Boeing 767-324
Service difficulty reports · 1,299
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 = '767324' 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 = '767324' 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 NOCA03906Lamp · inoperativeEMERGENCY LIGHT AT SEAT 19AB INOP.SDR NOCA03806Lamp · inoperativeEMERGENCY LIGHT AT SEAT 11GH INOP.SDR NOCA03706Lamp · inoperativeEMERGENCY LIGHT AT SEAT 9GH INOP.SDR NOCA03606Lamp · inoperativeL1 DOOR EMERGENCY LIGHT INOP.SDR NOCA02406Fuel Filter · dirtyLEFT ENGINE FUEL FILTER EICAS MESSAGE INFLIGHT. AIRCRAFT DIVERTED TO SID, 180 ETOPS DIVERSION.SDR NOCA02006Battery Pack · inoperativeEMERGENCY PATH LIGHTS ROWS 9 THROUGH 27 INOP. CHANGED 2 BATTERY PACKS/CHARGERS PER AMM 33-51-07, OPS OK.SDR NOCA0806Control Panel · malfunctionedEMERGENCY LIGHT DEACTIVATED A ROW 12G DUE TO ISLE SIDE PANEL REMOVED FOR EVALUATION.SDR NOCA0306Slide · misinstalledLT SLIDE ASSEMBLY BOTTOM ATTACH POINTS NOT SECURED DUE TO IMPROPER INSTALLATION, SLIDE REPLACED.SDR NOCA0106Slide · misinstalledL4 DOOR SLIDE DEPLOYED. ON INSPECTION FOUND SLIDE FELL OUT OF BUSTLE AND INFLATED. SLIDE WAS REPLACED FAILURE DUE TO IMPROPER INSTALLATION.SDR NOCA3005Rod End · brokenAIR TURNBACK FOUND NOSE GEAR DOOR LT AFT DOOR SUPPORT ROD BROKEN AT DOOR TO STRUT ATTACH POINT.SDR DL76G050765Cdu · inoperativeIR - RT CDU WENT BLANK EN ROUTE RESET WITH CB NO FIX. CDU LEFT NO FIX. CDU RT SELECT ON F/O SIDE GOT V TRACK FLAG. FOUND RT CDU COOLING SCREEN CLOGGED CAUSING O/HEAT. REPLACED RT FMS CDU PER MM. CKS OK.SDR NOCA2605Light · inoperativeROUTINE MAINTENANCE FOUND 1L EMERGENCY PATH ARROW LIGHT INOP.SDR DL76G050702Window · malfunctionedPILOTS WINDOW CAME OPEN ON T/O ROLL AFTER PASSING 80 KTS. PRIOR TO T/O HANDLE WAS VERIFIED IN LOCKED POSITION. ABORTED T/O ROLL AT 100 KTS. MTC VERIFIED OPERATION AND LOCKING MECHANISM WORKS OK. PERFORMED HIGH ENERGY STOP INSPECTION. ALL NORMAL.SDR DL76G050681Relay · inoperativeWHILE PERFORMING ETOPS PRE-DEPARTURE CHECK, NR 1 AND NR 2 LT AND RT OVERWING ESCAPE SLIDE SQUIB TEST LIGHTS WOULD NOT ILLUMINATE. REPLACED K-839 RELAY, SYSTEM TEST CHECKS OK.SDR NOCA2205Bulb · inoperativeEMERGENCY AISLE LIGHTS AT SEATS 12B, 12H, 14B, 15B, 23H AND 34B HALF LIT. RELAMPED EMERGENCY AISLE LIGHTS AT SEATS 12B, 12H, 14B, 15B, 23H AND 34B OPS CHECK NORMAL.SDR NOCA1705Track · damagedCAPTAINS SLIDING WINDOW OPENED ON ROTATION OUT OF JFK. CREW UNABLE TO CLOSE WINDOW IN FLIGHT. DUMPED