Boeing 767-281
Service difficulty reports · 1,831
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 = '767281' 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 = '767281' 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 ABXA2011081898Web · crackedLT WING L/E WEB AT WS 475 AT NR 5 SLAT AREA HAS CRACKED INBD UPPER CORNER. REMOVED L/E WEB. REPAIRED IAW SRM CH 51-70-11 AND INSTALLED IAW SRM CH 51-40-2 AWG.SDR ABXA2011081897Beam · corrodedLT LEADING EDGE RIB GUSSET (BEAM) AT LES 446.10 HAS AREA OF CORROSION. REMOVED AND REPLACED NOSE BEAM IAW 767 SRM 51-40-02 AWG.SDR ABXA2011081695Channel · crackedNR 1 PYLON LOWER T/E "U" CHANNEL IS CRACKED. JUST FWD OF PANEL 437. REMOVED AND REPLACED NR 1 PYLON LOWER TRAILING EDGE "U" CHANNEL IAW B767 SRM 51-40-02.SDR ABXA2011081694Support Angle · crackedNR 1 PYLON UPPER T/E SUPPORT ANGLE CRACKED JUST FWD OF PNL 437DB. REMOVED AND REPLACED NR 1 PYLON UPPER TRAILING EDGE SUPPORT ANGLE IAW B767 SRM 51-40-02.SDR ABXA2011080393Rib · corrodedNR 4 SLAT INBD AUX TRACK OUTBD LOWER PANEL ATTACH RIB CORRODED AROUND FORWARD NUT PLATE AND ATTACH FITTING SHIM PACK CORRODED ON OUTBD SIDE. REMOVED AND REPLACED RIB AND SHIM INSTALLED WITH HILOKS IAW 767 SRM 51-40-02 AWG.SDR ABXA2011080392Beam · crackedINSIDE NUMBER 2 PYLON UNDER 447BL ACCESS A LWR SUPPORT CHANNEL (BEAM PER DRAWING 313T1380) THE WAS FOUND CRACKED AT THE FWD END. REMOVED & REPLACED LOWER INBD CHANNEL & STRIKER PLATES. REMOVED & INSTALLED NEW FASTENERS IAW 767 SRM 51-40-2 AWG.SDR ABXA2011080391Stiffener · crackedRIGHT PYLON STIFFENER CRACKED OUTBD SIDE ABOVE EXHAUST NOZZLE UNDER PNL 446 CR. REMOVED & REPLACED STIFFENER WITH NEW PART WORKED IAW 767 SRM 51-40-02. ENGINE WAS REMOVED AND AWG.SDR ABXA2011080290Sill · corrodedALC DOOR SURROUND, MAIN SILL INNER CORD IS CORRODED AT FS 1346. REPAIRED ALC DOOR SURROUND SILL AS REQUIRED, IAW REA B653-59449 AWG.SDR ABXA2011080287Bear Strap · damagedFUSELAGE REPAIR EXTNL SKIN/INTRNL BEAR STRAP INSTALL ACCOMPLISHED JOB CARD REAB653-59457-MR DUE TO DUE TO PREVIOUS LINE DAMAGE INTERIM REPAIR ABX REA B65-58940-MR; DAMAGE CUTOUT 1.375 INCH AFT OF DOOR CUTOUT AND 1.50 INCH TALL, AIRCRAFT WAS GROUNDED.SDR ABXA2011072988Failsafe · crackedTERMINATING ACTION ON RT FAIL SAFE STRAP AT ST 955. COMPLIED WITH REA B653-59436-MR.SDR ABXA2011072770Pbe · unsecureCOCKPIT PBE IS SOFT. REPLACED PBE PER IPC 25-64-57-01.SDR ABXA2011071669Light · inoperativeEXTERIOR EMERGENCY LIGHT AT LOWER AFT CORNER OF MED DOES NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS PLACED TO "ON". RELAMPED, OP CHECK GOOD.SDR ABXA2011062365Sign · inoperativeEMERGENCY EXIT THRESHOLD SIGN, LOWER PORTION DOES NOT ILLUMINATE. REF REA B633-59369, EFFECTIVE ON N797AX WORK STEP 02 REMOVED AND REPLACED L1 DOOR EMERGENCY SIGN PER 767 MAINTENANCE MANUAL, USING P/N 82000-08704 SIGN IN LIEU OF P/N 82000-08707 SIGN. VERIFIEDSDR ABXA2011062055Light · inoperativeEXTERIOR EMERGENCY EXIT LIGHT 6388 FAILS TO ILLUMINATE. REPLACED BULB OPC GOOD IAW ABX B767-2A.SDR ABXA2011061557Spar Cap · corrodedCORROSION ON UPPER CAP OF FRONT SPAR LES 452 JUST INBOARD OF "T" DUCT. CUT OUT CORRODED SECTIONS OF UPPER SPLICE PLATE AND REPAIRED IAW REA B657-593.SDR ABXA2011061467Fitting · corrodedS39R END FITTING IS CORRODED AT FS 1087. REMOVED END FITTING AT FS 1087 SR39R FOR CORROSION CLEAN UP BEYOND LIMITS. REPLACED END FITTING IAW B767 SRM 51-40-02.SDR ABXA2011061462Spar Cap · corrodedCORROSION ON FRONT SPAR UPPER CAP BEHIND NR 9 SLAT INBOARD AUX TRACK. REPAIRED SPAR IAW REA B657-59317.SDR ABXA2011061356Skin · corrodedNR 2 SLAT LEADING EDGE UPPER SURFACE HAS AREA OF CORROSION AROUND FASTENER HAD AT APPROX WS 880. REMOVED AND INSTALLED NR 2 I/B AUX TRACK IAW B767 SRM 57-43-01 AND PANEL IAW B767 SRM 51-40-02. BLENDED CORROSION FOUND TO BE OUT OF LIMITS.SDR ABXA2011060868Stiffener · crackedVERTICAL STIFFENER ON CENTER WING FRONT SPAR CRACKED AT FLOOR SUPPORT. REPAIRED DAMAGED VERTICAL STIFFENER IAW B767-200 SRM 57-10-10.SDR ABXA2011060866Stringer · crackedSTRINGER 17L HAS 3 INCH CRACK ON LOWER FLANGE AT BS 680. REPAIRED STRINGER IAW B767 SRM 53-00-03.SDR ABXA2011060659Rib · corrodedNR 11 SLAT OUTBOARD AUX TRACK ATTACH FITTING INBOARD RIB HAS CORROSION AROUND NUT PLATE. REMOVED AND REPLACED NR 11 SLAT O/B AUX TRACK I/B RIB ASSY IAW B767 SRM 51-40-02.SDR ABXA2011060458Rib · corrodedNR 12 SLAT INBOARD AUX TRACK OUTBOARD FITTING ATTACH RIB CORRODED AT NUT PLATE AND FITTING SHIM PACK CORRODED. REMOVED AND REPLACED NR 12 SLAT I/B AUX TRACK O/B RIB ASSY IAW B767 SRM 51-40-02.SDR ABXA2011060364Rib · corrodedNR 12 SLAT INBOARD AUX TRACK OUTBOARD FITTING ATTACH RIB CORRODED AT NUT PLATE. REMOVED AND REPLACED NR 12 SLAT I/B AUX TRACK I/B ATTACH RIB IAW B767 SRM 51-40-02.SDR ABXA2011060363Rib · corrodedNR 12 SLAT OUTBOARD AUX TRACK INBOARD FITTING ATTACH RIB CORRODED AT NUT PLATE. REMOVED AND REPLACED DAMAGED RIB ON NR 12 SLAT OB AUX TRACK I/B RIB IAW B767-200 SRM 51-40-02.SDR ABXA2011060360Rib · corrodedNR 11 SLAT INBOARD AUX TRACK ATTACH FITTING INBOARD RIB HAS CORROSION AROUND NUT PLATE. REMOVED AND REPLACED DAMAGED RIB ON NR 11 INBOARD AUX TRACK INBOARD RIB IAW SRM B767-300 51-40-02.SDR ABXA2011051961Rib · corrodedNR 9 SLAT INBOARD AUX