Boeing 767-333
Service difficulty reports · 163
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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 = '767333' 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 = '767333' 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 CA100907003Relay · failedJUST OVER 6 HRS AFTER DEPARTURE, CREW REPORTED THERE WERE NO SERVICABLE LAVS AND THERE WAS A STRONG ELECTRICAL BURNING ODOR FROM ONE OF WASHROOMS. CREW DECLARED AN EMERGENCY AND DIVERTED. VISUAL INSP CARRIED OUT BEHIND ALL LAV PANELS. NO INDICATION OF ANY DSDR HALA2010072400331Skin · damagedDURING MX, SKIN DAMAGED. LOCATION LOWER AFT SKIN BODY STA 1780. BETWEEN STR 26R AND 27R, DAMAGE 4 IN X 4 IN. PERFORMED LAP SPLICE EXTERNAL REPAIR 12. IAW SRM 53-00-01-2-12, HAL M105 FILE NR R0059.SDR HALA2010062800279Computer · malfunctionedETOPS SIGNIFICANT SYS - (BTB) ELEVATOR FEEL STATUS MESSAGE ON AFTER START. ACCOMP FIM27-31-01, FIG 106, STEP 1 TO BLOCK 11 (EXAM DPI FOR RETURN FILTER MODULE FOR LT & CTR HYD SYS NO DEFECTS NOTED. R & R ELEV FEEL COMPUTER TILL STEP 3F(10). ACCOMP AMM27-31-19 SDR CA100629007Wire · arcedSPARKS NOTED, EMITTING FROM IFE WIRE BUNDLE SECTION ADJACENT PANEL AE0224 NEAR PANEL 37 AND TR-4 CB FOUND POPPED. FOUND WIRE ARCING AND SHORT TO CLAMP NEAR BOTTOM OF PANEL AE0224. BUNDLE OPENED, CLEANED AND INSPECTED. REF DWG EH1986: WIRE EHI986-305-12WHT SHSDR CA100712007Display · faultySTRONG ELECTRICAL ODOR, ROW 26/27 ACFT IN FLIGHT. CONFIRMED COMPLAINT. ISOLATED FAULT TO SEAT 28D SVDU INTERNALLY OVERHEATED/FAULT. REPLACED SEAT 28D SVDU WITH P2 DOWNLOAD AND OPS TESTED SERVICEABLE.SDR HALA2010061400258Modulating Valve · failedETOPS SIGNIFICANT SYS - CTR HYD DEMAND PUMP EICAS ILLUM ON ARRIVAL. REMOVED THE MODULATING VALVE FOR THE ADP IAW AMM 29-11-04. 4526. INSTALLED ADP VALVE IAW AMM 29-11-04 OPS CHECK IAW AMM 29-11-00/501. NO LEAKS NOTED.SDR CA091125001Bearing · failed(CAN) NR 4 MAIN WHEEL INNER BEARING HAD A COMPLETE FAILURE. MAINTENANCE SPOTTED THE MAIN WHEEL SITTING AT AN ODD ANGLE ON THE GATE AND INVESTIGATED. OUTER BEARING AND THE PIECES LEFT FROM THE INNER BEARING HAVE BEEN HANDED OVER TO BOEING FOR FURTHER INVESTISDR CA090702002Support Bracket · cracked(CAN) AFTER LANDING, CREW OBSERVED A LARGE SECTION OF INBD NR 1 ENG TRANSLATING SLEEVE MISSING. MX MEASURED DAMAGE AT 65 INCHES BY 13 INCHES. ACFT FERRIED BACK TO DEPARTURE WHERE MX OBSERVED INNER ACOUSTIC LINER SEGMENT AT 12 O`CLOCK POSITION, MISSING. SUPPSDR CA090309007Seat · jammed(CAN) DURING CRUISE, THE CAPT`S SEAT BECAME JAMMED IN THE FULL FWD POSITION (THEY HAD DIFFICULTY WITH THE MOTOR, AND THERE WAS NO ELECTRICAL REVERSE). A PHONE PATCH