N749AX
Service difficulty reports · 127
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N749AX' AND registry_match = 'registration' 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 n_number = 'N749AX' AND registry_match = 'registration' 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 ABXA20230612117Unknown · unknownEXPERIENCED LOSS OF PRESSURIZATION DURING DESCENT INTO KPHX. DESCENDING THROUGH FL270 VIA THE EAGUL6 ARRIVAL A CABIN ALT WARNING OCCURRED. OXYGEN MASKS WERE DONNED AND CHECKLIST WAS ACCOMPLISHED. PRESSURIZATION WAS REGAINED AND FLIGHT RESUMED NORMALLY. NO OTHESDR ABXA2023032035Actuator · failedEICAS TE FLAP DISAGREE WHEN FLAPS SELECTED TO 5 DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED BYPASS VALVE ROTARY ACTUATOR IAW B767 AMM 27-51-32. OPS CHK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2023013016Regulator Valve · defectiveLEFT ENGINE BLEED OFF, 0 DUCT PRESSURE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LEFT HPSOV IAW B767 AMM 36-11-07 . OPS AND BITE CHECK GOOD. ACCOMPLISHED BLEED SHIFT CHECK IAW B767 AMM 36-11-00, CHECKS GSDR ABXA20230104103Autobrake Sys · faultedAUTO BRAKE WILL NOT SET IN RTO AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED AUOBRAKES IAW MEL 32-42-1A, MX PROCEDUES C/W. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2023050986Skin · misrepairedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MISDRILLED WAS REPORTED COMMON TO FUSELAGE UPPER SKIN P/N 143T3111-1 LOCATED AT STA 705 AND S-1R. THE FINAL HOLE SIZE IS 0.323”. THEREFORE FOUND OUT OF LIMITS IAW 767-200 SRM 53-00-01 ALLOWABLE DAMAGE. FLIGHT VEHICLSDR ABXA20221122135None · noneDURING AIRCRAFT C-CHECK, CORROSION WAS FOUND IN THE BETWEEN BS 1307 & 1285, S36L. THERE IS A PREVIOUS EXTERNAL REPAIR DOUBLER AT BS 1300, S36L WAS REMOVED FOR DISPLACEMENT OF THE SKIN P/N 146T3211-1. THE MINIMUM REMAINING THICKNESS IS 0.045” THEREFORE IS OUTSDR ABXA20221122134Tear Strap · corrodedDURING AIRCRAFT C-CHECK, CORROSION WAS FOUND ON SURFACE OF THE TEAR STRAP INSTALLED ON SKIN. THE CORROSION WAS LOCATED AT BS 1285 AND BETWEEN S32L & S33L. NO ALLOWABLE DAMAGED NOR REPAIR WERE FOUND IN SRM. PERMANENT REPAIR INSTRUCTIONS WERE APPROVED. AIRCRAFSDR ABXA20221121132Cargo Track · corrodedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION COMMON TO MAIN DECK FLOOR CARGO TRACK P/N 368-53-16-94451-201AT STA 1600 AND LBL 11, THE ORIGINAL THICKNESS FOUND TO BE .071'', NO MATERIAL REMAINING CORROSION WENT ALL THE WAY THRU, TSDR ABXA2023050984Cargo Track · corrodedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION COMMON TO MAIN DECK FLOOR CARGO TRACK P/N 368-53-16-94451-201AT STA 1480 AND LBL 11, THE ORIGINAL THICKNESS FOUND TO BE .071'', NO MATERIAL REMAINING CORROSION WENT ALL THE WAY THRU, TSDR ABXA2023050985Failsafe · corrodedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED AN AREAS OF CORROSION ON THE UPPER SURFACE OF THE FAIL-SAFE STRAP (P/N 143T15910-2) INSTALLED ON THE FORWARD FRAME OF THE FORWARD LOWER CARGO DOOR JAMB. THE CORROSION WAS LOCATED AT STATION 53SDR ABXA20221121131Cargo Track · corrodedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION COMMON TO MAIN DECK FLOOR CARGO TRACK P/N 368-53-16-94336-201 AT STA 1087 AND LBL 77.5, THE ORIGINAL THICKNESS FOUND TO BE .071'', MATERIAL REMAINING AT DEEPEST POINT IS .055'', MATERISDR ABXA20221122136Shear Panel · corrodedDURING AIRCRAFT C-CHECK, CORROSION ON SHEAR PANEL PN 368-53-16-94372-201 BETWEEN STA 1480 AND 1502 AND LBL 76. THE ORIGINAL THICKNESS FOUND TO BE .073'', MATERIAL REMAINING AT DEEPEST POINT IS .026'', MATERIAL LOSS IS .047'', THERE IS NO ALLOWABLE DAMAGE AND/OSDR ABXA20221122137Floorbeam · corrodedDURING AIRCRAFT C-CHECK, MAINTENANCE REPORTED CORROSION COMMON TO FLOORBEAM P/N 368-53-16-94157-201 AT STA 1109 AND BL0. CORROSION WAS FOUND IN FLOORBEAM LOWER CHORD, THE ORIGINAL THICKNESS FOUND TO BE .600'', MATERIAL REMAINING AT DEEPEST POINT IS .200'', MASDR ABXA20221121133Stringer · corrodedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORT CORROSION WAS FOUND ON THE BOTTOM SURFACE OF THE HORIZONTAL FLANGE AND INBOARD SURFACE OF THE UPPER VERTICAL FLANGE ON THE RIGHT WHEEL WELL LONGERON OUTER CHORD PN: 145T8806-2 BETWEEN STA 1050-106SDR ABXA2022080994Warning Message · false activationSTATUS MESSAGE L FLT CONT ELEC. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE CW FIM 27-09 FAULT TREE 805. OPS CHECK GOOD AT THIS TIME. AC DOWNGRADED TO CAT I. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2022080692Warning Message · illuminatedRT BLEED VAL EICAS ILLUMINATED ON TAKE OFF, ABORTED TAKE OFF RT BLEED OVERHEAD ANNUNCIATOR ILLUM. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED RT. HPSOV SYSYEM IAW MEL 36-11-2-1. MAINTENANCE PROCEDURES C/W. AIRCRAFT RETURNED TO SERVISDR 2022FA0000301None · noneWARNING ELEX MESSAGE DURING TAXI. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. TROUBLESHOT WARN ELEX MSG TO BROKEN WIRE AT FO'S STICK SHAKER CONNECTOR D1399 PIN A. ACCOMPLISHED SPLICE REPAIR PER SWPM 20-10-13 ALL CHECKS NORMAL IAW AMM 2732-00 AND WDM 27-32-21 ASDR ABXA2022011207None · noneLEFT ENG FUEL VALVE FAILED TO OPEN DURING ENG START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE, MAINTENANCE RESEATED & CLEANED CONNECTOR @ #1 ENG FUEL ACT.OP'S CHK OK PER AMM 73-00-00 NIL DEFFECT NOTED. AICRAFT RETURNED TO SERVICE.SDR ABXA2022010705None · noneL ENG WOULD NOT START, L ENG FUEL VALVE EICAS MESSAGE DISPLAYED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE CYCLED FUEL CONTROL SWITCH, LEFT ENGINE VALVE CYCLED NORMALLY. ACCOMPLISHED LEFT ENGINE IDLE RUN IAW B767 AMM 71-00-00, NO DEFECTS.SDR ABXA20211121120None · noneRIGHT HYD ELECTRIC DEMAND PUMP EICAS MESSAGE AFER ENGINES