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 2004UALA01020Floorbeam · crackedNOSE COMPARTMENT AT STATION 247 APPROXIMATELY AT RBL 77 FLOORBEAM P-N 141T5104-7 WAS FOUND CRACKED AT WL 195.50.SDR 2004UALA01023Computer · failedRIGHT FMC CDU FAILED. RIGHT CDU WAS REPLACED. SHOP COULD NOT DUPLICATE CDU BLANKING DURING HOT, COLD AND VIBRATION OPERATION ON BENCH. AS A PRECAUTION, SHOP REPLACED COMPONENTS A6A2Q7, A6A2Q8, A6A2U16, A2A2U45, A2A2U48 IN CDU. THE CDU (MR40219-185) WAS REMSDR 2004UALA01006Switch · out of rigDIVERTED TO JFK DUE TO LEADING EDGE FLAP INDICATION PROBLEM. FOUND NR 9 LE SLAT SWITCH S303 OUT OF RIG. SHIMMED SWITCH TO ACHIEVE PROPER SWITCH TARGET GAP.SDR 2004UALA01005Battery Pack · dischargedPOSITION 1 EMERGENGY ESCAPE SLIDE SQUIB LIGHT FAILED TO ILLUMINATE DURING TEST. DEFECT CAUSED BY LOW BATTERY. REPLACED LEFT HAND BATTERY PACK.SDR 2004UALA00997Battery · dischargedRIGHT OVERWING SLIDE SQUIB DOES NOT TEST IN POSITION 1. DEFECT CAUSED BY LOW BATTERY. REPLACED RIGHT HAND BATTERY.SDR 2004UALA01009Angle · crackedIN E/E COMPARTMENT, CRACK ON UPPER ANGLE OF STATION 246 FLOORBEAM, LBL 10, AFT SIDE. SUBJECT OF OEM SERVICE BULLETIN AND INCORPORATED INTO ROUTINE INSPECTION PROGRAM.SDR 2004UALA00998Wire · burnedFOUND WIRES W298-021-08, W1046-913-08, W1046 -012-10, W1046-028-12. BURNED AT TB 5132 TERMINAL BLOCK INSIDE P37. REPLACED TERMINAL STRIP TB5132 IN P37 PANEL.SDR 2004UALA00999Support Angle · crackedE/E COMPARTMENT CRACK IN SUPPORT ANGLE STATION 246 FLOORBEAM AT RBL 5. MAJOR REPAIR ACCOMPLISHED. CRACK DUE TO BODY FLEXING/LOADING. CRACKED ANGLE WAS REPLACED.SDR 2004UALA00974Brake · smokeHEAVY SMOKE COMING FROM 4F MAIN TIRE WHEN TAXIING INTO GATE. BRAKE MR 32357 DASH 2181 REPLACED. 4F TIRE REPLACED. 3F TIRE REPLACED AS MATE. CLEANED INSIDE 4F AXLE AND FOUND PAINT DISCOLORATION. OUTSIDE OF AXLE FOUND NO DAMAGE TO CADMIUM PLATING. ACCOMPLISHEDSDR 2004UALA00983Compressor · stalledCOMPRESSOR STALL REPORTED ON NR 1 ENGINE, ON CLIMB, ENGINE SELF RECOVERED AND CONTINUED NORMAL OPERATION.SDR 2004UALA00972Warning Light · illuminatedAFT CARGO DOOR EICAS MESSAGE. TRIED 4 TIMES, UNABLE TO DUPLICATE FAULT ON GROUND.SDR 2004UALA00967Fitting · crackedRIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE FITTING INBOARD AND OUTBOARD FLANGES ARE CRACKED.SDR 2004UALA00943Floorbeam · crackedFLIGHT DECK FLOORBEAM AT STA 246 FORWARD FACE STIFFENER CRACKED LOWER CORNER AT LBL 25. BOEING SERVICE BULLETIN RECOMMENDED ROUTINE INSPECTION IN PLACE TO MONITOR THIS CRACKING OF STA 246 FLOORBEAM. CRACKING OCCURS DUE TO HIGHER THAN INITIALLY ANTICIPATED LOSDR 2004UALA00962Engine · surgesNR 2 ENG SILENT SURGE FLAGGED BY AIRCRAFT. THIS EVENT WAS A SILENT SURGE THAT WAS REPORTED BY THE ENGINEER WHO MONITORS THE ECM. THE EPR WAS BELOW 1.25. THE AIRCRAFT AND FLIGHT CREW DID NOT REPORT THIS EVENT. SURGE CHECKS WERE ACCOMPLISHED ON THE ENGINE WITH SDR 2004UALA00960Light · inoperativeEEL LIGHTS INOP BY ROWS 15AB THRU 19AB. REPLACED POWER STRIP.SDR 2004UALA00939Hydraulic System · leakingFLIGHT DIVERTED DUE TO RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. REPLACED RIGHT SYSTEM EDP. NO FURTHER REPORTS NEXT 20 AC CYCLES.SDR 2004UALA00925Hinge Fitting · crackedLT WING IB FLAP OB HINGE FITTING