FUEL AND RETURNED SAFELY TO JFK. REPLACED CAPTAINS SLIDING WINDOW AND LOWER TRACK, WINDOW OPERATES NORMALLY. IT COULD NOT BE DETERMINED IF WINDOW WAS LOCKESDR NOCA1205Idg · disengagedAT START OF TAKEOFF ROLL, LEFT GENERATOR DROPPED OFF LINE, "L IDG" EICAS MESSAGE. IDG SERVICED, ENGINE HIGH POWER RUN, ALL INDICATIONS NORMAL.SDR DL76G050511Module · malfunctionedRUDDER RATIO LIGHT AND MSG CAME ON DURING TAXI OUT. UNABLE TO RESET, RETURNED TO GATE. FOUND LEFT RUDDER RATIO MODULE FAULTED. RESET SAME, PERFORMED RUDDER RATIO TEST, CHECKS GODD. OK FOR SERVICE.SDR NOCA0905Lamp · inoperativeBOTH LIGHTS IN EMERGENCY LIGHT FIXTURE OVER RT SIDE FLAP ARE INOP. REPLACED BOTH LAMPS IN EMERGENCY LIGHT FIXTURE OVER RT WING FLAP. ONE LIGHT IN EMERGENCY LIGHT FIXTURE OVER RT WING BEHIND R3 DOOR IS OUT. REPLACE LAMP IN EMERGENCY LIGHT FIXTURE OVER RT WINSDR DL76G050376Battery Pack · dischargedON SQUIB TEST FOUND LEFT SIDE AND RT SPOILER WILL NOT TEST. REPLACED BATTERIES M962 AND M961 OFF WING BATTERY PACKS. OPS CKD NORMAL.SDR NOCA1005Battery Pack · inoperativeEMERGENCY LIGHTS OUT AT ROWS 18 HG THROUGH 27 HG. TROUBLESHOOT AND REPLACED BATTERY PACK AT SEAT 19HG, OPERATION CHECK NORMAL. EMERGENCY LIGHTS OUT AT L2 EXIT DOOR. TROUBLESHOOT AND REPLACED BATTERY PACK AT L2 JUMP SEAT OPERATION CHECK NORMAL.SDR NOCA0505Connector · looseJFK - DOOR OVERHEAD EXIT SIGN LIGHT INOP. SECURED LOOSE CONNECTOR OPS NORMAL. EMERGENCY LIGHT BEHIND SEAT 36AB FOUND LOOSE CONNECTION. R4 EMERGENCY LIGHT INOP CLEANED CONTACT OPS CHECKED NORMAL.SDR NOCA0105Fuse · blownDURING ROUTINE MAINTENANCE (DAILY CHECK), CABIN EMERGENCY ESCAPE PATH LIGHTING SYSTEMS LOCATIONS 11AB THROUGH 27AB FAILED TO ILLUMINATE DURING TEST. TROUBLESHOT AND FOUND BAD FUSE AT BATTERY POWER SUPPLY. REPLACED FUSE AT POWER SUPPLY. SYSTEM OPERATIONAL CHSDR DL76G050100Engine · damagedBORESCOPE NR 2 ENG BOOSTER (LPC) AND HPC PER AMM TASK 72-00-00-206-H00 DUE TO PARAMETER SHIFT ON ENG. TREND AND RECENT FAN BLADE REPLACEMENT FOR IMPACT. ENGINE FAILED BOROSCOPE INSPECTION. REPLACED ENGINE.SDR DL76G050046Wire Harness · chafedF/A RECEIVING SHOCKS WHEN CONTACTING METAL DOOR IN FWD GALLEY NEAR COFFEEMAKERS. REPAIRED CHAFED GALLEY POWER WIRES.SDR DL76G050034Battery · dischargedP-61 SQUIB TEST PANEL WON`T TEST CORRECTLY. REPLACED TEST PANEL, 2 EMERGENCY BATTERIES (M961 &M962 ) & 1 CHARGER ASSY. OPS CHECKS GOOD.SDR DL76G040665Bottle · discharged1L DOOR SLIDE BOTTLE READING 0 PSI. REMOVED AND