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.

SDR UIEA2017050300692Warning System · false activationLEFT ENGINE CONTROL EICAS MSG AFTER LANDING DURING TAXI IN. MESSAGE WAS NOT LATCHED FAULT REF AMM 71-00-00-726-268-H03 FFC STATIC TEST PERFORMED CHECKS/TEST NO FAULTS PRESENT.May 3, 2017 · N649GT · Boeing 767375 · Engine Fuel Indicating SystemSDR UIEA2017050100681Software · faultyEICAS STATUS PAGE DISPLAYS APU OIL ADD. UPDATED EICAS SOFTWARE PER AMM 31-41-02. OPS GOOD.Apr 28, 2017 · N1217A · Boeing 767375 · Central ComputersSDR UIEA2017042400627Window · failedRT SIDE WINDOW EICAS DURING CRUISE FLT. R & R WINDOW ASSEMBLY AND RIGGED IAW 56-11-02 OPS CHECKED GOOD.Apr 22, 2017 · N649GT · Boeing 767375 · Windshield/Door Rain/Ice RemovalSDR UIEA2017042400626Warning Message · false activationRT WINDOW HEAT EICAS, PERFORMED LEFT FWD OR RIGHT WINDOW ANTI ICING BITE PROCEDURE IAW FIM TASK 30-41-00-815 AND RIGHT FWD OR LEFT SIDE WINDOW ANTI ICING PROCEDURE 30-41-00-815. BITE TEST GOOD. NO FAULTS NOTED.Apr 22, 2017 · N649GT · Boeing 767375 · Windshield/Door Rain/Ice RemovalSDR UIEA2017042000611Warning Message · false activationDURING DESCENT AT 5000FT, RT WINDOW EICAS. PERFORMED TROUBLESHOOTING IAW FIM 30-41 TR 803, BITE TEST, SYSTEM OK, NO FAULTS PRESENT.Apr 19, 2017 · N649GT · Boeing 767375 · Windshield/Door Rain/Ice RemovalSDR UIEA2017041400581Valve · warning messageRIGHT ENGINE PRIORITY VALVE EICAS MESSAGE RECEIVED AFTER ENGINE START. DISAPPEARED AFTER 5 MINUTES. REMOVED AND REPLACED THE RT ENGINE PRIORITY VALVE IAW AMM 36-11-18. CHECKED OK.Apr 14, 2017 · N1217A · Boeing 767375 · Pneumatic Distribution SystemSDR UIEA2017041400582Pump · not reportedCIRCUIT BREAKER, RIGHT FUEL OVERRIDE PUMP. REMOVED AND REPLACED R/H OVERRIDE PUMP IAW AMM 28-22-05, AND 28-22-05-404-078-022. OPS CHECKED GOOD IAW AMM 28-31-00.Apr 14, 2017 · N1217A · Boeing 767375 · Fuel Boost PumpSDR UIEA2017041400580Fan · malfunctionedSTATUS MESSAGE FOR THE AFT EQUIPMENT EXHAUST FAN 1. REMOVED AND REPLACED THE EXHAUST FAN IAW AMM 21-58-00. OP CHECKED GOOD.Apr 14, 2017 · N649GT · Boeing 767375 · Air Distribution FanSDR UIEA2017040700527Selector Switch · stuckWEATHER RADAR FAILED MESSAGE, FOUND THE WEATHER RADAR PANEL SELECTOR SWITCH STUCK , CLEANED AND OPS CHECKED GOOD.Apr 7, 2017 · N649GT · Boeing 767375 · Weather Radar SystemSDR UIEA2017040700526Igniter · failedAPU COLD SOAK START ATTEMPT UNSUCCESSFUL TWICE. ATTEMPTED APU COLD SOAK START AFTER TWO HOURS AT FL 410. APU SHUT DOWN TWICE AFTER REACHING APPROXIMATELY 750 EGT. FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED THE APU IGNITER PLUG, OPS CHECKED OK IAW AMM 4Apr 7, 2017 · N649GT · Boeing 767375 · APU Start/Ignition SystemSDR UIEA2017040300497Connector · wornLEFT PACK COMPRESSOR OUTLET TEMP SENSOR TS41 FOUND THE ELECTRICAL CONNECTOR D00688 WORN. THE ELECTRICAL CONNECTOR WAS REMOVED AND REPLACED IAW WDM 21-51-12, REV 26. OPS CHECKED IAW 21-51-14, REV 120, AND FOUND SATISFACTORY.Apr 5, 2017 · N1217A · Boeing 767375 · Air Conditioning System WiringSDR UIEA2017031300325Stringer Splice · corrodedBS 434, STRINGER SPLICE 38R CORRODED. THE STRINGER SPLICE REMOVED & REPLACED IAW SRM 51-40-02, REV.103.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Longeron/StringerSDR UIEA2017040200485Support · wornRIGHT ENGINE, RT CORE COWL PRESSURE RELIEF DOOR ASSY INTERIOR SURFACE UPPER LANYARD ATTACHING SUPPORT FOUND WORN. REMOVED AND REPLACED IAW AMM 71-11-09, REV 120. LATCH CHECKED IAW AMM 71-11-09, REV 120, FOUND SATISFACTORY.