Boeing 767-3JHF
Service difficulty reports · 709
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 = '7673JHF' 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 = '7673JHF' 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 P5CA2020091800316Controller · faultedRIGHT PACK TEMP EICAS IN FLIGHT. PERFORMED PTC BITE TEST, FOUND CONTROLLER FAULT. REMOVED AND REPLACED CONTROLLER, IAW AMM 21-51-4.SDR P5CA2020091400312Controller · malfunctionedRIGHT PACK TEMP EICAS AFTER TAKEOFF, LEFT PACK DEFERRED. RETURN TO ICN. FOLLOWED FIM TASK 21-51 FAULT TREE 844 PERFORMED T/S, FOUND RT STANDBY CONTROLLER FAULT. REMOVED AND REPLACED RT STANDBY CONTROLLER AND CHECKED OK, NO FAULT FOUND PER AMM 21-51-14/401. SDR P5CA2020091530308Duct · crackedUPON ARRIVAL INTO THE COCKPIT THE TEMPERATURE WAS 29. T/S AND FOUND RT PACK COMPRESSOR OUTLET DUCT CRACKED. SWAPPED DUCT WITH LT PACK THEN RT PACK OPS CHKS NORMAL, AS PER AMM 21-51-03. APPROVED BY MCC. LT PACK IS ALREADY DEFERRED.SDR P5CA2020091400311Controller · malfunctionedLT PACK INOP, COCKPIT WOULD NOT COOL DOWN, REMAINED OVER 33'C AT FL 340 ENTIRE FLIGHT. TRANSFERRED TO MDDR 134263 IAW MEL 21-51-01-01, CAT C. REMOVED AND REPLACED LT PACK TEMP CONTROLLER AND OPER CHECKED OK, NO FAULT FOUND, PER AMM 21-51-14/401. A/C OK FOR SDR P5CA2020091180304Control Unit · malfunctionedAUTOBRAKES DISARM PRIOR TO LANDING. T/S AND FOUND SUSPECT ANTISKID/AUTOBRAKE CONT UNIT DEFECTIVE, PER WDM 32-42-03 P/N: S003T001-07. ITEM TRANSFERRED TO MDDR NR 134057, AS PER MEL 32-42-04-01A CAT C, CAT III RECTRICTED. INSTALLED PLACARD. REMOVED AND REPLASDR P5CA2020091070303Transmitter · malfunctionedLT ENG AFTER START 160 PSI (TOP OF SCALE), ALL OTHER INDICATIONS NORMAL. LEFT ENGINE OIL PRESSURE TRANSMITTER REPLACED, AS PER AMM 79-32-21. ENGINE SPIN CHECK OK, INDICATION NORMAL.SDR P5CA2020090860301Controller · malfunctionedLT PACK TEMP EICAS INDICATION ON DEPARTURE. RAN QRH TEMP EICAS AND INOP MSG EXTINGUISHED. BIT ON LPTC SHOWS CONT FAULT + RAI ACTUATOR, RESET + VERIFIED C/O IAW AMM 21-51-00. DEFECT CLEARED SUBS PACK OPS DURING TRANSIT SATIS. DUE HISTORY APPLIED MEL 21-51-0SDR P5CA2020090410300Actuator · malfunctionedON CLIMB OUT RECEIVED "L PACK TEMP" EICAS MESSAGE. COMPLIED WITH QRH.(<P>PACK TEMP CONT "AUTO" INOP. ITEM DEFERRED PER MEL 21-51-03-01, MDDR #133749, CAT 'C'.