CRACKED AFT VANE. SUPPLEMENTAL DATA UPDATE REPAIRED FITTING WITH ANGLE AND FILLER REPAIR.SDR 2004UALA00924Floorbeam · crackedFLOORBEAM STA 246 STIFFENER AT APPROX RBL 20 IS CRACKED. CRACK CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED & INSTALLED NEW STIFFENER.SDR 2004UALA00926Idg · vibrationDIVERTED WHEN LEFT ENGINE INDICATED IDLE FUEL FLOW AND IDLE THRUST. SHOP FOUND LOG PISTON FAILURE ON REMOVED LT IDG. CORRESPONDENCE BETWEEN COMPONENTS ENGINEERING, POWER PLANT ENGINEERING, SUNDSTRAND, AND PWA, INDICATES THERE IS A POTENTIAL ANOMALY FOR A WORSDR 2004UALA00921Floorbeam · crackedFLOORBEAM STA 246 STIFFENER AT RBL 15 IS CRACKED. CRACKS CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED AND INSTALLED NEW BRACKET.SDR 2004UALA00907Apu · inoperativeRETURNED TO THE FIELD WHEN THE LT GENERATOR WENT OFF LINE AND THE APU WOULD NOT START. APU START SWITCH AND APU ELECTRONIC CONTROL UNIT WERE REPLACED PREVIOUSLY DUE TO APU ALTITUDE STARTING PROBLEMS. THE ECU TESTED WITHIN LIMITS. APU START SWITCH WAS NOT ROSDR 2004UALA00894Check Valve · failedNR 2 ENGINE COMPRESSOR STALL. REPLACED ENGINE DUE TO UNABLE TO ROTATE. UPON SHOP TEARDOWN OF ENGINE, ROOT CAUSE OF THE SURGE WAS DETERMINED TO BE CATASTROPHIC FAILURE OF THE PNEUMATIC 8TH STAGE CHECK VALVE.SDR 2004UALA00911Hinge · crackedRIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE WITH REPAIR ANGLES AND FILLER.SDR 2004UALA00912Seat Track · crackedMAIN CABIN SEAT TRACK LBL 88 AT BS 747.5 TO 808 BROKEN, CRACKED AND CORRODED. DAMAGED SEAT TRACK REPLACED.SDR 2004UALA00914Hinge · crackedLEFT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE WITH REPAIR ANGLES.SDR 2004UALA00913Spar · crackedNR 2 NACELLE UPPER SPAR WEB IS CRACKED SEVERAL PLACES AS SEEN THROUGH ACCESS 446BL. REPAIRED UPPER SPAR WEB WITH DOUBLER AND FILLER JUST FWD OF PYLON AFT BLKHD PER SRM 54-53-01, FIG 208. PER SB 767-54-0092 R1 PROBABLE CAUSE OF CRACKING IS FLEXING OF PYLON MISDR 2004UALA00851Apu · malfunctionedRETURNED TO HNL DUE TO FAILED EN ROUTE ETOPS VERIFICATION, APU ALTITUDE START. SUPPLEMENTAL DATA UPDATE, THE CAUSE OF THE FAILED ALTITUDE START WAS NOT CONFIRMED. TEST CELL FINDINGS COULD NOT REPEAT NO START EVENT. THE FOLLOWING LRU WERE ROUTED-GENERATOR OISDR 2004UALA00850Warning System · activatedLEADING EDGE SLAT ASYMMETRY EICAS DISPLAYED. ACCOMPLISHED APPROPRIATE FAULT ISOLATION MANUAL, AND AIRCRAFT MAINTENANCE MANUAL PROCEDURES. BITE TESTED THE FSEU, AND PSEU, INSPECTED ALL TARGETS. OPERATED THE FLAPS ELECTRICALLY AND HYDRAULICALLY. NO FAULTS FOSDR 2004UALA00910Support Fitting · crackedRIGHT WING INBOARD MAIN FLAP REAR SIDE LINKAGE SUPPORT FITTING CRACKED, INBOARD AND OUTBOARD SIDES. MAJOR REPAIR ACCOMPLISHED. REPAIRED & INSTALLED SUPPORT FITTING.SDR 2004UALA00908Seat Track · crackedMID CABIN SEAT TRACK AT STA 725 AND STA 759, APPROX LBL 90, AFT END CRACKED. *S/D* DAMAGED SEAT TRACKS WERE REPLACED.SDR 2004UALA00909Arm · crackedLT IB AFT FLAP, IB HINGE ARM CRACKED BOTH SIDES AT ATTACH POINT TO MAIN FLAP. REPAIRED & INSTALLED FITTING.SDR 2004UALA00845Battery Pack · failedNR 1 RT WING SLIDE SQUIB FAILS TO TEST. REPLACED BOTH LEFT AND RIGHT BATTERY PACKS AND RIGHT ESCAPE SYSTEM RELAY ASSY M1136. SYSTEM TEST 1 AND 2 CHECK NORMAL.SDR 