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 UIEA2016071400582Detector · faultyEICAS MSG FWD CARGO DET 1, TRANSFERRED TO MDDR 68348 IAW MEL 26-16-01-01-01, CAT C. REMOVED AND REPLACED FWD CARGO NR 1 DETECTOR IAW AMM 26-16-01. OPS CHECK OK.SDR UIEA2016071400581Warning Message · false activationLEFT PACK TEMP EICAS MESSAGE. PERFORMED PACK TEMPERATURE CONTROLLER BITE TEST. BITE TESTED OK, NO MESSAGE FOUND IAW AMM 21-61-12-715.SDR UIEA2016071100574Hose · leakingLEAKING RUBBER HOSE IN LEFT PACK BAY DISCOVERED DURING WALKAROUND. SECURED THE LINE AND RECONNECTED IAW AMM 21-51-03, NO LEAKS NOTED.SDR UIEA2016070700567Circuit Card · failedNR 2 ENGINE FIRE LOOP 2 MESSAGE EICAS. REPLACED NR 2 ENGINE LOOP 2 FIRE DETECTION PRINTED CIRCUIT CARD IAW AMM 26-10-01. CHECKED OK.SDR UIEA2016070700565Circuit Card · failedWHEN LEFT PACK TURNED OFF, NO PACK OFF LIGHT AND NO L PACK OFF EICAS MESSAGE. REPLACED LEFT PACK FLOW CONTROL PRINTED CIRCUIT CARD IAW AMM 21-51-09. OPS CHECKED GOOD.SDR UIEA2016070700566Shutoff Valve · malfunctionedSTATUS MESSAGE RT IDG VALVE. REPLACED IDG AIR OIL HEAT EXCHANGER AIR SHUTOFF VALVE IAW AMM 24 11-07 OPS AND LEAK CHECKED OK.SDR UIEA2016070400562Fluid · lowRIGHT IDG VALVE STATUS TROUBLESHOOTING, FIM 24-20, FT 802. NO DEFECT NOTED ADDED ONE PINT, OIL TO IDG OK FOR SERVICES.SDR UIEA2016070700570Circuit Card · failedLT ENGINE SPEED CARD EICAS MESSAGE DISPLAYED. REPLACED LT ENG N2 SPEED CARD IAW AMM 73-21-54. OPS CHECKED GOOD.SDR UIEA2016070200558Switch · defectiveDURING ENGINE START RT ENGINE VALVE LIGHT FAILED TO CYCLE LAMP TEST CONFIRMED THAT THE LIGHT WAS FUNCTIONING PROPERLY. PLACED ON DEFERRAL. REPLACED SW LIGHT IAW 33-13-00. OPS CK OK IAW 28-22-01. THIS CLEARS MEL.SDR UIEA2016062200453Status Message · false activationSTATUS MESSAGE, FORWARD CARGO DETECTOR 1 PERFORMED LOWER CARGO SMOKE DETECTION SYS BITE IAW FIM 26-16, FT 806. SYS CHECKS OK, EICAS MESSAGE CLEARED.SDR UIEA2016062300455Warning System · activatedFLIGHT DECK TEMP EICAS, IN FLIGHT DECK TEMP, INOPERATIVE LIGHT ILLUMINATED MANUAL CONTROL, WORKS OK. PERFORMED ZONE TEMP CONTROL BITE PROCEDURE IAW FIM 21-61.SDR UIEA2016062300457Control Valve · faultyINTERMITTENT LT PACK OFF, EICAS MESSAGE DURING DESCENT. TRANSFERRED TO MDDT 67731 IAW MEL 21-51-03-01, CAT C. REMOVED AND REPLACED LEFT ACM TEMP CONTROL VALVE AS PER AMM 21-51-12. OPS CHECK NORMAL.SDR UIEA2016062300458Status Message · false activationFUEL QTY TOTALIZER INOPERATIVE STATUS MESSAGE. QTY BITE IAW FIM 28-41 F/T 852, NO FAULTS AT THIS TIME.SDR UIEA2016061600427Switch · faultyLT PACK BITE MAINTENANCE MESSAGE. REPLACED ALTITUDE SWITCH IAW AMM 21-51-17, OPS CHECK NORMAL.SDR UIEA2016060300400Warning Light · illuminatedRIGHT ENGINE VALVE LIGHT DID NOT CYCLE DURING START.SDR UIEA2016060300397Structure · damagedNUMBER 7 LOWER INBD SLAT DAMAGED. TEMPORARY REPAIR ACCOMPLISHED IAW 767-3, SRM 57-43-01-1A-1. ALLOWABLE DAMAGE 1 NOTE P & DETAIL & PERMANENT REPAIR BEFORE 24 MONTHS OR AT THE NEXT STRUCTURES C CHECK.SDR UIEA2016060300399Indicator · inoperativeFORWARD COMPARTMENT TEMP READOUT INOPERATIVE.SDR UIEA2016060200395Light · inoperativePORTABLE EMERGENCY LIGHT IN FLIGHT DECK INOPERATIVE. R & R FLIGHT DECK PORTABLE EMERGENCY LIGHT IAW TASK 33-51-01-862-014.SDR UIEA2016060200384Inlet · corrodedNUMBER 2 ENG NOSE INLET COWLING, INTERIOR HAS A PATCH OF CORROSION INTERNALLY & INBD SIDE, ACOUSTIC PANEL, APPROX 8 O' CLOCK.. R & R NR 2 NOSE COWL IAW AMM 71-11-01-404-005-H00 REV118 22 APR 16.SDR UIEA2016060200385Precooler · crackedNR 2 ENG PNEUMATIC AIR SUPPLY PRECOOLER CRACKED ON WELDS & LEAKS AT WELDS UNDER PRESS. R & R 2 ENG PRECOOLER IAW AMM 36-11-15-404-020-001. OPERATIONS & LEAK CHECKS GOOD.SDR UIEA2016060200387Frame · crackedBS 883.5, RBL 89, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK AT RADIUS. ACCOMPLISHED SB 767-53A0209 PGS 108 - 117 FIG 10 REV 2. NO FURTHER ACTION REQUIRED.SDR UIEA2016060200388Frame · crackedBS 903.5, RBL 89, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK AT RADIUS. ACCOMPLISHED SB 767-53A0209 FIG 18 PAGE 181 - 189 REV 2 & ECRA N649GT-53-B767-002.SDR UIEA2016060200389Frame · crackedBS 859.5, LBL 89, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK IN RADIUS. ACCOMPLISHED SERVICE BULLETIN 767-53A0209 FIG 7 PAGES 80 - 88 REV 2 EO 5753A038.SDR UIEA2016060200390Frame · crackedBS 903.5, LBL 89, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK AT RADIUS. ACCOMPLISHED SERVICE BULLETIN 767-53A0209 PGS 172 - 180 FIG17 REV.2.SDR UIEA2016060200391Smoke Detector · no testAFT CARGO FIRE DETECTION FAIL TO GIVE WARNING DURING SMOKE TEST. CLEANED AFT CARGO FIRE DETECTOR TUBING IAW MM TASK 26-16-00-107-011, METHOD 1, STEP 3, F1-3F10.SDR UIEA2016060200392Relay · malfunctionedSTANDBY POWER SYS CHECK FAILED IF EITHER TB14FC3 IS JUMPERED TO GROUND. STBY BUSS OFF LIGHT DOES NOT COME ON OR IF P6J17 CB IS RESET. R & R STBY POWER RELAY K105 IAW AMM TASK 24-33-01-004-004 PAR 2 & TASK 24-33-01-404-005 PAR 3.SDR UIEA2016060200393Sensor · delaminatedFUEL LEVEL SENSOR IS DELAMINATING IN RT WING SURGE TANK. R & R RT WING FUEL LEVEL SENSOR UNIT IAW MM 28-21-03-004-008 PGS 1 - 3 & MM 28-21-03-404-004 PGS 1 - 3.SDR UIEA2016060200394Battery Pack · inoperativeLEFT A ZONE EMERGENCY LIGHTS INOPERATIVE FROM BULLNOSE AFT. R & R M735 BATTERY ASSEMBLY IAW AMM TASK 33-51-07-422-010 STEPS 5A TO 5D.SDR UIEA2016060200374Skin · corrodedRIGHT WING, LOWER SKIN AT REAR SPAR, WBL 708 HAS EXFOLIATION. CORROSION WAS REMOVED BY BLENDING TO A 0.111 INCH MINIMUM THICKNESS FROM ORIGINAL THICKNESS OF 0.193 INCHES. REWORKED AREA WAS