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 UIEA2017040200447Rivet · shearedLEFT ENGINE, RT CORE COWL FWD LOWER SECTION FOUND SEVERAL RIVETS SHEARED. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200448Rivet · shearedLEFT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP ATTACHING RIVET FOUND SHEARED. THE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200449Rivet · shearedLEFT ENGINE, RT CORE COWL INTERIOR SURFACE MOST AFT HAT FRAME SPLICE ANGLE HAD ONE ATTACHING RIVET FOUND SHEARD. THE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200450Rivet · looseLEFT ENGINE, LT CORE COWL FWD LOWER SECTION FOUND SEVERAL RIVETS LOOSE. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200451Seal · crackedLEFT ENGINE, LT CORE COWL FAIRING ASSY AFT UPPER EDGE STRIP SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200452Seal · crackedRIGHT ENGINE, LT CORE COWL FAIRING ASSY AFT UPPER EDGE STRIP SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200453Seal · crackedRIGHT ENGINE, RT CORE COWL FAIRING ASSY AFT UPPER EDGE STRIP SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200454Seal · crackedRIGHT ENGINE, LT CORE COWL FAIRING ASSY FLIPPER DOOR SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200455Seal · crackedRIGHT ENGINE, RT CORE COWL FAIRING ASSY FLIPPER DOOR SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200457Seal · tornRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200456Seal · tornLEFT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200458Channel · wornLEFT ENGINE, LT CORE COWL INTERIOR SURFACE MOST AFT HAT CHANNEL HAD TWO EXISTING REPAIR ANGLE DOUBLERS FOUND WORN, LOCATED 19 INCHES & 30.3 INCHES FROM LOWER EDGE. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017040200463Frame · 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 UIEA2017040200464Channel · wornRIGHT ENGUNE, LT CORE COWL INTERIOR SURFACE MOST AFT HAT CHANNEL HAD ONE EXISTING REPAIR ANGLE DOUBLER WORN, LOCATED 6 INCHES FROM LOWER EDGE. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017040200465Frame · wornLEFT ENGINE, RT CORE COWL AFT ZEE FRAME HAS ONE EXISTING REPAIR ANGLE DOUBLER WORN, LOCATED 12 INCHES FROM LOWER EDGE. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200466Skin · wornRIGHT ENGINE, LT CORE COWL FAIRING SKIN UPPER AFT CUTOUT SECTION INTERIOR SURFACE FOUND WORN. THE SKIN WAS REPAIRED IAW SRM 54-423-01-2R-5, REPAIR 5 , REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Plate/SkinSDR UIEA2017040200467Rub Strip · wornLEFT ENGINE, RT 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 UIEA2017040200470Structure · damagedLEFT ENGINE, RT CORE COWL INTERIOR SURFACE AFT LOWER CORNER FOUND FASTENER HOLE ELONGATED ON SUPPORT TEE & HAT CHANNEL. REPAIRED IAW SRM 51-40-02 , REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200471Skin · crackedRIGHT ENGINE, LT CORE COWL SKIN UPPER AFT CUTOUT SECTION FOUND CRACKED. THE SKIN CUTOUT WAS REPAIRED IAW SRM 54-423-01-2R-4, REPAIR 4, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Plate/SkinSDR UIEA2017040200472Frame · damagedRIGHT ENGINE, RT CORE COWL INTERIOR SURFACE AFT LOWER CORNER FOUND FASTENER HOLE ELONGATED ON SUPPORT TEE & HAT FRAME. REAMED TO NEXT SIZE AND A NEW FASTENER INSTALLED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200473Rub Strip · wornLEFT ENGINE, RT CORE COWL FAIRING ASSY AFT UPPER EDGE STRIP SEAL FOUND CRACKED. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200474Rub Strip · wornLEFT ENGINE, RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER EDGE RUBSTRIP FOUND WORN. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200475Skin · crackedRIGHT ENGINE, RT CORE COWL SKIN UPPER AFT CUTOUT SECTION FOUND CRACKED. REPAIRED IAW SRM 54-42-01-2R-4, REPAIR 4, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Plate/SkinSDR UIEA2017040200476Rivet · looseRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE AFT UPPER PLATE FOUND RIVET LOOSE. THE LOOSE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Plate/SkinSDR UIEA2017040200477Frame · wornRT ENGINE, LT CORE COWL INTERIOR SURFACE SECOND ZEE FRAME FROM FWD ONE EXISTING REPAIR ANGLE DOUBLER FOUND WORN. FRAME REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200478Frame · wornRIGHT ENGINE, RT CORE COWL INTERIOR SURFACE SECOND ZEE FRAME FROM FWD FOUND WORN. THE AREA WAS CLEANED UP AND FOUND WITHIN LIMIT IAW SRM 54-42-02-1A-1, FIG 101, NOTE B, DETAIL 1, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200479Angle · crackedLEFT ENGINE, RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT ANGLE FOUND CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017040200480Longeron · wornRIGHT ENGINE, RT CORE COWL INTERIOR SURFACE LOWER MOST AFT LONGERON FOUND WORN. LONGERON REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200482Longeron · wornRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE LOWER AFT LONGERON FOUND WORN. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200483Retainer · crackedNR 2 ENGINE, RT FAN COWL INTERIOR SURFACE UPPER AFT EDGE SEAL RETAINER FOUND CRACKED. THE SEAL RETAINER WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200484Intercostal · wornRT ENGINE, RT CORE COWL PRESSURE RELIEF DOOR SURROUNDING INTERCOSTAL FOUND WORN. INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017040200487Adapter · wornNR 2 ENGINE, RT FAN COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN ADAPTER AND FITTING FOUND WORN, LOCATED AT FWD LOWER SECTION. REMOVED AND REPLACED IAW SRM 51-40-02 REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040200489Duct · wornRT ENG, RT CORE COWL PRECOOLER EXIT DUCT LIP FOUND WORN. REPAIRED IAW SB 71-032 REV 2.Apr 5, 2017 · N1217A · Boeing 767375 · Engine Mount SectionSDR UIEA2017040200490Fireshield · damagedRIGHT ENG, RT CORE COWL INTERIOR SURFACE FIRESHIELD FOUND WITH TWO HOLES. REPAIRED IAW SRM 54-42-01-2R-6, REPAIR 6, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Bulkhead/FirewallSDR UIEA2017040300493Seal · tornNR 2 ENGINE, RT FAN COWL LOWER EDGE MOST FWD AND SECOND FROM FWD SEALS FOUND TORN. REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040300494Feeder Cable · chafedFWD STRUT FEEDER WIRES FOUND WITH CHAFED. THE FEEDER WIRES PROTECTED WITH TEFLON TAPE IAW SWPM 20-10-13, REV 64, AND FOUND SATISFACTORY.Apr 5, 2017 · N1217A · Boeing 767375 · Powerplant System WiringSDR UIEA2017040300495Feeder Cable · chafedFWD STRUT, TWO FEEDER WIRES FOUND CHAFED. THE FEEDER WIRES PROTECTED WITH TEFLON TAPES IAW SWPM 20-10-13, REV 64, AND FOUND SATISFACTORY.Apr 5, 2017 · N1217A · Boeing 767375 · Powerplant System WiringSDR UIEA2017040300496Pseu · malfunctionedGROUND CREW CALL HORN ALWAYS ON, DOES NOT TO CUT OFF WHEN AIRCRAFT IN AIR MODE, DURING EQUIPMENT COOLING LOW FLOW DETECTOR CHECK. PSEU REMOVED, REPLACED AND TESTED IAW AMM 32-09-04, REV 120A, AND FOUND SATISFACTORY.Apr 5, 2017 · N1217A · Boeing 767375 · Cabin Cooling SystemSDR UIEA2017040300498Bypass Switch · no testLEFT ENGINE FUEL FILTER BYPASS SWITCH FAILED AN OPS TEST. THE BYPASS SWITCH WAS REMOVED AND REPLACED IAW AMM 73-34-01, REV 120. OPS TESTED IAW AMM 73-34-01 REV 120, AND FOUND SATISFACTORY.Apr 5, 2017 · N1217A · Boeing 767375 · Engine Fuel Indicating SystemSDR UIEA2017040300499Blade · nickedRIGHT ENGINE, NR 31 FAN BLADE L/E FOUND WITH ONE NICK.Apr 5, 2017 · N1217A · Boeing 767375 · Turbine Engine Compressor SectionSDR UIEA2017040300500Rod End · wornRIGHT ENGINE, AT THE 10 O'CLOCK POSITION, STARTER DUCT SUPPORT ROD INBD ROD END FOUND DAMAGED.Apr 5, 2017 · N1217A · Boeing 767375 · Engine Start Valves/ControlsSDR UIEA2017040300501Drip Tray · tornRIGHT ENGINE AT THE 2 O'CLOCK POSITION, THE STRUT TO ENGINE FUEL HOSE DRIP SHIELD FOUND TORN.Apr 5, 2017 · N1217A · Boeing 767375 · Engine (Turbine/Turboprop)SDR UIEA2017040300502Seal · detachedRIGHT ENGINE FAN CASE L/E SEAL UPPER PORTION, FOUND DETACHED.Apr 5, 2017 · N1217A · Boeing 767375 · Turbine Engine Air Inlet SectionSDR UIEA2017040400517Connector · corrodedD5930J ELECTRICAL CONNECTOR FOUND CORRODED. THE CONNECTOR WAS REMOVED & REPLACED IAW SWPM 20-61-00, REV 64, AND FOUND GOOD.Apr 5, 2017 · N1217A · Boeing 767375 · Fuel System WiringSDR UIEA2017040400516Connector · corrodedELECTRICAL CONNECTOR FOUND CORRODED. THE CONNECTOR WAS REMOVED & REPLACED IAW SWPM 20-61-00, REV 64, AND FOUND SATISFACTORY.Apr 5, 2017 · N1217A · Boeing 767375 · Air Conditioning System WiringSDR UIEA2017040400515Structure · erodedNR 2 ENGINE, RT FAN COWL FOUND ERODED. THE NR 2 ENGINE FAN COWL WAS REPAIRED IAW SRM 54-22-01, REPAIR 4, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040400514Structure · erodedNR 2 ENGINE, LT FAN COWL FOUND ERODED. THE FAN COWL WAS REPAIRED IAW SRM 54-22-01, REPAIR 4, REV 103.Apr 5, 2017 · N1217A · Boeing 767375 · Nacelle/Pylon, Main FrameSDR UIEA2017040400513Cooling Fan · scratchedFWD CARGO BAY RT AIR COOLING FAN FWD FLANGE FOUND WITH DEEP SCRATCHES. REMOVED AND REPLACED THE COOLING FAN IAW AMM 21-58-06, REV 120. OPS TEST CARRIED OUT IAW AMM 21-58-06, REV 120, AND FOUND SATISFACTORY.Apr 5, 2017 · N1217A · Boeing 767375 · Air Distribution FanSDR UIEA2017040400512Bonding Jumper · dirtyLEFT OTBD MAIN FUEL TANK FUELING SHUTOFF VALVE BONDING RESISTANCE CHECK, FOUND OUT OF TOLERANCE. THE BONDING JUMPER WAS REMOVED, CLEANED & INSTALLED IAW AMM 20-11-00, REV 120. A ELECTRICAL BONDING RESISTANCE CHECK PERFORMED IAW AMM 28-22-11, REV 120, AND FOUNApr 5, 2017 · N1217A · Boeing 767375 · Fuel System WiringSDR UIEA2017040400511Bonding Jumper · dirtyLEFT INBD MAIN FUEL TANK FUELING SHUTOFF VALVE BONDING RESISTANCE CHECK FOUND OUT OF TOLERANCE. THE BONDING JUMPER WAS REMOVED, CLEANED & INSTALLED IAW AMM 20-11-00, REV 120. BONDING RESISTANCE CHECK CARRIED OUT IAW AMM 28-22-11, REV 120 AND FOUND SATISFACTApr 5, 2017 · N1217A · Boeing 767375 · Fuel System Wiring
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