</P><P>LP 1153914 ITEM 7: PTC BITE SHOWS "RAM INLET ACTR" FAULT, SO REMOVED & REPLACED L PACK RAM AIR SDR P5CA2020090100299Apu · malfunctionedAFTER LANDING ON APU START, APU FAULT, EICAS MSG ONE RESTART ATTEMPT FAILED. ITEM TRANSFERRED TO DMI 133730 PER MEL 49-11-01A, CAT C. REPLACED APU IAW WORK CARD A-49-999-00-01, OPS GOOD. THIS CLEARS MDDR 133730. PLACARD REMOVED.SDR P5CA2020090100294Apu · faultedAPU FAULT AFTER ATTEMPTED START DURING TAXI. PERFORM BITE TEST OF ECU PER FIM 49-11 TASK 987. OPS CHECK NORMAL PER AMM 49-11-00,SDR P5CA202008310291Warning Message · false activationFWD CARGO BACKUP EICAS MSG(PERFORMED OPERATIONAL TEST IAW AMM 21-43-00 SYSTEM OK).SDR P5CA202008310292Idg · disconnectedRIGHT GEN DRIVE EICAS MESSAGE(RAN QRH DISCONNECTED DRIVE. CREW ADVISED IDG DISCONNECTED EICAS MAINTENANCE PAGE RIGHT IDG DRIVE/AUTO EVENT IDG OIL LEVEL CHECKED FULL 2 SCAV FILTER DELTA P IS SET PER MEL HYD HMG CHECKED C/OSI MEL 24-00-01-01 CAT B APPLIED MDDR SDR P5CA2020083100293Overheat Sys · malfunctionedRIGHT ENGINE OH LP1; LEFT ENGINE OH LP2 STS MESSAGE DISPLAYED(PERFORMED CONVERSION FIRE DETECTION SYSTEM PER EO 6726A005 THEN FIRE/OVERHEAT SYSTEM OPERATIONS CHECKED NML AS PER AMM 26-10-01 WDM 26-11-22).SDR P5CA2020081700285Start Valve · malfunctionedRIGHT ENGINE START VALVE INOPERABLE (APPLIED MEL 80-00-02-01 WITH MDDR 132891, CAT 'C'. C/W MAINT PROCEDURE, MCC MIZ TIME 007. LP 1131722 ITEM 4: REMOVE AND REPLACED RIGHT ENGINE STARTER VALVE OPS NORMAL PER AMM 80-11-02/401. ITEM CLOSED DMI # 132891, NOTIFIEDSDR P5CA2020081410282Ecu · malfunctionedAPU PNEUMATIC FUNCTION INOP( DUCT PRESS TOO LOW)(<P>TRANSFERRED TO MDDR 132716 AS PER MEL 49-11-01-01 CAT C.<BR /></P><P><BR DATA-MCE-BOGUS="1" /></P><P>REMOVED AND REPLACED APU ECU THEN OPERATED CHECK OK PER AMM 49-61-05/401. CLEARED MDDR 132716. NOTIFIED MCCSDR P5CA2020081410283Valve · malfunctionedAPU PNEUMATIC FUNCTION INOP (AUXILIARY POWER UNIT, PNEUMATIC FUNCTION)(<P>TRANSFERRED TO MEL 49-11-01-01, MDDR 132671 RAISED, CAT 'C'.<BR /></P><P>LP 1131759 ITEM 7: IAW AMM 49-53-01/401 REMOVED & REPLACED SURGE CONTROL VALVE AND APU BLEED SYSTEM NORMAL WITH ESDR P5CA2020080500274Warning Message · false activationHI FLOW INHIBIT STATUS MSG PRIOR TO BLOCK OUT FOLLOWED FIM 21-51 TASK 875, CYCLED PACKS AND OPS CHECK GOOD, MSG CLEARED.SDR P5CA2020080420272Apu · faultedAPU FAULT, APU BITE CARRIED OUT, NO LIGHT OFF, MINI FLAG CODE IGNITION UNIT. APU START ATTEMPT CARRIED OUT NORMAL. APU RESET IAW AMM 49-61-00.SDR P5CA2020080430273Ignition Unit · failedAPU COLD SOAK START UNSUCCESSFUL AFTER 3 ATTEMPTS AT FL 320, OAT -39C. APCU BITE SHOWS FAULT REASON NO LIGHT OFF, FAULT LRU IGNITION UNIT. REMOVED AND REPLACED APU IGNITER PLUG. . REMOVED AND REPLACED APU IGNITION UNIT IAW AMM 49-41-03-401. CHECKED GOOD.SDR P5CA2020072700271Unknown · odorFOUND WHEN #2 PACK ON, ODOR SMELL IN COCKPIT.