Boeing 767-319
Service difficulty reports · 243
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 = '767319' 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 = '767319' 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 IXXA2024042001Intercostal · crackedRW LEADING EDGE INTERCOSTAL CRACKED.SDR IXXA2024041704Skin · cracked#1 ENGINE INBOARD CORE COWL OUTER SKIN CRACKED.SDR IXXA2024041701Strap · cracked#1 ENGINE AFT PYLON ATTACH STRAP CORRODED.SDR IXXA2024041302Beam · corrodedAFT LOWER CARGO DOOR BEAM CORRODED.SDR IXXA2024041301Stiffener · crackedNOSE WHEEL WELL VERTICAL CHORD.SDR IXXA2024040501Skin Panel · delaminatedVERTICAL STAB. SKIN PANEL DELAMINATED.SDR IXXA2024041703Door Frame · corrodedALC DOOR FRAME HAS 4 EACH NUTPLATE HOLES WITH CORROSIONSDR IXXA2024041602Frame · corrodedALC STATION 1197 FRAME CAP HAS CORROSION ON UNDERSIDE OF LIP STR 34R AND 33RSDR IXXA202404160001Frame · corrodedALC STATION 1197+88 FRAME CAP CORROSION UNDERSIDE OF LIP ABOVE STR 33RSDR IXXA2024041803Channel · crackedRIGHT HAND HORZ STAB PANEL 347AR MOUNTING BRACKET CRACKEDSDR IXXA2024041802Frame · corrodedALC STA 1153 RT SIDE FRAME CAP CORRODEDSDR IXXA2024041806Stringer · corrodedALC STRINGER 39R CORRODED AT STA 1219SDR IXXA2024041804Tray · crackedFLC 10R PDU TRAY CRACKEDSDR IXXA2024030303001Stringer · gougedLH WING INTERNAL STRINGER L-10 HAS MULTIPLE GOUGES ON THE FWD FACING SURFACE. REPAIRED STRINGER PER FLIGHT VEHICLE CONSULTING, INC (FVCI) EO# 24012-10 REV. B DTD 02/12/2024SDR IXXA2024041805Skin · delaminatedLEFT HORZ UPPER SKIN PANEL DELAMINATED ON INNER SURFACESDR IXXA2024041801Skin · crackedRIGHT WING FIXED L/E CRACK ABOVE OUTBOARD END OF #8 SLATSDR IXXA20230821048Unknown · unknownFIRST OFFICER'S R2 WINDOW STUCK IN OPEN POSITION. OPERATED WINDOW IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 56-11-02. WINDOW FULLY CLOSED AND SEALED.SDR IXXA20230627039Unknown · unknownPRE-DEPARTURE CREW CALL BACK, R2 WINDOW FAILS TO CLOSE.AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. SYSTEM INSPECTION IAW B767 AMM 56-11-04 ISOLATED FAULT TO DAMAGES IN WINDOW SHEAR. REMOVED AND REPLACED #2 WINDOW MECHANISM SCREW ASSEMBLY. #2 WINDOW RIG, OPESDR IXXA20230614035Unknown · unknownDURING POST FLIGHT INSPECTION, LINE MAINTENANCE IDENTIFIED EMERGENCY LIGHT "UNARMED INDICATOR" DAMAGED. KORRY SWITCH FELL APART. REMOVED AND REPLACED EMERGENCY LIGHT "UNARMED" INDICATOR LED CAP MODULE IAW B767 AMM 33-16-02. OPERATIONAL CHECK GOOD. NO ADDITIONSDR IXXA2023060702Seat Track · crackedCAPTAINS FWD IB SEAT TRACK IS CRACKED.SDR IXXA2023060701Seat Track · crackedCAPTAINS FWD OB SEAT TRACK CRACKED.SDR IXXA2023060609Skin · crackedFUSELAGE SKIN AT THE R1 DOOR LOWER AFT CORNER IS CRACKED STA 335 (FOUND WITH HFEC OPEN HOLE SCAN).SDR IXXA2023060608Skin · crackedFUSELAGE SKIN IS CRACKED AT THE L1 DOOR CUTOUT LOWER CORNER STA 335 (FOUND WITH HFEC OPEN HOLE SCAN)SDR IXXA2023060607Unknown · unknown#1 PYLON, I/B SIDE, SUPPORT ANGLE CRACKED IN HYD BAY DOOR FWD HINGE CUTOUT.SDR IXXA2023060106Unknown · crackedRH BS 1809 FWD OUTER