START. AIRCRAFT BACK TO BLOCK AND GROUNED BY MAINTENANCE. MAINTENANCE INPECTED RIGHT HYDRAULIC SYSTEM AND FOUND NO DEFECTS. PREFORMED OPERATION CHECK OF THE RIGHT HYD DEMAND PUMP OPS CHECK GOOD IAW AMSDR ABXA202109098089Warning Message · illuminatedUPON INITIAL APPLICATION OF T/O POWER, GROUND SPEED WAS BELOW 10KTS. L HYD DEM PUMP EICAS MESSAGE ILLUMINATED. PER QRH, THE PUMP SWITCH WAS PLACED "ON" LIGHT REMAINED OUT. TAKE OFF WAS ABORTED AND AIRCRAFT EXITED RUNWAY TO TAXIWAY.CREW CONTACTED MAINTENANCE COSDR ABXA202108053069Control Panel · faultedON TAKE OFF - C HYD PRIM 1 ON EICAS. ABORTED TAKE OFF AND RETURNED TO BLOCK. MAINTENANCE GROUNDED AIRCRAFT. REMOVED & REPLACED HYD CONTROL PANEL IAW B767 AMM 29-11-40. AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA2021630063Hydraulic System · lowAFTER PUSH BACK CENTER HYD. QTY. UNSTABLE AND LOW. AIRCRAFT RETURNED BACK TO BLOCK AND GROUNDED BY MAINTENACE. CENTER HYD. SYSTEM DEFERRED PER MEL. AIRCRAFT RELEASED FOR FLIGHTSDR ABXA2021430029Bleed Valve · intermittentAFTER ENGINE START EICAS MSG "L ENG BLEED VAL" AND L DISCRETE LIGHT " BLEED" ILLUMINATED.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED DEFERRAL PROCEDURES IAW MEL FOR LEFT HIGH PRESSURE SHUT OFF REGULATING VALVE. AIRCRAFT RELEASED BSDR ABXA20200803206Antenna · brokenTIP OF LOWER ATC ANTENNA FOUND BROKEN OFF. DEFERRED BY MAINTENANCE PROCEDURES. AIRCRAFT DEPARTED AND CREW HAD AN ATC FAULT MESSAGE. AIRCRAFT RETURN TO BLOCK AND WAS GROUNDED. REMOVED AND REPLACED ATCD ANTENNA, IAW AMM 34-53-03. AIRCRAFT RELEASED FOR FLIGHSDR ABXA20200803198Warning Message · false activationRT REV ISOLATION VALVE EICAS MESSAGE AFTER ENGINE START. AIRCRAFT RETURNED TO GATE, AIRCRAFT WAS GROUNDED. MAINTENANCE INVESTIGATED PROBLEM. OPERATIONAL CHECK OF RT REVERSER GOOD, IAW AMM 78-31-00. REV CYCLED 3X TIMES WITH NO MESSAGES. AIRCRAFT RELEASED FSDR ABXA20200803196Warning Message · false activationSTAB TRIM EICAS AND DISCRETE LIGHT ILLUMINATED AFTER SETTING STAB TRIM DURING AFTER START CHECKLIST. T/S STAB TRIM, PER FIM 27-48 FT 809. NO FAULT NOTED, SYSTEM GOOD, PER B767 AMM 27-41-00 OPS TEST (HOR.STAB.TRIM CONTROL SYS) NO FAULTS NOTED. SYSTEM OPS CHESDR ABXA20200803184Warning Message · illuminatedCTR HYD SYS PRESS EICAS MESSAGE ILLUMINATED. MAINTENANCE SUSPECT AUTO FUNCTION OF ADP DID NOT COME ON. AIRCRAFT BACK TO GATE AND AIRCRAFT GROUNDED UNTIL MAINTENANCE DEFERRAL WAS COMPLETED.SDR ABXA20200803179Pump · malfunctionedC HYD SYS PRESS CAUTION EICAS MESSAGE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED FOR MAINTENANCE. ADP DEFERRED AND AIRCRAFT RETURNED TO SERVICE. DI 17491 ADP CONTROLLER AUTO FUNCTION MEL 29-11-4-1.SDR ABXA20200721144Stringer · corrodedSTA 1190 SR 39L AFT CARGO, REPLACED DAMAGED STRINGER. AIRCRAFT WAS GROUNDED.SDR ABXA20200721136Frame · corrodedBS 883.5 LBL 89. REPAIR FRAME WEB, INNER CHORD FREEZE