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017040200488Frame · wornRT ENGINE, RT CORE COWL AFT ZEE FRAME REPAIR ANGLE DOUBLER & FILLER FOUND WORN. REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017031300323Adapter · wornNR 1 ENGINE, RT FAN COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN ADAPTER FOUND WORN. THE ADAPTER WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017031300324Bulkhead Web · dentedAFT CABIN, AFT PRESSURE BULKHEAD BS 158 DENTED. TRIMMED & REPAIRED IAW SRM 53-80-08, REPAIR 2, DETAIL I, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, BulkheadSDR UIEA2017031300326Stringer Splice · corrodedBS 434, STRINGER SPLICE 37R CORRODED. THE STRINGER SPLICE WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Longeron/StringerSDR UIEA2017031300328Stringer Splice · corrodedBS 434, STRINGER SPLICE 38L CORRODED. THE STRINGER SPLICE WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Longeron/StringerSDR UIEA2017031300329Stringer Splice · corrodedFWD CARGO AT BS 434, STRINGER SPLICE 37L CORRODED. THE STRINGER SPLICE WAS REMOVED & REPLACED IW SRM 51-40-02, REV.103.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Longeron/StringerSDR UIEA2017031300330Stringer Splice · corrodedFWD CARGO BAY AT BS 434 STRINGER SPLICE 39R CORRODED. THE STRINGER SPLICE WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Longeron/StringerSDR UIEA2017031300331Stringer · corrodedFWD CARGO BAY, BS 434, STRINGER 36R CORRODED. REPAIRED IAW SRM 53-30-03, REPAIR 1, DETAIL III, REV 103, & EN 1043-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Longeron/StringerSDR UIEA2017031300332Skin · corrodedFWD CARGO BAY SKIN CORRODED UNDER STRINGER 36R, BS 430. THE SKIN WAS TRIMMED & REPAIRED IAW EN 1043-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Plate/SkinSDR UIEA2017031300333Door Frame · corrodedL2 DOOR CUTOUT BS 923.7, WL 200.73 FOUND THE DOOR FRAME WEB CORRODED. TRIMMED THE AREA & REPAIRED IAW EN 1071-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, StructureSDR UIEA2017031800362Shear Pin · wornNR 2 ENGINE, RT FAN COWL LOWER MOST FWD AND AFT SHEAR PIN FOUND WORN. THE SHEAR PIN WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017031600356Butt Joint · corrodedFWD CARGO BAY, BS 434 BETWEEN STRINGERS 35L AND 35R, BUTT SPLICE FOUND CORRODED. THE BUTT SPLICE WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, StructureSDR UIEA2017031600352Web · corrodedAFT CARGO BAY, THE WEB WAS FOUND CORRODED. THE WEB WAS TRIMMED & WEB REPAIRED IAW EN1076-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Miscellaneous StructureSDR UIEA2017031500351Web · crackedAFT CARGO AT BS 1197+66, LBL 41, WL 120 STIFFENER TO WEB HAD TWO RIVETS SHEARED AND WEB CRACKED. THE WEB WAS TRIMMED & REPAIRED IAW EN1078-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Miscellaneous StructureSDR UIEA2017031500350Tee Fitting · corrodedAFT CARGO, BS 1219, WL 124.43, LBL 44 - RBL 44, FOUND THE TEE FITTING FOUND MULTIPLE AREAS OF SURFACE CORROSION. THE TEE FITTING WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Attach FittingsSDR UIEA2017031500349Tee Fitting · corrodedAFT CARGO, BS 1197+132, WL 124.43, LBL 44 - RBL 44, FOUND THE TEE FITTING WITH MULTIPLE AREAS OF CORROSION ON THE ANCHOR NUT ATTACHMENT AREA. THE TEE FITTING WAS REMOVED & REPLACED IAW SRM 51-40-02, REV.103.