TRACK ATTACH FITTING OUTBOARD RIB HAS CORROSION UNDER NUT PLATE AT FORWARD END. REMOVED AND REPLACED NR 9 SLAT I/B AUX TRACK O/B RIB ASSY IAW B767 SRM 51-40-02.SDR ABXA2011051853Harness · missingESCAPE HARNESS 3 EA MISSING FROM FLIGHT DECK. REF B767-2A ITEM NR 7D. DEFERRED: 68733 DEFERRED IAW 767 MEL 25-61-1-2. PLACARD INSTALLED. MUST BE CLEARED BY 5/27/11 CODE 11. AIRCRAFT WAS NOT GROUNDED.SDR ABXA2011051251Pbe · unserviceablePBE LOST VACUUM SEAL. DEF DI 68682 CODE 27 DEFERRED IAW GMM & B767-2A PLACARD INSTALLED.SDR ABXA2011051045Spar · damagedRT SPAR SIDE FRAME STA 955 (PICKLE FORK) LEVELING COMPOUND SHRUNK, CRACKED AND LIFTED IN SEVERAL AREAS. CORROSION IS ALSO EVIDENT IN AFT CENTER POCKET. REMOVED LEVELING COMPOUND FOUND SIDE FRAME (PICKLE FORK) CORRODED. REMOVED AND REPLACED SIDE FRAME IAW B7SDR ABXA2011051752Spar · corrodedLW FWD UPPER SPAR IS CORRODED EXTERIOR SURFACE AT LES698. REPAIRED UPPER SPAR IAW B657-59256. CORROSION 3.5" X 1.2" X .062.SDR ABXA2011042837Gasket · damagedFUEL LEAK RIGHT ENGINE. FOUND DAMAGED GASKET ON FUEL TUBE AT ENGINE DRIVEN FUEL PUMP. REPLACED GASKET IAW AMM 73-11-06-6 AND PERFORMED ENGINE T/O POWER AND LEAK CHECK IAW AMM 71-00-00-5 TEST 4. FOUND NO LEAKS AT THIS TIME. AIRCRAFT WAS GROUNDED.SDR ABXA2011041835Harness · missingONE EACH DESCENT HARNESS MISSING AT THE SUPERNUMARY AREA. DEF # 68451. DEFERRED 1 EACH DESCENT HARNESS AT THE SUPERNUMARY AREA PER MEL 25-16-1-2. PLACARD INSTALLED MBCB 4/19/11. AIRCRAFT WAS NOT GROUNDED.SDR ABXA2011051040Tee Fitting · corrodedLT T-FITTING CORRODED (FAIL SAFE STRAP AREA). REMOVED T-FITTING, DRILLED NEW REPLACEMENT FITTING IAW B767 SRM 51-40-05. NEW FITTING TO BE RE-INSTALLED PER REA B653-59247-SB.SDR ABXA2011041834Inertia Reel · missing1 EACH INERTIAL REEL DEVICE MISSING AT SUPERNUMARY AREA POSITION. DEF 68450 CODE 11 DEFERRED 1 EACH INTERTIAL DESCENT DEEVICE PER MEL 25-16-1-1. PLACARD INSTALLED MBCB 4-29-11.SDR ABXA2011041633Harness · missingCREW SERVICE AREA MISSING 1 DESCENT HARNESS. DEFERRED IAW MEL 21-61-1-2 CAR C. MBCB 4/26/11. PLACARD INSTALLED.SDR ABXA2011041532Inertia Reel · unserviceableDURING S/C FOUND NR 2 INERTIAL REEL UNSERVICEABLE. DEFERRED 68428. DEFERRED IAW MEL 15-61-1-1, CAT C, CODE 11.SDR ABXA2011041531Harness · missingONE DESCENT HARNESS MISSING FROM SUPERNUMERARY AREA. DEFERRED IAW MEL 25-61-1-2 CODE 11, CAT C. PLACARD MSG 4/25/11. AIRCRAFT WAS NOT GROUNDED.SDR ABXA2011041530Unknown · unserviceableON S/C FOUND 1 DESCENT DEVICE UNSERVICEABLE (POSITION #6) DEFERRED 68425. DEFERRED IAW MEL 25-61-1-1 CAT C CODE 11. REMOVED AND REPLACED NR 6 DESCENT DEVICE P/N 