(<P>PER AMM TASK 21-51-21-004-001/404-015 REV. INSP PACK WATER SEPARATOR AND NO CONTAMINATION FOUND. AFT APU CHANGED PER AMM TASK 21-00-21-102-030 REV 130, CHECK NO ODOR SMELL WHEN OPERATING PACK 2.</P>)SDR P5CA2020072700270Plug · leakingFOUND #1 ENG STARTER DRAIN PLUG CHECK VALVE FUNCTION FAIL AND OIL LEAK(<P>PER AMM TASK 12-22-02-603-054-001 REV 130 REPLACE #1 ENG STARTER DRAIN PLUG AND SERVICE STARTER OIL WITH MOBILE JET -11 AND OVERFLOW, CONDITION CHK NO LEAK FOUND AND CONDITION SATISFACTOSDR P5CA2020072700269Plug · no testFOUND #2 ENG STARTER DRAIN PLUG CHECK VALVE FUNCTION FAIL AND OIL LEAK.(<P>PER AMM TASK 12-22-02-603-054-001 REV 130 REPLACED #2 ENG STARTER DRAIN PLUG AND SERVICE STARTER OIL WITH MOBIL JET -11 AND OVERFLOW, CONDITION CHECK NO LEAK FOUND. JOB COMPLETED AND COSDR P5CA2020072000266Control Valve · faultedRIGHT PACK INOPERATIVE. PERFORMED APU PNEUMATIC FUNCTION SYSTEM, CHECKED OK, REPLACED FLOW CONTROL VALVE IAW AMM 21-51-00. PERFORMED SYSTEM TEST, CHECKED OK.SDR P5CA2020070600248Terminal · contaminatedAFTER TAKEOFF APPROX 4 MINUTES IN FLIGHT "L ENG FIRE LP 1" STATUS MESSAGE INTERMITTENTLY DISPLAY. AFTER APPROX 30 MIN, STATUS MSG DID NOT DISPLAY. PERFORMED RESISTANCE INSULATION CHK BTWN L-ENG LP 1 FIRE DET CARD AND AFT UPR, AFT LWR, FWD LWR DEFECTORS PER WSDR P5CA2020063000208Starter · wornFOUND APU STARTER MOTOR BRUSH WORN OUT. IAW AMM 49-41-01-404-007 R 130 TO REPLACE STARTER MOTOR OF APU AND PERFORMED OPER TEST, RESULT NORMAL.SDR P5CA2020063000209Sleeve · brokenFOUND APU SURGE SLEEVE BROKEN. PER AMM 49-53-01-004-001 / 49-53-01-404-010 REV 130 REPLACE APU SURGE SLEEVE, OPERATION AND CONDITION CHECK NORMAL, NO LEAK FOUND.SDR P5CA2020062970206Latch · inoperativeEMERGENCY ESCAPE ROPE DOOR ABOVE CO-PILOT SEAT DOES NOT PROPERLY LATCH.(<P>ADJUSTED LATCH, OPERATIONAL CHECK NORMAL IAW AMM 25-61-00.</P>)SDR P5CA2020062900207Circuit Card · inoperativeL/H ENG FIRE WARNING LIGHT INOPERATIVE. REMOVED & REPLACED WITH NEW DETECT CARD IAW AMM 26-10-01 AND SYSTEM OPERATIONAL CHECKED OK.SDR P5CA2020062960205Terminal · loose"R ENG FIRE LP 2" STATUS MESSAGE DISPLAYED. CHECKED & FOUND #2 ENG LOWER AFT LOOP 2 TERMINAL LOOSE. TIGHTENED TERMINAL IAW AMM 26-11-00, OPERATIONAL CHECKS OK.SDR P5CA2020062600204Circuit Card · faulty"R ENG FIRE LP 1" STATUS MSG DISPLAYED. REMOVED AND REPLACED M683 LOOP 1 FIRE DETECTOR RIGHT CARD PER AMM 2610-01/401, REMOVED AND REPLACED M684 LOOP 2 FIRE DETECTOR RIGHT CARD PER AMM 26-10-01/401, REMOVED AND REPLACED M10274 LOGIC TEST FIRE/OVHT CARD 2 AND SDR P5CA2020062520201Anti-Ice System · unknownENGINE ANT-ICE IN AUTO REMAINED ON FOR THE LAST 13 MIN OF FLIGHT WITH CLEAR SKIES. 