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Attach FittingsSDR UIEA2017031400343Skin · corrodedLEFT AFT LOWER FUSELAGE AT SKIN BS 1582 - 1614, STRINGER 36L FOUND BUTT AND LAP JOINT AREA CORRODED. THE CORROSION WAS REMOVED & REPAIRED IAW EN 1020-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Plate/SkinSDR UIEA2017031400344Skin · corrodedAFT CARGO, BS 1263, STRINGER 37-38R, BILGE AREA INNER SURFACE SKIN CORRODED. AREA TRIMMED OUT & REPAIRED IAW EN 1069-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Plate/SkinSDR UIEA2017031400342Skin · corrodedRIGHT AFT LOWER FUSELAGE SKIN BS 1583.5 - 1610, STRINGER 36R, FOUND THE LAP JOINT AREA CORRODED. THE CORROSION WAS REMOVAL & REPAIRED IAW EN 1020-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Plate/SkinSDR UIEA2017031300340Skin · corrodedCORROSION FOUND ON THE SKIN, LBL 3 TO RBL 3, BS 955. THE CORROSION WAS REMOVED & REPAIRED IAW EN 1022-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Plate/SkinSDR UIEA2017031300337Skin · corrodedLEFT AFT LOWER FUSELAGE SKIN BS 1582, STRINGER 26L, FOUND THE LAP JOINT AREA CORRODED. THE CORROSION WAS REMOVED IAW EN 1040-17, REV-.Apr 5, 2017 · N1217A · Boeing 767375 · Fuselage Main, Plate/SkinSDR UIEA2017040100423Shear Pin · wornNR 1 ENGINE, RT FAN COWL LOWER MOST FWD SHEAR PIN FOUND WORN. THE SHEAR PIN WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200427Fairing · damagedNR 1 PYLON FAIRING ASSY, HAD ONE ELONGATED HOLE OUTBOARD AFT FAIRING ASSY. REPAIRED IAW EN1048-17, REV.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200430Adapter · wornLEFT ENGINE, LT CORE COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN SUPPORT BRACKET & ADAPTER WERE FOUND WORN. REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200445Rub Strip · wornRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200443Rub Strip · wornLEFT ENGINE, LT CORE COWL INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200442Rub Strip · wornLEFT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP FOUND WORN. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200441Stop · wornRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE MOST AFT HAT CHANNEL HAD ONE STOP FOUND WORN. THE HAT FRAME STOP REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200440Rub Strip · damagedRIGHT ENGINE, RT CORE COWL EXTERIOR SURFACE FWD EDGE SEVERAL WEAR STRIP WITH COATING FRETTED & CRACKED.THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200439Rub Strip · crackedRIGHT ENGINE, LT CORE COWL EXTERIOR SURFACE FWD EDGE SEVERAL WEAR STRIP FOUND COATING FRETTED & CRACKED. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200438Frame · crackedRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER SECOND FRAME FROM AFT, FOUND CRACKED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200436Rub Strip · crackedLEFT ENGINE, RT CORE COWL EXTERIOR SURFACE FWD EDGE SEVERAL WEAR STRIP FOUND COATING FRETTED & CRACKED. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200435Rub Strip · crackedLEFT ENGINE, LEFT CORE COWL EXTERIOR SURFACE FWD EDGE SEVERAL WEAR STRIP FOUND THE COATING FRETTING & CRACKED. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200434Adapter · wornRIGHT ENGINE, RT CORE COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN SUPPORT BRACKET &;ADAPTER FOUND WORN. REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200433Adapter · wornRT ENGINE, LT CORE COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN SUPPORT BRACKET & ADAPTER FOUND WORN. THE BRACKET AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200432Adapter · wornLEFT ENGINE, RT CORE COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN SUPPORT BRACKET & ADAPTER WERE FOUND WORN. THE HOLD OPEN ROD STOW PIN BRACKET AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200446Rivet · shearedLEFT ENGINE, RT CORE COWL EXTERIOR SURFACE PRECOOLER ASSY FOUND RIVET SHEARED. THE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main Frame
Back to Boeing 767-375