PLUG. AIRCRAFT WAS GROUNDED. REPAIRED FRAME WEB, INNER CHORD, SPLICE. AIRCRAFT WAS GROUNDED.SDR ABXA20200721135Frame · corrodedBS 883.5, LBL 89. REPAIR FRAME WEB, INNER CHORD FREEZE PLUG. AIRCRAFT WAS GROUNDED.SDR ABXA20200721142Flap Track · corroded#2 FLAP TRACK ASSY HOLE REPAIR. AIRCRAFT WAS GROUNDED.SDR ABXA20200721143Stringer · corrodedSTA 1085 SR 30L. CORROSION REPAIR ON STRINGER LOWER CHORD. AIRCRAFT WAS GROUNDED.SDR ABXA20200721141Skin · corrodedSTA 1080 STR 30L. BLEND OUT FUSELAGE SKIN INTERNAL. AIRCRAFT WAS GROUNDED.SDR ABXA20200721134Structure · crackedBS 859.5, LBL 89 REPAIRED CRACKED INNER CHORD. AIRCRAFT WAS GROUNDED.SDR ABXA20200721145Keelbeam · corrodedSTA 1039 LBL 15 CORROSION UNDER KEEL BEAM CHORD REPAIRED. AIRCRAFT WAS GROUNDED.SDR ABXA20200721130Angle · crackedBS 1725.5 CRACKED ANGLE ABOVE APU INLET. AIRCRAFT WAS GROUNDED.SDR ABXA20200721140Skin · corrodedSTA 1186 SR 38R, FUSELAGE SKIN DOUBLER REPAIR. AIRCRAFT WAS GROUNDED.SDR ABXA20200721138Skin · damagedBS 1330 SR 33L FUSELAGE SKIN DOUBLER REPAIR. AIRCRAFT WAS GROUNDED.SDR ABXA20200721137Structure · corrodedSTA 1065 SR 30L LOWER CHORD TRIM OUT REPAIR. AIRCRAFT WAS GROUNDED.SDR ABXA20200721139Skin · damagedSTA 1239 SR39L-39R REMOVED NICK FROM INTERNAL SKIN AREA. AIRCRAFT WAS GROUNDED.SDR ABXA20200721131Support Fitting · corrodedSTA 1091 SR29L-30L, REPLACED THE CORRODED SUPPRT FITTING. AIRCRAFT WAS GROUNDED.SDR ABXA20200721133Angle · crackedBS 1725.5 REPLACED CRACKED ANGLE BELOW APU INLET. AIRCRAFT WAS GROUNDED.SDR ABXA20200721132Beam · corrodedWS 897, REPLACED CORRODED NOSE BEAM-LH WING LE BEHIND #2 SLAT. AIRCRAFT WAS GROUNDED.SDR ABXA202005153061Guide Vane · damaged#1 ENGINE 12 OCLOCK POSITION EXIT GUIDE VANE FAIRING DAMAGED. AIRCRAFT WAS GROUNDED.SDR ABXA201912106177Eec · malfunctionedTHE RIGHT ENGINE DID NOT REACH CLIMB POWER AT HIGH ALTITUDE (FL260) WITH THE ELECTRONIC ENGINE CONTROL ON. THE ENGINE ONLY PRODUCED 105% WITH THE THRUST LEVER FULL FORWARD. THRUST LEVERS WERE SPLIT OVER 1.5 INCHES. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDSDR ABXA2019103128163Skin · corrodedCORROSION ON FUSELAGE SKIN AT FUSELAGE STATION 1330, STRINGER 33L. THE SKIN WAS REPAIRED, THE AIRPLANE WAS GROUNDED.SDR ABXA20190904140Escape Rope · dislodgedDURING LANDING, THREE DESCENT DEVICES WERE DISLODGED FROM THEIR STORAGE CONTAINER LOCATED IN THE SUPERNUMERARY COMPARTMENT CEILING. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE THREE DESCENT DEVICES WERE REPLACED WITH SERVICEABLE DESCENT DEVICES. TSDR ABXA20190702129Fastener · missingRIGHT WING INBOARD FLAP, MID HINGE POINT IS MISSING THE HINGE BOLT, NUT, AND WASHERS. THE HARDWARE POSSIBLY DEPARTED DURING OPERATION OF THE AIRCRAFT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND NEW HARDWARE WAS INSTALLED. REFERENCE IPC 27-51-03-15 IT
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