Actuator · failed(CAN) AILERON LOCKOUT MESSAGE ON ENGINE INDICATING AND ALERT AND CREW ALERT SYSTEM ON CLIMB AND DESCENT. REPLACED RT AILERON LOCKOUT ACTUATOR.
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