Boeing 767-223
Service difficulty reports · 2,039
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 = '767223' 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 = '767223' 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 ABXA202008073160Warning Message · illuminatedL FWD WINDOW EICAS MESSAGE ON CLIMB OUT.CONTINUED TO DESTINATION. AIRCRAFT WAS GROUNDEDSDR ABXA202008053157Warning Message · illuminatedL FWD WINDOW EICAS ON CLIMB OUT. AIRCRAFT WAS GROUNDED.SDR ABXA20200710122Speaker · abnormalLOUD SQUEAL COMING FROM CAPTAIN`S. SPEAKER, UNABLE TO CONTROL. AIRCRAFT WAS GROUNDED.SDR IXXA20200519010Mount Bracket · gougedAIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-54-408-00-02 " GVI - EXTERNAL - NO. 2 NACELLE STRUT" LEFT AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 LEFT CORE COWL. REMOVED AND REPLACED LEFT AFT PRECOOLER MOUNT BRACKET IAW B767 SRM SDR ABXR2020050600026Bracket · crackedL/H AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 L/H CORE COWL. REMOVED AND REPLACED L/H AFT PRECOOLER MOUNT BRACKET IAW B767 SRM 51-40-02 PARA 9 AND IAW 47404FAB04.SDR ABXR2020050600027Tee Fitting · corrodedCORROSION ON INTERIOR "T" SECTION OF ALC DOOR 10" FROM AFT EDGE, 24" FROM TOP EDGE.REMOVED AND REPLACED INTERIOR "T" SECTION OF ALC 3RD FROM TOP USING 140T2604-3 IAW BOEING DWG# 140T2604.SDR IXXA20200519015Floor Support · corrodedAIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-572-00-01 "GVI - INTERNAL - BULK CARGO COMPARTMENT BULK FLOOR SUPPORT" F.S. 1417 HAS CORROSION ALONG LENGTH OF THE SUPPORT TOP SIDE. REMOVED AND INSTALLED "Z" BEAM IAW BOEING DWG 452T3260 REV ESDR IXXA20200519012Skin · corrodedAIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-073-00-01, ALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS. REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND
DOC 47404FAB02.SDR ABXR2020050600028Web · corrodedALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS.REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND DOC 47404FAB02SDR IXXA20200519014Skin · crackedAIRCRAGT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-53-730-00-02 "GVI - EXTERNAL - EXTERIOR SECTION 48 - RIGHT SIDE", THE FOLLOWING FINDINGS WERE NOTED: AFT RIGHT EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. REPAIRED EXTESDR IXXA20200519013Web · brokenAIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-105-00-01 "DET - FORWARD NACELLE STRUT FAIRING - NACELLE 2 (EZAP)" THE FOLLOWING FINDINGS WERE NOTED:
NUMBER 2 PYLON - WEB AND BRACKET WHICH THE NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARDSDR ABXR2020050600030Stringer Splice · corrodedSTRINGER SPLICE AT STA. 434 S31R CORRODED.REMOVED AND REPLACED CORRODED SPLICE AT STA 434 S31R IAW B767 SRM 51-40-02.SDR ABXR2020050600029Web · crackedNUMBER 2 PYLON - WEB AND BRACKET THAT NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARD END OF PYLON AT PASS THRU ARE WORN/BROKEN.REPLACE WORE BRACKET IAW B767 SRM 51-40-02, NEW WEB REPLACEMENT DONE ON AMES REA 47404FAB01 ON #2 PYLON FWD END.SDR ABXR2020050600031Skin · crackedAFT R/H EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. (VERIFIED WITH HFEC SURFACE SCAN).REPAIRED EXTERIOR FUSELAGE SKIN STA 1654.5 S3R-S8R IAW B767 SRM 53-80-01 REPAIR 4.SDR IXXA20200519020Stringer Splice · corrodedAIRCRAFT GROUNDED FOR CHECK-C24. STRINGER SPLICE AT STA. 434 S31R CORRODED. REMOVED AND REPLACED CORRODED SPLICE AT STA 434 S31R IAW B767 SRM 51-40-02.SDR IXXA20200519019Stringer · corrodedAIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD 53-460-00-01, " DET - INTERNAL - BODY BELOW FORWARD CARGO COMPARTMENT FLOOR" THE FOLLOWING FINDS WERE NOTED: CORROSION ON S36L, F.S.588. REPAIRED STRINGER IAW B767-200 SRM 53-00-03 REPAIR 2.SDR IXXA20200519017Stringer · corrodedAIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-454-00-01, "GVI - INTERNAL - BULK CARGO COMPARTMENT" THE FOLLOWING FINDINGS WERE NOTED: FLC - CORROSION ON STRINGER 32R JUST FORWARD OF STA.434. REPAIRED STRINGER 32R STA. 412-434 IAW B767 SRM SDR IXXA20200519016Stringer · corrodedAIRCRAFT GROUNDED FOR CHECK-C-24.IN COMPLIANCE OF TASK CARD ATI-53-454-00-01,"GVI - INTERNAL - BULK CARGO COMPARTMENT" FLC - CORROSION ON STRINGER 31R AT STA.412. REPAIRED STRINGER 31R STA 412-434 IAW B767 SRM 53-00-03 REPAIR 2.SDR IXXA20200519018Stringer · corrodedAIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD 53-682-00-01, "GVI - INTERNAL - FUSELAGE UPPER LOBE INTERIOR" THE FOLLOWING FINDS WERE NOTED: FOUND STRINGER CRACKED AT STATION 682 S12 LEFT. REPLACED STRINGER SECTION AT S12 L/H STA 682 AND SPLICED ASDR IXXA20200519009Slat · bulgedAIRCRAFT GROUNDED FOR C-CHECK 24. IN COMPLIANCE OF TASK CARD ATI-57-806-00-02, "GVI - ZONAL - INBOARD SLAT NO. 7" THE FOLLOWING FINDINGS WERE NOTED:
7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.SDR ABXR2020050600025Slat · corrodedNUMBER 7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.REPAIRED #7 SLAT LOWER LEADING EDGE IAW REA# 47404REA02SDR IXXA20200223002Keelbeam · corrodedDURING KEEL BEAM INSPECTION PER ATI TASK S53-052-02, EXFOLIATION CORROSION IDENTIFIED AT PANEL 149BL, SEC 45, FS 999. AIRCRAFT GROUNDED FOR REPAIR. DAMAGE MEASURED AT 1.5 X 9/16. TOTAL BLEND OUT MEASURED 2.375 (L) X 1.125 (W) AND DEEPEST BLEND POINT MEASURED SDR IXXA20191109021Unknown · faultedIN CRUISE VIA AIRLINK, CREW REPORTS POSSIBLE FUEL LEAK FROM LEFT MAIN TANK, UNABLE TO COMPENSATE, FUEL LEAK IS NOT INTERNAL, 2900LBS FUEL IN-BALANCE, UNABLE TO CONTROL WITH CROSSFEED. AS A PRECAUTIONARY MEASURE, AIR TURN BACK TO KPHX WITH AN EMERGENCY DECLARATSDR ABXA2019112202173Escape Reel · dislodgedTWO EMERGENCY DESCENT DEVICES WERE DISLODGED FROM THEIR STORAGE CONTAINER LOCATED IN THE SUPERNUMERARY COMPARTMENT CEILING. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE TWO DESCENT DEVICES WERE REPLACED WITH SERVICEABLE DESCENT DEVICES. THE CAUSE FSDR ABXA2019102517161Escape Reel · detachedONE DESCENT DEVICE WAS FOUND DISLODGED FROM ITS STORAGE CONTAINER LOCATED IN THE SUPERNUMERARY COMPARTMENT CEILING. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE DESCENT DEVICE WAS REPLACED WITH SERVICEABLE DESCENT DEVICE. THE CAUSE FOR THE DESCENT SDR ABXA201910316172Stringer · crackedCRACK IN OUTBOARD SURFACE OF STRINGER 25L AT FUSELAGE STATION 676+6. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316171Stringer · crackedCRACK IN OUTBOARD SURFACE OF STRINGER 24L AT FUSELAGE STATION 676+7.75. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316170Stringer · crackedCRACK IN OUTBOARD SURFACE OF STRINGER 23L AT FUSELAGE STATION 676. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316169Skin · crackedCRACK IN RIGHT ENGINE OUTBOARD CORE COWL LOWER LONGERON AT SECOND FROM AFT LATCH. THE CORE COWL WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316168Stringer Splice · corrodedCORROSION ON THE SPLICE FITTING AT FUSELAGE STATION 786, STRINGER 39L. THE SPLICE FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316167Structure · gougedGOUGE IN THE RIGHT PYLON AFT FAIRING CHORD BELOW THE LATCH PIN. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316166Keelbeam · corrodedCORROSION ON THE KEEL BEAM FLANGE UPPER SURFACE AT FUSELAGE STATION 820. THE KEEL BEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201910316165Attach Angle · corrodedCORROSION ON THE ATTACH ANGLE AT FUSELAGE STATION 786, RIGHT BUTT LINE 4, KEEL BEAM AREA. THE ATTACH ANGLE WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXR2019010800016Splice · corrodedRT KEEL BEAM 790 RBL 11 OB SPLICE FITTING CORRODED.SDR IXXA20180617027Connector · dirtyPREDEPARTURE CHECK: FLIGHT COMPARTMENT EMERGENCY EXIT SINGLE LIGHT INOPERATIVE. GENERAL VISUAL INSPECTION. CLEANED AND SECURED CONNECTOR. OPERATIONAL CHECK SATISFACTORY IAW B767 AMM 33-51-01. FAULT NOT DUPLICATED. NO FURTHER DEFECTS NOTED. NO PREVIOUS HISTORY SDR IXXA20180421018Autopilot Sys · malfunctionedAT FL 370, CRUISE FLIGHT AUTOPILOT EICAS OFF. RE-ENGAGED THE AUTOPILOT EICAS OFF AGAIN. TRIED LEFT AND RIGHT AUTOPILOT, AUTOPILOT OFF QUICKER. CENTER ON AGAIN STAYED ON UNTIL DESCENT, H/S USED AUTOPILOT OFF, DESCENT TO FL 280, NON RVSM HAND ROLL DIFFICUSDR IXXA20180515023Failsafe · crackedRIGHT WING FAILSAFE STRAP AT WS 955, REAMED HOLES IAW SRM 51-40-02. LOWER HOLE DAMAGE EXTENDED BEYOND ALLOWABLE LIMITS AND WAS REPAIRED IAW 47317REA01.SDR IXXA20180515022Bulkhead · dentedAFT PRESSURE BULKHEAD WAS FOUND DENTED. REPAIRED THE BULKHEAD IAW REA 47317, REA 05, REV IR.SDR IXXA20180515021Skin · bulgedBULGING FUSELAGE SKIN BS 462, STRINGER 23R. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01, REPAIR 1.SDR IXXA20180515020Seat Track · crackedFIRST OFFICER'S RIGHT FORWARD SEAT TRACK WAS CRACKED. REMOVED AND REPLACED THE SEAT TRACK IAW IAW AMM 25-11-01-822-095-001SDR IXXA20180515019Failsafe · crackedLT FAILSAFE STRAP LOWER HOLE COMMON TO THE TEE FITTING CRACKED. THE FAILSAFE WAS REPAIRED.SDR ABXA20180322044Intercostal · damagedEVIDENCE OF BURN DAMAGE ON AN INTERCOSTAL ASSEMBLY AND TWO OF THE THREE APU GENERATOR FEEDER WIRES FROM CONTACT WITH THE INTERCOSTAL AT BS 1021, RBL 35.SDR IXXA20180227010Stringer · corrodedHORIZONTAL STAB CONTROL BOX INTERNAL. CORROSION ON THE OTBD SIDE OF RIB 2L LOWER LT STRINGER 11, VERTICAL LEG FWD SIDE. INSTALLED A NEW HORIZONTAL STABILIZER STRINGER IAW SRM 31-40-02 & REA 47308 AB01. AIRCRAFT GROUNDED.SDR IXXA20180301012Bushing · corrodedLEFT LANDING GEAR H BLOCK DAMAGED BUSHINGS WITH CORROSION. REPAIRED L/H LANDING GEAR "H" BLOCK IAW REA 47308REA08 TO REMOVE CORROSION.SDR IXXA20180227011Stringer · crackedLEFT FUSELAGE STRINGER 24L CRACKED AT BS 676 AT THE STRINGER SPLICE. REMOVED THE SECTION OF THE STRINGER. FABRICATED A REPAIR STRINGER AND SPLICE DOUBLER AND INSTALLED IAW SRM 53-00-03, FIG 201, REPAIR 2. AIRCRAFT GROUNDED.SDR IXXA20180227009Strut · corrodedLEFT WING LEADING EDGE STRUT AT INBOARD END OF THE NR 5 SLAT TAI TELESCOPING DUCT CORRODED AROUND END OF DUCT. THE STRUT WAS REMOVED AND REPLACED IAW DWG 114T2201. AIRCRAFT GROUNDED.SDR IXXA20180227008Keelbeam · corrodedLEFT KEEL LOWER FLANGE UPPER SURFACE CORRODED AT BS 999. REPAIRED LOWER INBOARD KEEL FLANGE IAW SRM 53-50-12, REPAIR 1. AIRCRAFT GROUNDED.SDR ABXA20171002123Fitting · crackedCRACK IN PRESSURE DECK FITTING (PYLON FITTING) AT FUSELAGE STATION 1062. THE FITTING WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171002122Stringer · crackedCRACK IN AFT LOWER SIDE OF STRINGER 13L AT SPLICE. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20171002121Structure · corrodedCORROSION AROUND NUTPLATES AND STIFFENERS ON THE CHORD AT THE LEFT WING REAR SPAR TO TRAILING EDGE UPPER PANEL. THE CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.
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