WAS ESTABLISHED WITH MX CONTROL. THE FIRE AXE WAS USED TO DISLODGE THE SEAT AND THE FLIGHT CONTSDR CA090212001Spar · failedON TAXI OUT, R RUDDER TEST FAILED. RUDDER PEDAL APPEARS TO BIND. UNABLE TO ACHIEVE MORE THAN HALF DEFLECTION. INITIAL INSPECTION FOUND CTR PCA (LT HYD SYS) FULLY RETRACTED IN THE LT RUDDER DEFLECTION POSITION, WITH ONLY LT HYD SYS PRESSURIZED, RUDDER APPROX SDR CA090210011Duct · crackedDURING INSPECTION FOUND AC DUCT CRACK THE DAMAGE AIR CONDITIONING DUCT RUN’S FROM A TRIM AIR SUPPLY MODULATING VALVE (UNPRESSURIZE AREA) TO THE MIX MANIFOLD OUTLET DUCT (FWD CARGO PRESSURIZE AREA) THR : 60554 TCY : 9972 TLN : 9972.SDR CA090211002Duct · crackedDURING THE INSPECTION FOUND AC DUCT CRACK, THE DAMAGE AIR CONDITIONING DUCT RUN`S FROM A TRIM AIR SUPPLY MODULATING VALVE (UNPRESSURIZED AREA) TO THE MIX MANIFOLD OUTLET DUCT (FWD CARGO PRESSURIZE AREA).SDR HALA0800523Aileron · malfunctionedETOPS SIGNIFICANT SYSTEM ON CLIMB TO 320 W/AUTO PILOT ON BOTH (LT AND RT) INBD AILERON INDICES ON THE FLIGHT CONTROL STATUS DISPLAYS WERE 1/3 OF TOTAL SCALE ABOVE THE MEDIAN LINE. AT LEVEL, BOTH INDICES WENT TO 1/4 SCALE ABOVE MEDIAN. TURNING AUTO PILOT OFF SDR CA080222004Electrical Box · burned(CAN) WIRING DAMAGE FOUND IN FWD CARGO HANDLING ACCESS PANEL P35 DURING THE (XM) VISIT. 57 WIRES BURN, 3 WIRES MAJOR DAMAGED, 1 FOUND CUT, FOUND LUG DAMAGE ON TERMINAL A1,B1,C1 OF RELAY K245 (P35). FOUND WIRES DAMAGE ON CONNECTOR D5886P. AFTER AN INVESTIGATSDR CA070528010Unknown · malfunctioned(CAN) A FLIGHT ATTENDANT RECEIVED AN ELECTRIC SHOCK FROM THE WATER DISPENSER IN THE REAR GALLEY. COFFEE MAKERS REMOVED, GALLEY WIRING INSPECTED AND CONTINUITY CHECK CARRIED OUT (L-4355954). MORE IT TROUBLESHOOTING STEPS HAVE BEEN PROVIDED BUT NOT COMPLETED YSDR CA070328005Actuator · failed(CAN) SEAT LOCATION ON THE ACFT WAS 7F, AND FAILED IN FLIGHT. LEG REST ACTUATOR KEPT DRIVING THE FOOTREST BACKWARD, AND PUNCTURED THE REAR SPAR OF THE SEAT. THERE IS A CONCERN THAT ECU SOFTWARE 2.8 MAY BE TO BLAME, BUT INVESTIGATION IS ON GOING. THERE HAS BEENSDR CA060825001Wire · chafed(CAN) LT ELECTRIC HYDRAULIC PUMP PRESSUE SWITCH S27 WIRING FOUND CHAFED 6 INCHES FROM CONNECTOR D56, WIRING TEMPORARILY REPAIRED IAW AMM FAULT WAS INTERMITTENT AND 4 S27 PRESSURE SWITCHS HAD BEEN REPLACED OVER THE LAST FEW MONTHS. (TC NR 20060825001)SDR CA050517001Lock · melted(CAN) FAULT: ELECTRICAL BURNING SMELL NOTED AROUND VCR IN FORWARD GALLEY, LAVATORY AND OVERHEAD AREA. RETURNED. ACTION: BURNED ELEC SMELL LOCATED AS COMING FROM COCKPIT DOOR LOCK SOLENOID. SOLENOID AND HARDWARE REMOVED AND PLACED IN PLASTIC BAG IN OPB. AREA SDR CA050516001Tire · failedFOUND NR 1 MAIN