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 ABXA20171002120Attach Angle · corrodedCORROSION ON THE ATTACH ANGLE FOR PANEL 196BR IN THE RIGHT WHEEL WELL. THE ANGLE WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171002119Frame · crackedDURING ULTRASONIC INSPECTION REQUIRED BY AD 2012-22-17, A CRACK WAS FOUND IN THE INNER CHORD OF THE RIGHT SIDE FRAME BELOW FLOOR LEVEL OF THE UPPER CARGO COMPARTMENT. THE CHORD WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20171002118Keelbeam · corrodedCORROSION ON UPPER SURFACE OF LOWER INBOARD HORIZONTAL FLANGE OF THE LEFT KEEL BEAM AT BS 1007 - 1014. THE KEEL BEAM WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20170830098Carabiner · missingTHREE EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THREE NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS USDR IXXA20170803275Unknown · odorOIL SMELL THRU THE BLEED SYSTEM IN THE COCKPIT DURING CLIMB OUT. AIRCRAFT GROUNDED FOR UNSCHED MAINTENANCE AND COMPLIANCE OF CONDITIONAL INSPECTIONS IAW 05-50. WORK IN PROGRESS.SDR IXXA20170726253Escape Reel · failedEMERGENCY DESCENT DEVICE NUMBER 5 PARTIALLY EXTENDED. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW MMS 25-61-03. AIRCRAFT RELEASED TO SERVICE.SDR IXXA20170726252Escape Reel · inoperativeEMERGENCY DESCENT DEVICE NUMBER 7 IN THE SUPERNUMERARY AREA WILL NOT EXTEND. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW 25-61-03. ACFT RELEASED TO SERVICE.SDR IXXA20170724250Escape Reel · failedEMERGENCY DESCENT DEVICE NUMBER 1 IN THE SUPERNUMERARY AREA WILL NOT EXTEND. REMOVED AND REPLACED EMERGENCY DESCENT DEVICE IAW MMS 25-61-03.SDR ABXA20170308013Escape Rope · defectiveTWO DESCENT DEVICES WERE FOUND NOT PROPERLY STOWED. THE AIRPLANE WAS REMOVED FROM SERVICE. THE DESCENT DEVICES WERE REPLACED WITH SERVICEABLE DESCENT DEVICES. THE CAUSE FOR THE DESCENT DEVICES BECOMING UNSTOWED IS UNKNOWN.SDR IXXA20170228155Bracket · damagedDURING COMPLIANCE OF AD 2008-06-06: DETAILED INSPECTION AND LUBRICATION FOR THE DRIVE MECHANISM OF THE HORIZONTAL STABILIZER, FOUND LEFT HORIZONTAL STAB UPPER BODY FAIRING DOOR, INCLUDING ATTACH BRACKETS, DAMAGED. LINKAGE FOR THE HORIZONTAL STABILIZER TO BODY SDR IXXA20170228154Structure · damagedFOUND THE LEFT HORIZONTAL STAB UPPER BODY FAIRING DOOR, INCLUDING ATTACH BRACKETS, DAMAGED. REPAIRED IAW EO 53-767-5811.SDR IXXA20170201054Pump · inoperativeON APPROACH SELECTED FLAPS 1. FLAPS WENT TO 1, EICAS MESSAGE CENTER HYDRAULIC SYS PRESS ANNUNCIATED. ON STATUS PAGE C HYD QTY READ 0. DURING THE ALTERNATE FLAP EXTENSION THE CAUTION AURAL BEEPER SOUNDED AND EICAS MESSAGE APPEARED "L/E SLAT DISAGREE AND T/E FLASDR ABXA20161029152Escape Rope · unwanted deployAFTER NORMAL LANDING, THE CREW FOUND TWO INERTIAL REEL HANDLES DANGLING TO THE FLOOR OF THE SUPERNUMERARY COMPARTMENT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) UNTIL ONE OF THE DESCENT DEVICES WAS REWOUND, RESEALED, AND RESTOWED. THE OTHER INERTIAL RESDR ABXA20161011148Support · corrodedNUMBER ONE FLAP SUPPORT GOUGED AND SIGNS OF CORROSION. REPAIRED IAW REA B657-62231-MR AND JC 57500006-001. AIRCRAFT WAS GROUNDED.SDR IXXA20161007077Torque Tube · bentCREW REPORTED THE MAIN CARGO DOOR LIGHT AND WARNING HORN SOUND ANNUNICATED AS AIRCRAFT PASSED THROUGH 19,000 FT. CREW DECLARED AN EMERGENCY. QRA PROCEDURE. NO LOSS OF CABIN PRESSURIZATION. AIR TURN BACK. INSPECTION AFTER LANDING NOTED MAIN CARGO DOOR WAS CLOSESDR IXXA20161003073Angle · crackedANGLE AT BS 1843 AFT SIDE OF FIRE WALL HAS SEVERAL CRACKS AT LBL 10 AND RBL 10. REMOVED AND REPLACED ANGLE IAW SRM 51-70-11. ACFT GROUNDED.SDR IXXA20161003072Stringer · chafedRRCA HYDRAULIC HOSE INSIDE VERTICAL STABILIZER STRINGER 3R DAMAGED IN TWO PLACES. REPAIRED VERTICAL STABILIZER STRINGER IAW SRM 65-30-03. ACFT GROUNDED.SDR IXXA20161004074Support · corrodedLEFT WING TRAILING EDGE UPPER AFT PANEL SUPPORT AT BS 400 CORRODED. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-02. AIRCRAFT GROUNDEDSDR ABXA20160917145Escape Reel · unwanted deployTWO DESCENT DEVICES WERE FOUND NOT PROPERLY STOWED. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) UNTIL THE DESCENT DEVICES WERE REPLACED WITH SERVICEABLE DESCENT DEVICES. THE CAUSE FOR THE DESCENT DEVICE BECOMING UNSTOWED IS UNKNOWN.SDR IXXA20160920070Firewall · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. APU FIRE WALL FORWARD SIDE HAS SEVERAL CRACKS AT VERTICAL STIFFENERS, ACCESS 313AL. APU FIREWALL FORWARD SIDE WEB CRACKS REPAIRED IAW SRM 53-80-30, FIG 201, REPAIR 1, DWG 353T0400, IAW 47233REA01.SDR IXXA20160920069Angle · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 AFT STRUT TOP ANGLE JUST FORWARD OF MOUNTING FLANGE 437DB IS CRACKED. R & R TOP ANGLE JUST FORWARD OF MOUNT FLANGE 437 DB.SDR IXXA20161003071Structure · corrodedCORROSION ON THE LEFT WING TRAILING EDGE SUPPORT STRUCTURE UPPER CHORD JUST FORWARD OF THE NR 6 SPOILER IN BOARD FORWARD CORNER. CORROSION ON THE LEFT WIN TRAILING EDGE SUPPORT STRUCTURE UPPER CHORD FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH SRM 57-51-02. NESDR IXXA20160920065Skin · dentedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT FUSELAGE EXTERNAL SKIN HAS A DENT AT STA 1794, S37R. REPAIRED AFT FUSELAGE EXTERNAL SKIN AT STATION 1794 IAW 47233, REA 04 & SRM 53-00-01.SDR IXXA20160920067Gusset · chafedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 PYLON UNDER 431AT FORWARD CORNERS ON SKIN CHAFED. R & R FORWARD CORNER GUSSETS ON NR 1 PYLON UNDER 431AT IAW SRM 51-40-02, PARA 5 AND 7.SDR IXXA201609200066Longeron · corrodedACFT GROUNDED FOR HEAVY MAINTENANCE. FUSELAGE STA 1046-1049, & 1055, RT BUTT LINE 95 ON TOP OF OVER WING LONGERON IS CORRODED. REMOVED ANGLE AND FASTENERS, BLENDED, CORROSION REA 47233, REA 02, COMPLETED IN AREA BLENDED. REINSTALLED ANGLE AND FASTENERS IAW SDR IXXA20160920068Beam · chafedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 PYLON OTBD HYDRAULIC BAY LOWER BEAM IS CHAFED VERY THIN AT FORWARD END. R & R LOWER