CHORD CRACKED.SDR IXXA2023060105Skin · crackedINBOARD FWD CORNER OF #2 STRUT CRACKED.SDR IXXA2023060104Seat Track · crackedFIRST OFFICER'S FWD OUTBOARD SEAT TRACK IS CRACKED.SDR IXXA2023060103Seat Track · crackedFIRST OFFICER'S FWD INBOARD SEAT TRACK IS CRACKED.SDR IXXA2023060102Rib · crackedLEFT WING FIXED LEADING EDGE SUPPORT IS CRACKED.SDR IXXA2023060101Rib · crackedRIGHT WING LEADING EDGE RIB CRACKEDSDR IXXA2023052801Frame · damaged#2 PYLON L/E FRAME DAMAGEDSDR IXXA2024041705Skin · crackedR/H FUSELAGE SKIN AT R1 DOOR LOWER CORNER CUTOUT CRACK INDICATION STA 335, STR 20RSDR IXXA2023040311Skin · unknownREPAIR/PREVENTIVE MODIFICATION ON L/H LOWER WING SKIN AT INBOARD SEGMENT OF STRINGER L-9.5 BETWEEN WSTA 879.2 - 990.2 IAW T/C 57-767-06242.SDR IXXA2023040310Skin · unknownREPAIR/PREVENTIVE MODIFICATION ON R/H LOWER WING SKIN AT INBOARD SEGMENT OF STRINGER L-9.5 BETWEEN WSTA 879.2 - 990.2 IAW ATI AD TASK CARD ATI-57-767-06243.SDR IXXA2024041702Skin · delaminatedVERTICAL STAB LEFT LEAFING EDGE DELAMINATEDSDR IXXA2023040302Panel · gouged#2 ENGINE INBOARD THRUST REVERSER MATING SURFACES GOUGEDSDR IXXA2023040301Angle · gouged#2 ENGINE OUTBOARD THRUST REVERSER INSIDE MATING SURFACES GOUGEDSDR IXXA2023033001Thrust Reverser · gouged1 EA GOUGE ON #1 ENG. OUTBD THRUST REVERSER MEASURING 17.75" LONG X 2.15" WIDE WITH 0.039" REMAINING MATERIAL AFTER BLENDOUT.SDR IXXA2023040205Bracket · brokenSTANDOFF ANGLE BRACKET IN FWD LWR CARGO BROKENSDR IXXA2023040102Bulkhead · cracked2E CRACKS WERE DETECTED ON THE R/H FORWARD OUTER CHORD I/B FLANGE AT BS 1809.5 BULKHEAD WHILE ACCOMPLISHING INSPECTION PER T/C ATI-53-767-05111. PERMANENT REINFORCING REPAIR WAS INSTALLED PER EO NO. 53-767-5111 REV 05.SDR IXXA2023040307Fairing · delaminatedDELAMINATION ON LEFT HAND HORIZONTAL STABILIZER LOWER BEAM SPAR 240.7SDR IXXA2023040206Unknown · unknownWHILE INSTALLING FLOOR PANELS FOR MOD, DISCOVERED A PREVIOUS REPAIR SPLICE FASTENER WOULD IMPEDE THE INSTALLATION OF THE FLOOR PANEL FASTENERSDR IXXA2023040303Rib · gouged#2 ENGINE OUTBOARD THRUST REVERSER INSIDE FWD STIFFENER GOUGEDSDR IXXA2023040204Thrust Reverser · gouged#2 ENG OUTBOARD THRUST REVERSER INSIDE RIB GOUGEDSDR IXXA2023040101Support · corrodedFWD CARGO DOOR CUTOUT LWR DOOR SILL UPPER SURFACE AT APPROX STA 610 HAS CORROSION. CORROSION WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED. BLEND AT MEASUREMENTS BEFORE REPAIR: UPPER SURFACE 1=2", W=1.8", LOWER SURFACE 1=2", W= 1.3", REMAINING THICKNESS=0.061SDR IXXA2023040401Door Sill · corrodedUPON REMOVAL OF FWD CARGO #4 ROLL OUT/STOP LOCK FOUND MATTING SURFACE HAS FRETTING CORROSION.SDR IXXA2023040103Skin Panel · gougedRH WING LWR SKIN HAS SEVERAL GOUGES OUTBOARD OF PYLONSDR IXXA2023040308Unknown · corrodedAFT CARGO DOOR INNER CHORD BEAM CORRODEDSDR IXXA2023040309Splice Plate · corrodedLEFT WING FRONT SPAR LOWER CHORD UPPER SURFACE CORRODED INBOARD OF PYLON WING ATTACHMENT FITTINGSDR IXXA2023040202Skin Panel · gougedSCRATCHES/GOUGE MARKS ON RH ALT STATIC PORT.
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