WHEEL RECAP, 3/4 THICK, MISSING. TIRE PRESS STILL 220PSI. NR 1 MAIN WHEEL CHANGED AS PER MM32-45-01.SDR CA041129007Fuel Heater · failed(CAN) MIDWAY THROUGH THE FLT, THE LT ENG OIL QTY BEGAN TO DECREASE AT THE RATE OF APPROX 1 LITRE EVERY 10 -15 MINUTES. LT ENG THRUST REDUCED OIL QTY STILL DECREASED TO ZERO OIL PRESS AND TEMP REMAINED NORMAL ACTION: REPLACED SERVO FUEL HEATER IAW MM 73-11-09.SDR CA041123006Pump · contaminated(CAN) UNABLE TO START NR 2 ENG. DUE FUEL VALVE LT AT PEDESTAL & EICAS MSG FOR 'R FUEL VALVE'. CHECKED 28VDC AT FUEL CUTOFF SW AND PWR AVAILABLE. REPLACED FUEL S/O VALVE SOLENOID, NO FIX. REPLACED HMU, NO FIX. REMOVED FUEL PUMP AND FOUND CONTAMINATED WITH MESDR CA040407001Engine · leaking(CAN) LT ENGINE SHUTDOWN, OIL IND LOW, FOUND OIL IN TAIL PIPES. REPORT TO FOLLOW.SDR CA040120001Windshield · broken(CAN) WHILE IN FLIGHT, R1 WINDSHIELD OUTER PANE SHATTERED. (FL370) R1 WINDOW REPLACED IAW AMM 56-11-01 REMOVED: UNI 56-10-0174 MPN: 141T4801-50 INSTALLED: UNI 56-10-0174 MPN: 141T4801-50SDR CA040113004Windshield · failed(CAN) WHILE IN FLT ENROUTE FROM YYZ TO TLV, R1 WINDSHIELD OUTER PANE SHATTERED. FLT CONTINUED WITHOUT FURTHER INCIDENT. MTCE POOLED A WINDOW AND CHANGED.SDR CA031028001Rod End · unsafetied(CAN) RT ELEVATOR LOST MOTION DEVICE TO ELEVATOR CONTROL ROD END AT LOST MOTION DEVICE NOT IN SAFETY. ROUTINE INSPECTION DURING A M01 CHECK FOUND THE ROD END WAS NOT IN SAFETY. LOCKWIRE COULD BE INSERTED THROUGH THE INSPECTION HOLE. THE WITNESS SEAL FROM THE SDR CA031027002Panel · missing(CAN) RT HORIZONTAL STABILIZER LOWER TRAILING EDGE ACCESS PANELS AFT SUPPORT BEAMS MISSING 7 HORIZONTAL ATTACH BOLTS BASED ON THE CONDITION OF THE AREA IN WHICH THE DISCREPANCIES WERE FOUND AND THEFACT THAT THE ACFT WAS ON A M01 CHECK INDICATES THAT THE ACFT WSDR CA031002004Pump · failed(CAN) A/C WAS ENROUTE FROM YYZ TO FCO AND WHILE OVER YQB HAD A NR 1 ENG LOW OIL PRESSURE WARNING. CREW SHUTDOWN NR 1 ENG AND DIVERTED TO YUL. APPEARS TO BE MAIN OIL PUMP FAILURE. METAL HAS BEEN FOUND IN GEARBOX. ENGINE CHANGE UNDERWAY.SDR CA031003002Bushing · loose(CAN) ROLLING AILERON BEYOND 3 UNITS ON CONTROL COLUMN BINDING FELT. WHEEL VERY SLOW TO RETURN TO NORMAL. NOT AS STIFF WITH INPUT TO THE LEFT. WHEEL WOULD NOT RETURN TO NEUTRAL ON ITS OWN. FOUND INBOARD DROOP QUADRANT SIEZED. (CROSS SHAFT) ON INSPECTION OFSDR CA030528013Slide · deployed(CAN) LT O/H WING CHUTE WAS ACCIDENTALLY DEPLOYED BY FLT OPS DURING A TRAINING SESSION. THE CHUTE DID NOT DEPLOY COMPLETELY. THE LOWER SECTION OF THE CHUTE WAS PREVENTED FROM COMPLETE DEPLOYMENT BY THE IB SIDE. CONFIRMED, OPERATOR NEVER CHANGED OR REMOVED THISDR CA030205002Compressor · stalled(CAN) DURING FLIGHT YYZ/LHR, ACFT DIVERTED TO YUL, DUE TO LT. ENGINE COMPRESSOR STALL. ENGINE SHUT DOWN. RESTARTED BUT HIGH VIBRATION, AND RISING EGT. SO ENGINE SHUT DOWN AGAIN.ACFT REMOVED FROM SERVICE TO CARRY OUT BOROSCOPE AND INVESTIGATION.SDR CA030115001Alternator · broken(CAN) ORIGINAL WRITE UP STATED, LT ENGINE OIL QUANTITY SLOWLY DROPPED TO ZERO DURING CRUISE. OIL TEMP STEADY AT 3 DEGREES ABOVE RT ENGINE. OIL PRESSURE FLUCTUATED AT 2-10 PSI BELOW RT ENGINE. LT ENGINE EICAS MESSAGE SHOWING. AIRCRAFT PROCEEDED TO YVR WITH LT ESDR CA021015001Control Valve · malfunctioned(CAN) ON DESCENT INTO YYZ (15000) A STRONG ODOR WAS NOTED AND REPORTED THROUGHOUT THE AIRCRAFT. ODOR WAS NAUSEOUS AND DISSIPATED AFTER RECIRCULATION FAN TURNED ON. DURING INSPECTION OF AIRCRAFT FOUND THE LT PACK TEMP CONTROL VALVE MOTOR RUNNING CONSTANTLY TO SDR CA020906004Compressor · damaged(CAN) AFTER LANDING, SPARKS NOTICED COMING OUT BY LT ENGINE TAIL PIPE. ALL PARAMETERS NORMAL, METAL DEBRIS IN TAIL CONE. BOROSCOPE FOUND EXCESSIVE COMPRESSOR DAMAGE. ENGINE REPLACED.SDR CA020828003Control Unit · failed(CAN) CABIN CREW REPORTED 'PASSENGER READING LIGHT NOT WORKING IN Y CLASS.' THE 1ST OBSERVATION BY MAINT NOTED THAT IN CENTER SECTION OF AFT CABIN, ROWS 19DEF TO 36DEF, CALL LIGHT ILLUMINATED AT SEAT 36DEF, 26DEF & APPROXAMITELY ROW 20 OR 21DEF. CALL LIGSDR CA020502014Asymmetry Switch · failed(CAN) AT 400 FEET AFTER TAKEOFF CREW REPORTED AN AILERON LOCKOUT MESSAGE, RUDDER RATIO MESSAGE AND NONE OF THE 3 AUTOPILOTS COULD BE ENGAGED. AIRCRAFT RETURNED TO AIRPORT.BOTH LT AND RT STABILIZER TRIM/ELEVATOR ASYMMETRY MODULES (SAM) REPLACED AS PER AMM 27-09SDR CA020502013Thrust Reverser · contaminated(CAN) BOTH REVERSERS ONLY DEPLOYED AT MID TRAVEL ON LANDING.FOUND MOISTURE TRAP IN THE THRUST REVERSERS CDU (CONTROL AND DRIVE UNIT). REMOVED ALL MOISTURE, FUNCTIONAL TEST CARRIED OUT, AIRCRAFT FOUND SERVICEABLE.SDR CA020315008Windshield · failed(CAN) FIRST OFFICER WINDSHIELD SHATTERED IN FLIGHT, AIRCRAFT RETURNED TO HEATHROW. REPLACED WINDSHIELD AND HEAT CONTROLLER.SDR CA020124006Filter · failed(CAN) FLIGHT CREW REPORT THAT THEY HAD A FUEL FILTER LIGHT ON EICAS FOR BOTH ENGINES. FOUND TO BE FINE MANUFACTURING DEBRIS (NEW AIRCRAFT). REPLACED TWO FILTERS AND DRAIN ALL RESERVOIRS, GROUND RUN AND LEAK CHECK CARRIED OUT. FLEET MANAGEMENT REQUEST TO HAVE BSDR CA011019009Engine · failed(CAN) DURING INITIAL CLIMB ON GEAR RETRACTION LEFT ENGINE HAD A RECOVERABLE SURGE. (MOMENTARY WITH LOUD BANG) WITH NO VARIANCE IN ENGINE PARAMETERS. FLIGHT DATA RECORDER READ OUT PERFORMED REVEALING ENGINE SUSTAINED A CATEGORY LEVEL 3 SURGE. LT ENGINE REPLASDR CA010814003Indicator · leaking(CAN) ENROUTE FROM TEL AVIV TO TORONTO AFTER THE LT SYSTEM WAS TOPPED OFF (IN TLV) LOSS OF HYDRAULIC FLUID OF THE L/H SYSTEM, THE A/C RE-ROUTED AND ASK FOR AN EMERGENCY LANDING. A/C LANDED SAFELY WITHOUT FURTHER INCIDENT. FOUND TO BE A LEAK AT THE DIFFERENTIALSDR CA010308004Bolt · sheared(CAN) ONE BOLT FOUND SHEARED ATTACHING WHEEL HUN HALVES OF NR 3 MAIN WHEEL TIRE ASSEMBLE. MAIN WHEEL TIRE ASSEMBLE REPLACED AS PER MAINTENANCE MANUAL TASK 32-45-08-400.SDR CA001212013Fcu · failed(CAN) ON APPROACH AT SPEED 170K, SELECTED FLAPS FROM 20 TO 25, FLAPS STOPPED AT 23 DEGREES, CAUTION LIGHT TRAILING EDGE FLAP DISAGREE. GO AROUND CARRIED OUT. CHANGED FLAP SLAT ELECTRONIC CONTROL UNIT (FSCU). OPERATION CHECK NORMAL.SDR CA001129033Inverter · failed(CAN) CREW REPORT OF BURNING SMELL/SMOKE IN COCKPIT, STANDBY POWER INVERTER MESSAGE CAME ON ENGINE INDICATING AND CREW ALERT SYSTEM.CIRCUIT BREAKER PULLED FOR STANDBY INVERTER AND BEGAN SMOKE EVACUATION PROCEDURE. WHEN SWITCHES TO NORMAL, SMELL RETURNED. AIRCRSDR CA001004021Control Unit · failed(CAN) UPON SELECTION OF FLAPS (25 FLAP) ICAS MESSAGE TE FLAP DISAGREE AND STATUS MESSAGE TE FLAP SHUTDOWN ILUMINATED. FLAP INDICATION SHOWED SLIGHTLY ASYMMETRY AT 23 DEGREES. CHENAGED FLAP SLAT ELECTRICAL UNIT (F.S.E.U.) AND TEST CARRIED OUT AS PER FAUALT ISOLSDR CA000621042Bolt · sheared(CAN) AFTER A/C ARRIVED AT GATE (YUL) MAINT FOUND ON WALK AROUND CHECK DAMAGE TO RT LOWER WING PANEL , RT LDG GEAR DRAG STRUT, & RIGHT LDG GEAR STRUT DOOR. HEAD OF BOLT ATTACHING RIGHT STRUT DOOR TO LANDING GEAR STRUT FOUND SHEARED OFF. STRUT DOOR THEN ALLOWEDSDR CA000621037Valve · failed(CAN) DURING TAXI, AIRCRAFT STOPPED RESPONDING TO RIGHT STEERING TILLER OR RIGHT RUDDER PEDAL INPUTS. STEERING WOULD ONLY RESPOND TO CENTRE TO LEFT POSITIONS. AIRCRAFT RETURNED TO GATE. NOSE WHEEL STEERING METERING VALVE MODULE REPLACED AND SYSTEM CHECKED SERVSDR CA000530072Switch · burned(CAN) CENTER HYD PUMP FAILED IN CRUISE ELECTRICAL BURN SMELL IN COCKPIT, SMOKE EVIDENT, PUMP SHUT OFF, SMOKE DISSIPATED. SWAPPED C1 AND C2 DELAY MODULE AND CHANGED C1 LIGHT SWITCH. ON CLIMB THERE WAS A BURNING SMELL, C1 HYD SYSTEM SHUT DOWN A/C DIVERTED. FOUNDSDR CA000501029Spar · damaged(CAN) NO TEXTSDR CA000410024Bolt · loose(CAN) RUDDER LOWER POWER CONTROL ACTUATOR INPUT CRANK LH PIVOT BOLT LOOSE AND NUT BACKED OFF. LOOSE BOLT ALSO FOUND FOULING ADJACENT CRANK LH LUG. NUT STILL HAD SELF LOCKING ABILITY. NEW BOLT, BUSHING, NUT AND WASHER INSTALLED.SDR CA000328017Wire · damaged(CAN) EICAS CREW ALERT SYS MESSAGE FOR THE RT ENGINE SHUT OFF VALVE INOPERATIVE. REPLACED WIRING.
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