BEAM IN NR 1 OTBD HYDRAULIC BAY IAW SRM 51-40-02, SECTION 5, PARA B AND SECTION 7, PARA D.SDR IXXA20160818045Tee Fitting · corrodedRIGHT TEE FITTING IS CORRODED AT THE AFT LOWER BOLT HOLE. MATCH DRILLED NEW TEE FITTING IAW SRM 51-10-02. INSTALLED IAW ENGINEERING DOCUMENT 47008ORD04.SDR IXXA20160818047Strap · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. RIGHT FAILSAFE STRAP LOWER HOLE HAS CRACKED AT 10:00 POSITION, VERIFIED WITH HFEC SURFACE SCAN AND ROTARY SCAN. FAILSAFE STRAP TRIM OUT AND REPAIR ACCOMPLISHED IAW EA 47008ORD04.SDR IXXA20160818046Tee Fitting · corrodedLEFT TEE FITTING IS CORRODED AT THE AFT LOWER BOLT HOLE. A NEW TEE FITTING MATCH DRILLED IAW SRM 51-40-05. THE TEE FITTING WAS INSTALLED IAW ENGINEERING DOCUMENT 47008ORD03.SDR IXXA20160817044Failsafe · crackedLEFT FAILSAFE STRAP HAS CRACK INDICATION IN LOWER BOLT HOLE OF TRIM OUT AREA. FAILSAFE STRAP TRIM OUT AND REPAIRED IAW ENGINEERING DOCUMENT 47008ORD03.SDR IXXA201605250381Battery · dischargedFLIGHT DECK EMER FLASH LIGHT INDICATOR LED DOES NOT FLASH. R & R EMER FLASHLIGHT BATTERY. OPERATIONAL CHECKED SATISFACTORY. FAULT NOT DUPLICATED.SDR IXXA20160512026Skin · corrodedCORROSION LT UPPER WING AT STATION 1075.2, TEMPORARY REPAIR OF LT WING SKIN AT STATION 1090 IAW 46971REA28. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C CHECK IAW 46971REA28 STEP 9 REFERENCE ATI COI 47257.SDR IXXA20160519036Frame · corrodedLEFT FRAME 883.15 IS CRACKED ON AFT LOWER SIDE, AT STUD BEAM BELOW CARGO DECK. REPAIRED IAW EO 53-767-4907.SDR IXXA20160517029Floorbeam · corrodedCORROSION UNDER NUTPLATE ON LOWER FLOORBEAM CHORD, AT STATION 1263, RBL 26 IN AREA OF PDU ATTACH BOLT. R & R FLOORBEAM IAW AMM 25-53-01, SRM 51-40-02, 51-40-03 & 51-20-01. BEAM FABRICATED IAW REA 47206FAB01.SDR IXXA20160517032Door Sill · corrodedSTATION 642, STRINGER 32R, DOOR SILL CHORD CORRODED. BLENDED CORROSION ON DOOR SILL CHORD IAW SRM 53-00-15. REPAIRED LOWER SILL OUTER CHORD IAW SRM 51-70-12.SDR IXXA20160519035Support Beam · corrodedRIGHT WING NR 8 FLAP SUPPORT, 1-2-3 BEAM HAS CORROSION IN TWO EA FASTENERS. REPAIRED RT WING NR 8 FLAP SUPPORT IAW REA 47206REA03.SDR IXXA20160519034Support Beam · corrodedRIGHT WING NR 7 FLAP SUPPORT, 1-2-3 BEAM HAS CORROSION IN ONE EACH FASTENER. REPAIRED RT WING NR 7 FLAP SUPPORT, 1-2-3 BEAM IAW REA 47206REA02.SDR IXXA20160519033Support · corrodedRIGHT WING OTBD FLAP NR 8 SUPPORT, OTBD RIB ACTUATOR BORE HAS EDGE PITTING AT 3 LOCATIONS ON THE INBD BORE & 1 LOCATION ON THE OTBD BORE. RT WING OTBD FLAP NR 8 SUPPORT BORE REPAIRED IAW REQUEST FOR ENGINEERING DOCUMENT 47206REA04.SDR IXXA20160517031Stringer · corrodedSTATION 752, STRINGER 34L, CORRODED AT DOME NUT. REPAIRED STRINGER 34L IAW SRM 53-00-03.SDR IXXA20160517030Structure · crackedNUMBER 1 PYLON OTBD HYD BAY DOOR, ACCESS CUT OUT FWD LOWER CORNER STRUCTURE, INSIDE CRACKED & WORN. R & R NR 1 PYLON OTBD HYD BAY DOOR , ACCESS CUT OUT FWD LOWER CHORD IAW SRM 51-40-02 & DWG 313T1300.SDR CA160126011Control