Boeing 767-31B
Service difficulty reports · 617
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 = '76731B' 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 = '76731B' 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 UIEA2017070701124Support Bracket · wornNR 2 ENGINE, LT CORE COWL HOLD OPEN ROD END SUPPORT BRACKET FOUND WORN. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070701125Rub Strip · damagedNR 2 ENGINE, LT CORE COWL EXTERIOR FWD SURFACE WEAR STRIP FOUND DAMAGED. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070701126Rivet · shearedNR 2 ENGINE, LEFT CORE COWL FAIRING EXTERIOR SURFACE AFT SECTION FOUND RIVETS SHEARED. THE SHEARED RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070701127Structure · scratchedNR 2 ENGINE, LT CORE COWL EXTERIOR SURFACE FOUND SCRATCHED. THE SCRATCH WAS SMOOTHED AND FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, DETAIL 3, REV 104.SDR UIEA2017070701128Door · damagedNR 2 ENGINE, LEFT CORE COWL FLIPPER DOOR FOUND DAMAGED. THE DOOR WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070701129Seal · wornNR 2 ENGINE, LEFT CORE COWL AFT UPPER EDGE STRIP SEAL FOUND WORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070801130Longeron · crackedNR 2 ENGINE, LT CORE COWL MOST AFT LONGERON FOUND CRACKED. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070601116Rivet · shearedNR 1 ENGINE, LEFT CORE COWL UPPER AFT EDGE WEAR STRIP ATTACHING RIVET FOUND SHEARED. THE SHEARED RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070101087Channel · wornNR 1 ENGINE, LT CORE COWL MOST AFT HAT CHANNEL TWO EXISTING REPAIRS FOUND WORN. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070101083Frame · wornNR 2 ENGINE, LT CORE COWL SECOND ZEE FRAME FROM FWD FOUND EXISTING REPAIR WORN. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062001040Bracket · wornNR 1 ENGINE, RT CORE COWL FAIRING MOST FWD END BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062001042Fairing · wornNR 1 ENGINE, RT CORE COWL FAIRING SKIN INTERIOR SURFACE FOUND WORN. ACCOMPLISHED A FAIRING SKIN REPAIR IAW SRM 54-45-01-2R-11, FIG 202, DETAIL 3, REV 104.SDR UIEA2017062001044Rub Strip · wornNR 1 ENGINE, LT CORE COWL FAIRING INTERIOR SURFACE AFT UPPER SECTION OF RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062001045Skin · wornNR 1 ENGINE, LEFT CORE COWL FAIRING SKIN INTERIOR SURFACE FOUND WORN LOCATED AT UPPER AFT CUT-OUT SECTION. THE SKIN WAS REPAIRED IAW SRM 54-42-01-2R-5, REPAIR 5, FIG 202, DETAIL 3, REV 104.SDR UIEA2017062001046Stop · wornNR 1 ENGINE LEFT CORE COWL ATTACH STOP FOUND WORN. THE STOP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062201049Rub Strip · wornNR 2 ENGINE LEFT CORE COWL INTERIOR SURFACE AFT UPPER SECTION RUB STRIP FOUND WORN. THE SECTION OF THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062301056Seal · damagedNR 1 ENGINE RIGHT CORE COWL FAIRING FLIPPER DOOR SEAL FOUND DAMAGED. THE DOOR SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062301057Rub Strip · wornNR 1 ENGINE RIGHT CORE COWL UPPER AFT EDGE WEAR STRIP FOUND WORN. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062301058Angle · crackedNR 1 ENGINE LEFT CORE COWL FAIRING INTERIOR SURFACE MOST AFT ANGLE FOUND CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062301059Seal · damagedNR 1 ENGINE LEFT CORE COWL FAIRING AFT UPPER EDGE STRIP SEAL FOUND DAMAGED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070101080Frame · chafedNR 2 ENGINE LEFT CORE COWL MOST AFT FRAME FOUND A CHAFED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017061201003Rub Strip · wornNR 1 ENGINE NOSE COWL AT THE 1 TO 3 O'CLOCK POSITIONS, FOUND THE RUB STRIP WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017061201002Rub Strip · wornNR 1 ENGINE NOSE COWL AT THE 3 TO 5 O'CLOCK POSITIONS FOUND THE RUB STRIP WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017061201001Rub Strip · wornNR 1 ENGINE NOSE COWL AT 6 O'CLOCK POSITION FOUND RUB STRIP WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017061200998Bracket · wornNR 2 ENGINE LT FAN COWL PRESSURE RELIEF DOOR ASSY FWD LANYARD SUPPORT BRACKET FOUND WORN. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017060800989Skin · dentedRIGHT AFT UPPER FUSELAGE APPROX BETWEEN BS 1197+22 TO 1197+44, APPROXIMATELY 3 INCHES ABOVE STRINGER 19R, FOUND A DENT. REPAIRED IAW SRM 53-00-01-2R-14, REPAIR 14, FIG 201, REV 104.SDR UIEA2017071301194Skin · damagedFUSELAGE SKIN DAMAGED BOTTOM SIDE BS 137 AND RBL 10.5. ACCOMPLISHED A REPAIR IAW EO 6753A513, REV O, PART 1. NO CRACK INDICATIONS NOTED AT THIS TIME IAW NDT M PART 6-51-00-01.SDR UIEA2017062701069Warning Message · illuminatedMAIN CARGO DOOR MESSAGE CLIMBING THROUGH 14000'FT, ATB.SDR UIEA2017061200999Valve · unknownCOCKPIT TRIM VALVE INDICATION, BOTH DIGITAL IN ECS MAINTENANCES PAGE & MANUAL ON OVERHEAD PANEL. WHEN EVER IT CASSES THE 70 TOOLEDDS THE FULL CLOSE POS . IN START TO FLUCTUTE FROM CLOSE TO 0.70 WORKS OK. TEST FLIGHT(<DIV>COCKPIT TRIM AIR VALVE REPLACED SDR UIEA2017061201000Warning Light · false activationAFTER 30 MINUTES OF FLIGHT, THE RT FWD FUEL PRESSURE MESSAGE ILLUMINATED AND THE PRESSURE LIGHT IN BOTTON. TEST FLIGHT. PERFORMED TROUBLESHOOTING IAW FIM 28-22, FT819 FOUND K107 , AND THE RT FWD RELAY OPEN AND PERFORMED A RESET. PERFORMED FIM FIG 119 FT 83SDR UIEA2017060800987Gasket · missingFWD CARGO BAY EQUIPMENT COOLING SYSTEM, 5 GASKETS ARE MISSING. NEW GASKETS INSTALLED IAW MM 21-58-00.SDR UIEA2017060800952Keelbeam · corrodedFUSELAGE KEEL BEAM LBL 9.50 AND RBL 9.50, FROM BS 676 TO 1307 AT ANCHOR NUTS ARE CORRODED.SDR UIEA2017060800953Sleeve · corrodedRT AND LT BOOST PUMP SLEEVES ARE CORRODED. SLEEVES REPLACED IAW MM 28-22-05.SDR UIEA2017060800954Bonding · dirtyOVERRIDE, JETTISON PUMP AT LT WING HIGH BONDING RESISTANCE. BONDING CLEANED &TREATED, CHECKED AND FOUND OK IAW MM 20-41-00.SDR UIEA2017060800955Bonding · dirtyENGINE FUEL SHUTOFF VALVE ACTUATOR AT LT WING TANK, BONDING HIGH RESISTANCE. THE BONDING WAS REMOVED CLEANED REINSTALLED CHECKED AND FOUND OK IAW MM 20-41-00SDR UIEA2017060800956Tube · corrodedAPU DRAIN MAST TUBE CORRODED. THE DRAIN MAST TUBE WAS REPLACED IAW MM 49-16-00.SDR UIEA2017060800957Bolt · corrodedAPU ISOLATOR VIBRATION BOLTS CORRODED. VIBRATION BOLTS REPLACED IAW MM 49-11-01.SDR UIEA2017060800958Clamp · corrodedAPU LT AIR SURGE BLEED DUCT CLAMPS ARE CORRODED. APU SURGE BLEED DUCT CLAMP REPLACED IAW MM 49-53-01.SDR UIEA2017060800959Structure · delaminatedNR 2 ENGINE, FAN COWL INNER SIDE IS DELAMINATED. REPLACED IAW MM 71-11-04.SDR UIEA2017060800962Strip · brokenNR 1 ENGINE, INLET COWL AFT BULKHEAD WEARSTRIP BROKEN AT 6 O'CLOCK , AND 9 O'CLOCK POSITIONS. THE WEARSTRIP WAS REPLACED IAW MM 71-11-04.SDR UIEA2017060800961Support · chafedNR 2 ENGINE, LT FAN COWL AFT OPEN ROD SUPPORT CHAFED. THE SUPPORT WAS REPLACED IAW MM 71-11-11-201.SDR UIEA2017060800963Latch · corrodedNR 2 ENGINE, FAN COWL LATCHES CORRODED. THE LATCHES WERE CLEANED IAW MM 20-30-03.SDR UIEA2017060800965Seal · tornNR 2 ENGINE, RT FAN COWL HAS A TORN SEAL. THE FAN COWL ASSY WAS REPLACED IAW MM 71-11-04.SDR UIEA2017060800967Seal · tornNR 2 ENGINE RT FAN COWL HAD A TORN SEAL. THE SEAL REPLACED IAW MM 71-11-04.SDR UIEA2017060800973Rub Strip · looseNR 2 ENGINE INLET COWL AFT BULKHEAD RUBSTRIP HAS RIVETS MISSING AT 6 O'CLOCK POSITION. REPLACED THE RIVETS IAW MM 71-11-04.SDR UIEA2017060800974Shutoff Valve · no testNR 1 ENGINE PRSOV FAILED TEST. THE PRSOV WAS REPLACED IAW MM 36-11-09.SDR UIEA2017060800975Fire Loop · damagedNR 2 ENGINE EICAS MESSAGE FOR THE NR 2 FIRE LOOP. THE FIRE LOOP WAS REPLACED IAW MM 26-11-01.SDR UIEA2017060800976Restraint · damagedLEFT PACK FLEXIBLE TIE RESTRAINT IS DAMAGED. LT PACK RESTRAINT TIE REPLACED IAW MM 21-51-00.SDR UIEA2017060800979Bracket · looseNR 1 ENGINE, LT CORE COWL HOLD OPEN BRACKET WORN. BRACKET FASTENERS REPLACED IAW MM 26-23-02.SDR UIEA2017060800980Skin · scratchedNR 2 ENGINE, RT CORE COWL SCRATCHED IN THE MIDDLE. SCRATCH SMOOTHED IAW SRM 51-10-02, NDT CHECKED IAW D634T301, PART 6 51-00-19, NO CRACKS FOUND. THICKNESS MEASURED IAW D 634T301, PART 4 51-00-10, & FOUND WITH IN LIMITS IAW SRM 54-42-01.
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