2004UALA00841Control Unit · malfunctionedELECTRICAL UTILITY BUSS PROBLEM. LT AND RT UTILITY BUSS TRIPPED ABOUT 20 MINUTES OUT. UNABLE TO RESET AND THE AIRCRAFT RETURNED TO IAD. RELAYS K148 (SYS 1 AIR/GND) AND K10109 (UTIL/GALLEY PWR FLT RESET) WERE REPLACED AS A PRECAUTION. M116 BUSS POWER CONTROSDR 2004UALA00915Seat Track · crackedCABIN SEAT TRACK STA 755, AND RBL 85 CRACKED. DAMAGED SEAT TRACK REPLACED.SDR 2004UALA00808Outflow Valve · failedFLIGHT RETURNED TO FIELD WITH CABIN PRESSURE FAULTS. THE EQUIPMENT COOLING OVERBOARD EXHAUST VALVE FAILED. THE VALVE WAS NOT DEACTIVATED PER THE MEL CAUSING A LOSS OF CABIN PRESSURIZATION ON THE SUBSEQUENT FLIGHT. THE VALVE WAS RE-DEFERRED PER THE MEL AND REPLSDR 2004UALA00828Hinge · brokenLT WING, REAR SPAR, OUTBOARD FLAP OUTBOARD HINGE FITTING BROKEN IN HALF. FLAP TRANSMISSION OVER TORQUE LIMIT INDICATOR ALSO POPPED. SUPPLEMENTAL DATA UPDATE, REAR SPAR RIB POST PART NR 113T1369-1 REPLACED. FLAP TRANSMISSION OVERTORQUE LIMIT INDICATOR RESET.SDR 2004UALA00827Battery Pack · dischargedCENTER LT OVERWING EMERGENCY LIGHT HAS ONE INOP LAMP. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED BATTERY PACK M738 AND RELAMPED LT CENTER OVERWING LIGHT ASSEMBLY.SDR 2004UALA00826Battery Pack · dischargedDOOR 2L UPPER INTERIOR EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK M739.SDR 2004UALA00825Battery Pack · dischargedDOOR 2R UPPER INTERIOR EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK AT AFT RT ATTENDANTS SEAT.SDR 2004UALA00824Battery Pack · dischargedCABIN DOORS 2R AND 2L EXTERIOR EMERGENCY LIGHTS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK M734 IN RT AFT CABIN.SDR 2004UALA00810Hinge · crackedRT INBD AFT FLAP EXTERNAL HINGE IS CRACKED AT THE MID FLAP AFT SPAR. REPAIRED FITTING WITH ANGLE REPAIR.SDR 2004UALA00809Floorbeam · corrodedCABIN FLOORBEAM UPPER SURFACE CORRODED, STA 808-813, RBL 57. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SPLICE.SDR 2006UALA01154Latch · failedRIGHT OVERWING DOOR LATCH INTEGRATOR FAILS TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW 767 MM 25-65-98SDR 2006UALA01153Latch · wornLT O/W COMPT DOOR LATCH NR 3 PINHOLE EDGE MARGIN WORN BEYOND LIMITS, LATCH REPLACED.SDR 2004UALA00792Smoke · detectedRETURNED TO FIELD DUE TO SMOKE IN COCKPIT.SDR 2004UALA00791Smoke · detectedRETURNED TO FIELD DUE TO SMOKE IN COCKPIT.SDR 2004UALA00778Capacitor · failedRETURNED TO FIELD DUE TO SMOKE IN COCKPIT. FLT CREW REPORTED THAT CAPTAIN'S ELECTRONIC HORIZONTAL SITUATION INDICATOR (EHSI) WENT BLANK DURING THE INCIDENT. CAPTAIN'S EHSI WAS REPLACED. SHOP DETERMINED THAT THE REMOVED EHSI HAD A FAILED CAPACITOR C116 ON CASDR 2004UALA00775Squib · will not testRIGHT EMERGENCY ESCAPE SLIDE SQUIB WILL NOT TEST. REPLACED RIGHT ESCAPE SYSTEM RELAY ASSY M1136. SQUIB TESTS OK.SDR 2004UALA00767Pump · leakingLOST RIGHT HYDRAULIC SYSTEM EN ROUTE, CONTINUING TO DESTINATION. LOSS OF PRESSURE DUE TO FAILED NR 2 ENGINE DRIVEN PUMP. PUMP HAS INDICATION OF OVERHEAT CONDITION. NO ADDITIONAL DETAILS FROM OSV REPORTED.SDR 2004UALA00742Light · intermittentEEL LIGHT STRIP FLASH INTERMITTENTLY AT ONLY SEATS 21, 22, 23 LEFT SIDE (END). REPLACED LIGHT PACK UNDERNEATH SEAT 23 AB.
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