SHOT PENNED, ALODINED & PRIMED. STAGE 1 STATIC STRENGTH APPROVAL REQSDR UIEA2016060200367Radar · malfunctionedWEATHER RADAR INOPERATIVE LT & RT POSITION. PERFORMED OPERATIONS TEST IAW AMM 34-43-00-715-001-001. SYS TESTS NORMAL ON MAS WO HM77-20004.SDR UIEA2016060200370Battery Pack · inoperativeLEFT OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R M736 BATTERY ASSEMBLY IAW AMM 33-51-07-422-012 STEPS 5A - 5D. ADJUSTED TARGET ON 5198 IAW 53-71.SDR UIEA2016060200371Battery Pack · inoperativeALL EXTERIOR EMERGENCY SLIDE LIGHTS & RT OVERWING LIGHTS FAILED ENDURANCE TEST. R & R THE BATTERY ASSEMBLIES.SDR UIEA2016060200372Power Supply · malfunctionedFOUR INTERNAL EMERGENCY LIGHTS NOT ILLUMINATING WHEN SYS TURNED ON. REMOVED EMERGENCY LIGHT POWER SUPPLY M739 IAW AMM 33-51-07-002-006. INSTALLED OVERHEAD EMERGECY LIGHT M739 IAW AMM 33-51-07-402-010.SDR UIEA2016060200373Skin · dentedFOUND DENT IN FUSELAGE AT 535 FWD OF BULK PIT DOOR. REPAIRED DENT ON FUSELAGE IAW SRM 53-00-01-2R-6 PAGES 2 - 4 FIG 201 SHEET 1 - 3.SDR UIEA2016060200375Skin · damagedBS 1197 + 78, BELOW STRINGER 18 HAS LIGHTNING STRIKE DAMAGE ON SKIN. REMOVED LIGHTNING STRIKE DAMAGE & INSTALLED A FLUSH SKIN REPAIR WITH INTERNAL DOUBLER IAW SRM 53-00-01-2R-6, ALODINE & PRIMED IAW SRM 51-10-2 PAGE 8.SDR CA160223005Fan · malfunctioned(CAN) IN PREPARATION FOR DEPARTURE IT WAS REPORTED BY GROOMERS THERE WAS A BURNING ODOR IN THE CABIN OF THE ACFT. MAINTENANCE WAS ADVISED AND INVESTIGATION RESULTED IN THE AFT GALLEY EQUIPMENT FAN MALFUNCTIONING AND AN MEL WAS APPLIED. FLIGHT WAS DELAYED APPRSDR CA151208001Control Module · leaking(CAN) FOLLOWING PUSHBACK,CENTER HYD SYSTEM LEAK. POOL OF FLUID WAS OBSERVED ABOUT 30 FT IN DIAMETER AND A TRAIL OF SPRAY COULD BE SEEN ALONG THE PUSHBACK PATH. EICAS MESSAGES APPEARED. MOC AND DISPATCH ADVISED. MAINTENANCE ADVISED THE LEAK CAME FROM THE TAISDR CA151202007Module · leaking(CAN) ON APPROACH FLIGHT, EXPERIENCED A L/E SLAT ASYMMETRY. A MISSED APPROACH WAS CONDUCTED AND THE QRH WAS CARRIED OUT BEFORE RETURNING FOR LANDING. AN EMERGENCY WAS NOT DECLARED. REPLACED FLAP/SLAT SHUTOFF VALVE MODULE IAW AMM 27-51-48-022-001.SDR CA151109008Priority Valve · failed(CAN) FLIGHT DIVERTED BACK TO AIRPORT DUE GEAR PROBLEMS. NLG RETRACT ACTR REPALCED IAW AMM 32-34-01-PB401 NLG PRIORITY VALVE CHANGED IAW AMM 32-34-07-404-009. LEAK CHECK OPEN TESTED NLG IAW AMM 32-34-00-715-001. EXT/RETRACTION NIL FAULTS.SDR CA151109006Fan · failed(CAN) FLIGHT CREW ADVISED AFTER ARRIVAL THEY HAD SMOKE IN THE CABIN EN-ROUTE. RESOLUTION L RECIRCULATION FUN REPLACED IAW AMM TASK 21-25-01 PLUS FAN INSTALLATION TEST C/O IAW TASK 25-21-01-864-022, NO FAULT FOUND MEL CLEARED.SDR CA151105006Proximity Sensor · out of adjust(CAN) SECOND DEPARTURE ATTEMPT, ACFT RETURNED TO