379103C-29 IN CREW SERVICE AREA IAW B767 SF MMS 25-61-03. AIRCRAFT WAS NOT GROUNDED.SDR ABXA2011041529Harness · missingONE DESCENT HARNESS MISSING FROM SUPERNUMERARY AREA. DEFERRED: 68427 DEFERRED IAW MEL 25-61-1-2, CAT C, CODE 11. MBCB 4/25/11. PLACARD CLR DI #68427. REMOVED AND REPLACED NR 6 DESCENT DEVICE P/N 379103C-29 IN FLIGHT COMPARTMENT AREA IAW B767 SF MMS 25-61-0SDR ABXA2011051042Keelbeam · corrodedRT KEEL BEAM LOWER SURFACE AT APPROX STA 1014 IS CORRODED. RT KEEL BEAM LWR SURFACE AT APPROX STA 1014 CORRODED. REMOVED AND REPAIRED IAW B767 SRM 53-50-12 FIG 201.SDR ABXA2011051047Bulkhead · canningAPB OIL CAN EXTEND BEYONDS REPAIR RS 17-18 TS1-OE. REPAIRED IAW B767-200 SRM 53-80-08 FIG 201. REPEAT INSPECTION OF CRITICAL ROW AT 2,500 CYCLE INTERVAL.SDR ABXA2011051046Bulkhead · canningAPB OIL CAN EXTENDS BEYOND REPAIR RS 18-19, TS1-OE. REPAIRED OIL CAN IAW B767-200 SRM 53-80-08 FIG 201. REPEAT INSPECTION AT 3,000 CYCLE INTERVALS.SDR ABXA2011041228Inertia Reel · defectiveWHILE CHECK EMERGENCY ESCAPE REELS AT THE MAIN ENTRY DOOR. NR 1 DEVICE DROPPED ALL THE WAY TO THE FLOOR. DEF DI 68399 CODE 11. REMOVED NR 1 ESCAPE REEL FROM MAIN ENTRY DOOR AREA PER MEL 25-61-1-1. DEFERRED PER MEL 25-61-1-1 PLAC INSTALLED. REPLACED PREVISDR ABXA2011051044Stringer · crackedS18L CRACKED UNDER SPLICE AT FS 676. REPAIRED STRINGER 18L IAW REA B653-59243-MR.SDR ABXA2011051043Stringer · crackedS17L CRACKED UNDER SPLICE AT FS 676. REPAIRED STRINGER 17L IAW REA B653-59243-MR.SDR ABXA2011051041Door · damagedRT FWD CORNER OF MEC DOOR CHAFED AND BENT. FOUND DMG TO BE GREATER THAN .100 DEPTH IAW B767-200 SRM 52-40-01 FIG 101. FABRICATED REPAIR DOUBLER FROM 2024T3. INSTALLED REPAIR DOUBLER PER 767 SRM 52-40-012 FIG 201.SDR ABXA2011051048Angle · crackedNR 2 PYLON RT SIDE ANGLE LOCATED BETWEEN AFT STRUT FAIRING AND CORE COWL HINGE HAS 2 INCH CRACK. REMOVED NR 2 PYLON RT SIDE, ANGLE AND WELD REPAIRED IAW ABX PROCESS STANDARD MANUAL 900-7-2-1. RE-INSTALLED BRACKET IAW B767-200 SRM 51-40-02.SDR ABXA2011051049Bracket · crackedINBOARD CORE COWL T-BRACKET CRACKED AT FIRST RIB O/B OF 2ND FROM AFT END HINGE. REMOVED AND REPLACED T-BRACKET ON I/B COWL AT FIRST R.B O/B OF 2ND FROM AFT HINGE IAW 767 DRAWING 314T1210.SDR ABXA2011040127Inertia Reel · defectiveINERTIA REELS NOT PROPERLY STOWED. REPLACED INERTIA REELS FROM LOCATION 1 & 4 IAW B767 MM 25-61-03-4.SDR ABXA2011040126Inertia Reel · defectiveINERTIA REELS NOT PROPERLY STOWED. REPLACED 3 INERTIA REELS PER B767 AMM 25-61-03-4 IN SUPERNUMERARY AREA. AIRCRAFT WAS NOT GROUNDED.
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