48 C. LT & RT ENG THERMAL NACELLE ANTI-ICE VALVES OPERATION CHECK COMPLETED IAW AMM 30-21-03-714. ALL OPS & INDICATIONS NORMAL.SDR P5CA2020061760196Unknown · unknownIN FLIGHT, FLT DECK TEMP BECAME UNCONTROLLABLE. RAN QRH CABIN TEMP HOT, COMPLETED FLT WITH PACKS IN STBY. TESTED BOTH PTC AND ZTC AND ALL CHECKED OK IAW AMM 21-51-00/501, 21-61-03/501 AIR CONDITION SYSTEM CHECKED OK ON GROUND.SDR P5CA2020061600195Unknown · malfunctionedIN FLIGHT, FLT DECK TEMP BECAME UNCONTROLLABLE. RAN QRH CABIN TEMP HOT (FREIGHTER). COMPLETED FLIGHT WITH PACKS IN STNY-N. PACK TEMP CONTROLLERS AND ZONE TEMP CONTROLLER BITE TEST C/O OK IAW 21-61-00.SDR P5CA2020061600192Apu · shutdownPRIOR TO PUSH AND ENGINE START APU FAILED: SHUT DOWN WITH FAULT LIGHT. PERFORMED APU BITE AND NO FAULT FOUND AS PER AMM 49-61-05. APU OPS NORMAL AS PER AMM 49-11-00.SDR P5CA2020061500191Gcu · malfunctionedAFTER ENG START L GEN OFF EICAS ANNUNCIATED. RESET L GEN CONTROL PER NON-NORMAL, OPS NORMAL REMAINDER OF FLIGHT. FOUND BPCN BITE NO FAULT, REMOVED AND REPLACED LEFT GCU BY MCC REQUEST THEN LEFT GENERATION SYS OPS NORMAL. ALSO FOUND NO FAULT WITH ENG RUNNING PESDR P5CA2020061000189Warning Message · false activationAFTER ENGINE START "L GEN OFF" EICAS MSG. WITH THE LEFT GEN CONT OFF LIGHT ILLUMINATED. ACCOMPLISHED QRH L GEN CONT SWITCH OFF. THEN LEFT GEN OPERATED NORMAL. INFO NOTED FOR FURTHER REPORT IF REC'D. OPS OK REF AMM 24-11-00.SDR P5CA2020060900187Controller · faultedLEFT A/C PACK WAS INOPERATIVE. PTC BITE SHOWS A CONTROLLER FAULT. PERFORMED LT PTC VERIFICATION, TESTED OK IAW AMM 21-51-14. REMOVED AND REPLACED THE PACK, TEMP CONTROLLER IAW AMM 21-51-14/401. BITE TESTED NORMAL.SDR P5CA2020060800175Warning System · false activationLT PACK TEMP EICAS OBSERVED ON CLIMB OUT. PERFORMED QRH; PROC. DID NOT RESET. CONTINUED FLIGHT W/ LEFT PACK OFF IAW QRH. IAW FIM 21-51 TASK 877, LT PTC BITE CONTROLLER AND INLET DOOR ACTR FAULT LIGHT ON. PFM VERIFY. RESET, BOTH LIGHT GONE. PERFORMED LT PACK CHSDR P5CA2020060800174Warning System · false activationAT 0950Z, FL200 NR 1 PACK TEMP EICAS MSG, ACCOMPLISHED QRH CHECKLIST THRU "L" PACK CONTROL SELECTOR OFF. PACK INOP LIGHT REMAINED ON DURING PROCEDURE. LEFT HAND PACK CONTROLLER / BITE TEST CARRIED OUT. LEFT RAM AIR INLET DOOR FAULT ANNUNCIATION. VERIFY AND RESSDR P5CA2020060800172Warning System · false activationSTATUS MESSAGE L ENG FIRE LP 1 ILLUMINATED, EXTINGUISHED MULTIPLE TIMES DURING FLIGHT. ALREADY EXISTING STATUS MESSAGE, ALSO ENGINE FIRE DETECTION SYSTEM GROUND TEST PASSED PER AMM 26-11-00/501.SDR P5CA2020061700169Guide Vane · damagedFIVEOF OGV'S ON RT ENGINE FOUND DELAMINATED AT 9 O`CLOCK LOOKING FROM AFT. PERFORMED TEMPORARY REPAIR IAW EO 1972A783, REMOVED AND REPLACED THE NR 2 ENGINE FAN CASES OGV'S IAW AMM 72-33-04.SDR P5CA2020060200169Guide Vane · delaminatedFIVE OF OGV'S ON RT ENGINE FOUND DELAMINATED AT 9 O CLOCK LOOKING FROM AFT. PERFORMED TEMPORARY REPAIR AS PER EO 1972A783. REPEAT INSPECTION EVERY 3 FLT CYCLES FOR THE INTEGRITY. PERMANENT REPAIR NEED BEFORE 25 FLT CYCLES. RAISED NON-MEL #129103.SDR P5CA2020060100167Sense Line · looseRIGHT ENG PRV STATUS MESSAGE. AIR SUPPLY BITE TEST SHOWED NO FAULT DETECTED. PRV FULLY CLOSED WHICH IS NORMAL. TIGHTENED SENSE LINES. COMPLIED WITH ENG RUN. PNEUMATIC TEST OK. NO FAULTS NOTED, MESSAGE ERASED IAW FIM 36-10 FT 841 AND AMM 71-00-00/201.SDR P5CA2020052900166Oxygen Mask · defectiveCREW REPORTED CAPTAIN`S OXY MASK BAFFLE IS BAD. REMOVED & REPLACED CAPTAIN`S OXY MASK IAW AMM 35-11-51-401.SDR P5CA2020051300159Valve · inoperativeFOUND OVERRIDE VALVE INOP WHEN PERFORMING EO6721A012.(<P>PER AMM 21-58-20-024-035/21-58-20-424-033 REV 130 REPLACED OVERRIDE VALVE. TESTED NORMAL AND CONDITION CHECK NORMAL.</P>)SDR P5CA2020051100152Packing · damagedFOUND ENG-1 PRV ACTUATOR UNION AIR LEAK.(<P>IAW AMM TASK 36-11-18-004-001/040-018-01 REV 130 PERFORM REPLACEMENT OF ENG-1 PRV ACTUATOR UNION PACKING. IAW AMM TASK 36-11-09-782-138-001 REV 130 PERFORM PRESSURIZED AIR LEAK TEST, RESULT NO LEAK FOUND. </P>)SDR P5CA2020051100153Starter · damagedFOUND RH ENG STARTER MCD HAS METAL CHIPS.(<P>PER AMM TASK 80-11-01-004-084/404-081 REV 130 REPLACED RH ENG STARTER AND CONDITION CHECK NORMAL. PER AMM TASK 71-00-00-862-053-H03 REV 130 PERFORM RH ENG RUN AND TEST NORMAL. </P>)SDR P5CA2020051100154Packing · damagedFOUND ENG 2 PRV ACTUATOR UNION AIR LEAK(<P>IAW AMM TASK 36-11-18-004-001-001/040-018-01 REV 130 PERFORM REPLACEMENT OF ENG-2 PRV ACTUATOR UNION PACKING. IAW AMM TASK 36-11-09-782-138-001 REV 130 PERFORM PRESSURIZED AIR LEAK TEST, RESULT NO LEAK FOUND. </P>)SDR P5CA2020051100155Warning System · false activationFOUND MSG "FAILURE LEFT PRSOV CLOSED AND OPEN SWITCHES DISAGREE" DUE TO PERFORM ASM SYSTEM TEST.(<P>IAW AMM 36-11-09-862-082-001 REV 130 PERFORM L/H PRSOV INSTALLATION TEST. TEST RESULT SATISFACTORY AND NO RELATED MESSAGES FOUND.</P>)SDR P5CA2020050100149Unknown · smokeSMELL OF BURNING RUBBER AND SMOKE FOR 10 SECS (APPROX) ON DESCENT THROUGH 15,000 FT.(<P>CHECKED LAVATORY P6, P11 PNL AND COCKPIT CONTROL PNL, GALLEY AREA, NO SMOKE BURNING SMELL FOUND. NO EICAS MSG PER AMM 26-00-00, MEC AREA AND AIR CONDITION CHK NORMAL. PER A
Back to Boeing 767-3JHF