AIRPORT. ACCOUNT SAME EICAS MESSAGE LANDING GEAR MONITOR. RESOLUTION FOUND SENSOR 235 OUT OF LIMIT INTERMITTENTLY. SENSOR 235 RT NLG ADJUSTED IAW AMM 32-61-03-822-022 TEST OK ON PROXIMITY BOX.SDR CA151103001Probe · failed(CAN) DUAL AUTO PILOT FAILURE SHORTLY AFTER DEPARTING. CAPTAIN PHONE PATCHED WITH MOC. UNABLE TO RESOLVE THE AUTO PILOT FAILURE. RETURNED TO DEPARTURE AIRPORT AND OVERWEIGHT LANDING CARRIED OUT. RESOLUTION REPLACED TAT PROBE REF AMM 34-12-02. CHECKS SERVICEASDR CA150909007Connector · not seated(CAN) IN CRUISE LOST RUDDER TRIM APPROXIMATELY 1HR OUT OF IST. DIVERSION TO LHR. RESOLUTION: C/B RESET, CONNECTOR PLUGS RESEATED AS PER FIM 27-21-00-990-805 OPERATIONAL TEST CARRIED OUT. ALL FUNCTIONS NORMAL.SDR CA150908002Sensor · contaminated(CAN) EMERGENCY DECLARED WITH ATC DUE TO FLIGHT CONTROL PROBLEMS. FLIGHT LANDED. IN FLT: L/E SLAT ASSYM EICAS MESSAGE. QRH CHECKLIST COMPLETED. OPERATED SLATS/FLAPS FULL CYCLE NUMEROUS TIMES. NO SLAT ASSYMETRY, NO MSGS, NORM OPS. PSEU BITE SHOWED "294". PSSDR CA150824003Coffeemaker · failed(CAN) SMOKE WAS DISCOVERED IN THE FORWARD GALLEY. CREW WAS JUST IN THE PROCESS OF RECEIVING THEIR ATC CLEARANCE. THE CREW DECLARED MAYDAY AND PROCEEDED TO THE NEAREST AIRPORT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IS INVESTIGATING THE CAUSESDR CA150730010Flap System · malfunctioned(CAN) FLIGHT EXPERIENCED LEADING FLAP ASYMMETRY ON FINAL APPROACH. NORMAL LANDING WAS CARRIED OUT. MAINTENANCE CONTROL ADVISED. RESOLUTION FAULTS CLEARED. NO HISTORY. FIM TASK 27-81-00-815-809 CARRIED OUT UNABLE TO FAULT. SYS CONSIDERED SERVICEABLE.SDR CA151119009Tire · failed(CAN) ON ROTATION FROM RUNWAY AIRCRAFT SUSTAINED A PROBABLE BLOWN TIRE RESULTING DAMAGE TO THE LEFT WING. THE AIRCRAFT IS RETURNING AND WILL LAND OVERWEIGHT. RESOLUTION - MAIN WHEEL ASSY NR 1, 2, 3, & 6 REPLACED. FOUND CORE CRUSHED AREA 16 X14 ON THE LOWER SDR CA151002009Cover · cracked(CAN) FOLLOWING INSPECTION AS REQUIRED BY AD 2014-22-09 AND SB 767-27A0229, OUT OF 4 ACFT INSPECTED, 1 AIRCRAFT WAS FOUND WITH A CRACKED COVER ASSY ON THE ACTUATOR FOUND IN POSITION NR 3. THE CONDITION IS NOT SOMETHING THAT THE SB IS LOOKING FOR AS THE SB IS SDR CA150324002Flap System · failed(CAN) THE ACFT ENCOUNTERED A FLAP DISAGREE ON FINAL APPROACH. THE FLIGHT CREW COMMENCED A MISSED APPROACH. THE SECOND APPROACH WAS OTHERWISE ROUTINE. NO ADVERSE PASSENGER REACTION WAS REPORTED. RESOLUTION NO MSG FOUND AND FLAP/SLAT OPERATIONAL TEST CARRIEDSDR CA150302010Shutoff Valve · defective(CAN) DEPARTURE DELAYED DUE TO RT ENGINE BLEED FLUCTUATING ON INBD LEG. AFTER DEPARTURE REPEAT RT ENGINE BLEED FLUCTUATING. IN CONCURRANCE WITH MOC DIVERTING FOR MAINTENANCE. RT ENGINE HP VAVLE REMOVED AND INSTALLED IN RT ENGINE PRV POSITION. REV AND INSTA
Back to Boeing 767-375