Valve · cracked(CAN) DURING PRE-DEPARTURE CHECK A HYDRAULIC LEAK WAS NOTED COMING FROM THE RT MLG ANTI-SKID VALVE MODULE ASSY, CLOSER INVESTIGATION FOUND THE NR 3 ANTI-SKID CONTROL VALVE ON THE MODULE HAD A CRACKED HOUSING. THE NR 3 ANTI-SKID CONTROL VALVE WAS REPLACED IAW SDR CA151104008Bearing · overheated(CAN) INITIAL INDICATION WAS A STATUS MESSAGE, C HYD SYS MAINT. A CHECK OF THE HYDRAULIC PRESSURES REVEALED THE CENTER HYD SYS WAS BELOW NORMAL PRESSURE, 2010 PSI. QUANTITIES ALL OK. WITHIN A FEW MINUTES THERE WAS AN EICAS MESSAGE OF, C1 HYD PRESSURE, FOLLOWSDR ABXA20151014189Skin · corrodedCORROSION ON LT FUSELAGE SKIN, STATION 955 C/T FAILSAFE TRIM OUT AREA GOING FWD UNDER FAILSAFE STRAP. FAIL SAFE REMOVED ON EA 53500013-008. REMOVED ALL CORROSION, NDT TESTED, NO DEFECTS NOTED. COMPLIED WITH EA 53500013-004 & REA B657-61768MR. REFERENCE EASDR ABXA20151013173Skin · corrodedRIGHT STATION 18.09 PREVIOUS REPAIR DOUBLER, BETWEEN STRINGERS 9RT & 10RT. REQUEST ENGINEERING INSTRUCTIONS. REMOVED DOUBLER, CLEANED HOLES TO LEVEL 3, PERFORMED HFEC ON HOLES & AREA AROUND HOLES. PERFORMED GVI OF 22" AROUND 1809 REPAIR. FABRICATED RT DOUBSDR ABXA20151012175Frame · crackedRIGHT FRAME INNER CHORD AT STATION 883.5, RBL 89 HAS A .250 CRACK IN TRANSITION RADIUS. REPAIRED CHORD IAW EA 53000050-101. CRACKED .50, PN 691T0003-44, PART NAME CHORD RT INNER, SN N/A, FS & BS LOCATION FROM 883.5 STRINGER & WS LOCATION RBL 89. ACFT WAS GNSDR ABXA20151007190Tee Fitting · corrodedUPON CURSORY INSPECTION, FOUND CORROSION WITHIN AREA UNDER THIRD INBD HEAT SHIELD PANEL AT LOWER AFT PYLON AREA, APPROX NAC STATION 400. R & R CORRODED T FITTING IAW BCSF SRM 51-40-02 & DWG 313T1355. SDR INFO, CORRODED LEVEL 2, PN 313T1355-128, PART NAME T FSDR ABXA20151003188Failsafe · crackedLEFT STATION 955, FAIL SAFE STRAP HAS .125 CRACK APPROX 2:00 POSITION AT THE BOTTOM FASTENER HOLE. LT FAIL SAFE STRAP IS BEING REPLACED. NEW FAIL SAFE STRAP PN 145T2524U21 TO BE INSTALLED ON EA53500013-008. SDR INFO CRACKED .125", PN 145T2524, PART NAME FAISDR ABXA20151002165Stiffener · corrodedLEFT WW AFT SPAR BULKHEAD FS 955, LBL 9, INBD VERTICAL ANGLE HAS TOOLING MARKS ON INBD SIDE IN NUMEROUS PLACES. BLENDED TOOLING MARKS ON REAR SPAR STIFFENER IAW REA 66740-MR. SDR INFO CORRODED, PN 111T 1005-1, SN N/A, PART NAME STIFFENER, LOCATION FROM STATISDR ABXA20151001170Longeron · corrodedCORROSION ON UPPER SIDE OF OVERWING LONGERON IN UPPER FWD OTBD CORNER OF RT WW, AROUND FASTENERS & ON FASTENER HEADS FROM FS 975 - 985. REMOVED CORROSION ORIGINAL .080, REMOVED .012, REMAINING .068 IAW REA B653-61757-MR RFTS E-46344 REV IR DATE 9 23 15. SDR SDR ABXA20151001169Longeron · corrodedCORROSION ON UPPER SIDE OF OVERWING LONGERON IN UPPER FWD OTBD CORNER OF RT WW FROM FS 965 - 975. REMOVED CORROSION ORIGINAL .080, REMOVED .012, REMAINING .068 IAW REA B653-61757-MR RFTS E-46344 REV IR DATE 9 23 15. SDR INFO CORRODED LEVEL 2, PN 145T8800-20,
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