REPLACED 1L DOOR SLIDE PER AMM 25-66-01.SDR DL76G031149Battery · dischargedON PDC FOUND LEFT SLIDE AND RIGHT SPOILER SQUIBS NOT TESTING IN COCKPIT. REPLACED BATTERY PACK AT 22G, CHECKS NORMAL.SDR DL76G030606Tube · looseON DEPARTURE, RIGHT ENGINE OIL PRESSURE AND QTY WENT TO ZERO. FOUND SHROUD B-NUT ON NBR 6 BEARING SCAV SUPPLY TUBE LOOSE - SECURED SAME - LIMITS FOR LOSS OF OIL PSI NOT EXCEEDED IAW PIREP AND MTC OBSERVANCE - C/W REQD INSPN IAW AMM 72-00-00- LK AND OPS CK GDSDR DL76G030581Engine · failedON TAKEOFF ROLL, ABORTED AT 100 KTS DUE TO NR 2 ENG FAILURE. FLAMES REPORTED COMING FROM THE FRONT AND REAR OF THE ENG. ENG EXPERIENCED A COMPRESSOR STALL. ENGINE CHANGE IN WORK IN BOM.SDR DL76G030306Smoke Detector · will not testON L/O FOUND LT AFT LAV SMOKE DETECTOR WILL NOT TEST. REPLACED DETECTOR, CHECKS OK.SDR DL76G030119Power Supply · dischargedON PDC FOUND LEFT OVERWING SLIDE SQUIB NOT ILLUMINATING WITH TEST SWITCH 1. RT SPOILER SQUIB LIGHT WILL NOT ILLUMINATE WITH TEST SWITCH 2. INSTALLED NEW BATTERY POWER SUPPLY AND BATTERY M962. ALL SQUIB TESTS NOW OK.SDR DL76G020612Control Unit · malfunctionedIN CRUISE LOST LEFT SYMBOL GENERATOR FOLLOWED 5 MINS LATER BY RUDDER RATIO AND AILERON LOCKOUT EICAS MSGS AND LOSS OF ALL 3 AUTOPILOTS. FOUND LEFT SAM W/ FAULT BALL. WILL NOT RESET. CYCLED 1L AND 2LAC AND DC FLT CTL ELEC C/B'S. ALL FAULTS CLEARED. REPLACESDR DL76G020233Coffeemaker · malfunctionedDURING CRUISE A BURNING ELECTRICAL SMELL IN FORWARD GALLEY FAULT TRACED TO NUMBER 1 COFFEEMAKER. REMOVED SAME, CB PULLED AND COLLARED NIS LGW FWD TO MCO AND PLACARD PER MEL. CB PULL FOR COFFEEMAKER 2 AS PRECAUTION.SDR DL76G011221Cdu · failedCAPTS FMC CDU WENT BLANK. REPLACED CDU. FMS OPS CHECKS OK.SDR DL76G001164Skin · puncturedTHE FUSELAGE SKIN WAS TORN AND DENTED FROM CONTACT WITH GROUND EQUIPMENT AT STRINGER 23R BETWEEN FS 654+22 & FS 654+44. THE DAMAGED SECTION OF STRINGER WAS REMOVED AND SPLICED PER THE B767 SRM. THE DAMAGE TO THE SKIN WAS REMOVED WITH A 9.8 X 1.2 CUTOUT AND ASDR DL76G992468Oven · malfunctionedGALLEY MID CABIN CENTER OVEN OVERHEATS, TOP WILL NOT SHUT OFF. REPLACED OVEN, SYSTEM CHECKS NORMAL.SDR DL76G992338Air Dist · odorELECT ODOR IN FWD CAB AND AFTER CAPTS SIG GEN WENT OUT, OUTSIDE ELECTRICAL ACTIVITY WAS HIGH. AFTER SHUTTING OFF UTIL BUSSES THE ODOR WENT AWAY IMMEDIATELY. LATER INFLIGHT ALL GALLEY C/BS PULLED AND RT UTILITY BUS TURNED ON WITH RECIRC FANS OFF. NO FUMES RESDR AU990868Shaft · broken(AUS) THRUST REVERSER LEFT UPPER INBOARD FLEXSHAFT LOCATED BETWEEN THE ELECTRO MECHANICAL BRAKE AND THE UPPER ANGLE GEARBOX BROKEN.SDR DL76G991367Fan · failedSTRONG ELECTRICAL SMELL AROUND SEATS 35-37 F/G. FOUND AFT EQ EXHAUST FAN 1 EMITTING ELECTRICAL ODOR, REPLACED FAN.SDR DL76G991130Valve · leakingON TAXI OUT, FOUND FUEL LEAKING ON RT WING. FOUND SURGE BOX RELIEF VALVE LEAKING. RESEATED, LEAK CHECKS NORMAL.SDR DL76G990834Overheat Loop · malfunctionedAT FL330, LEFT ENGINE OVHT LIGHT ON PEDESTAL. RETARDED ENG TO IDLE, LIGHT REMAINED ON FOR APPROX 3 MINUTES. NO ASSOCIATED MASTER CAUTION OR EICAS MESSAGE. REPLACED OVHT DET LOOP M684 AND LOGIC TEST CARD. ALSO, CHECKED ALL CLAMPS ON ENGINE AND TIGHTENED SAMSDR DL76G990741Logic Card · malfunctionedLEFT ENGINE OVERHEAT LIGHT PASSING 10,000 FT, LIGHT EXTINGUISHED WHEN POWER REDUCED. INSPECTED OVERHEAT LOOP AT LEFT ENGINE, CHECKS OK. MOTORED ENGINE, INSPECTED FOR AIR LEAKS AT LOOP AREA, NO LEAKS. REPLACED LOGIC TEST CARD M10224. RAN ENGINE AT T/O POWERSDR DL76G990041Terminal · brokenSTATUS MSG LEFT ENGINE FIRE LOOP 1 AND FIRE LOOP 2 AND NO LEFT ENGINE FIRE TEST. FOUND TERMINALS BROKEN AT WIRES W5340-9001 AND 9002R ON LWR FWD LOOP. INSTALLED TEMPORARY TERMINAL AND MTC FERRIED A/C FOR PERM REPAIR.SDR AU981605Nut · loose(AUS) OUTBOARD FLAP SUPPORT BEAM ATTACH BOLT NUTS (AFT TWO) ON THE RT OUTBOARD INBOARD BEAM FAILED TORQUE THRESHOLD TEST. ALL SIX BOLTS, NUTS AND WASHERS ATTACHING THE FLAP TO THE SUPPORT BEAM WERE REPLACED PER BOEING ALERT SB 767-27A0151 AND AMM27-51-20. FOSDR AU981482Pin · damaged(AUS) NR 6 BRAKE HOUSING ANTI-ROTATION PIN HAD A SMALL AREA OF CHROME PLATING MISSING. AREA OF PLATING MISSING WAS APPROXIMATELY 12.7 MM BY 12.7 MM (0.5 INCH BY 0.5 INCH).SDR AU981489Cvr · malfunctioned(AUS) COCKPIT VOICE RECORDER INOPERATIVE. WORKSHOP INSPECTION FOUND THE FOLLOWING DEFECTS: 1. TAPE STALLED AT CAPSTAN. 2. TAPE WORN. 3. TAPE GUIDE ROLLER WORN AND BEARINGS CONTAMINATED. 4. DRIVE BELT SLIPPING. 5. DESK ASSEMBLY CONTAMINATED. 6. EXCSDR AU981105Valve · sticking(AUS) EQUIPMENT COOLING OVERRIDE/SMOKE CLEARANCE VALVE STUCK IN THE CLOSED POSITION. PART TC: 8,350.SDR AU981098Fire Detector · faulty(AUS) LT ENGINE FIRE DETECTION SYSTEM FAULTY DUE TO DECREASED INSULATION RESISTANCE BETWEEN ACTIVE ELEMENTS WITHIN THE DETECTOR CAUSED BY MIGRATION OF METAL PARTICLES FROM THE SENSOR CORE. PART TC:4,199.
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