N768AX
Service difficulty reports · 89
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 = 'N768AX' 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 = 'N768AX' 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 ABXA20231126216Unknown · unknownWHILE CONFIGURING FOR LANDING . WE GOT A L/E SLAT ASMY & DISCRETE LIGHT OCCURRED DURING APPROACH FLAPS @ 25 DEGS . MISSED APPROACH WAS ACCOMPLISHED & EMERGENCY WAS DECLARED. AFTER LANDING A/C GROUNDED BY MAINTENANCE. T/S PER FIM 27-58 FT 803. NO FAULTS NOSDR ABXA20231013198Fuse · unserviceableAFTER TAKEOFF, UPON RETRACTING THE LANDING GEAR A GEAR DISAGREE FLT ABX3102 .DIVERTED BACK TO PHX. AC GROUNDED DEFERRED THE LANDING GEAR ACTUATING SYSTEM IAW MEL 32-30-1. MAINTENANCE PROCEDURES C/W. PLACARDS INSTALLED. MBCB 10/23/2023.A/C REPO.FLIGHT TO ILN ,SDR ABXA20230711144Selector Valve · faultedRESERVE BRK VALVE EICAS DURING TAXI OUT, VALVE LT ON SWITCH ON AND ISO VLV LT ON ACC PANEL ON, SW OFF. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED TEST TO ISOLATE C1 ACMPCENTER SYSTEM PER AMM 29-11-00, ISOLATED ACMP SUPPLY SHUTOFFSDR ABXA20230703141Unknown · unknownAILERON LOCKOUT EICAS/DISCRETE LIGHT ILLUMINATED DURING PUSHBACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RERACKED / RH STAB TRIM AILERON LOCKOUT MODULE. PREFORMED AILERON LOCKOUT TEST IAW B767 AMM 27-11-00. TEST GOOD .OPS CK GOOD ACSDR ABXA20230522111Unknown · unknownSTAB TRIM EICAS MESSAGE ON CLIMBOUT AT 7000 MSL STAB TRIM EICAS MESSAGE REMAINED ILLUMINATED WITH BOTH AUTOPILOT ENGAGED AND DISENGAGED AFTER LANDING WHEN RESET TO 2. STAB EICAS MESSAGE EXTINGUISHED. STAB TRIMMING WAS AT 1/2 RATE. CREW ELECTED TO RETURN TO DEPSDR ABXA2023050473Unknown · unknownTRAILING EDGE FLAP DISAGREEMENT EICAS MESSAGE DISPLAYED DURING FINAL SEGMENT OF THE APPROACH AND A MISS APPROACH WAS ACCOMPLISHED TO COMPLETE THE REQUIRED NON NORMAL CHECKLIST AND AN EMERGENCY WAS DECLARED DUE TO HIGHER THAN NORMAL LANDING SPEED AND STRONG GUSSDR ABXA2023041859Unknown · unknownE/E ACCESS DOOR ON EICAS AND ACCESS DOOR LIGHT OVERHEAD. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE OPENED AND CLOSED E+E ACCESS DOOR FROM INSIDE AND OUTSIDE THE A/C IAW B767 AMM 52-71-00 AND VERIFIED EICAS MESSAGE AND OVERHEAD WARNING DISSDR ABXA2023041858Unknown · unknownR ENG STARTER EICAS MSG ON GROUND DURING START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED RT. ENG. START VALVE IAW MEL 80-00-2-1. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2023011207Cabin Air Sys · fault messageFWD CABIN TEMP EICAS ADVISORY MSG. FWD CABIN TEMP INOP DISCRETE LIGHT ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLESHOT AND THEN DEFERRED PER MEL 21-61-1-2. MAINTENANCE PROCEDURES COMPLIED WITH. AIRCRAFT RETURNED TO SERVISDR ABXA2023011106Throttle · failedTHRUST MANAGEMENT FAILED, RESET AND FAILED ON THE PUSH. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED TMC IAW MEL 22-30-1A. PLACARD INSTALLED; MX PROCEDURES C/W. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2022072286None · faultyRH ENG BLEED VALVE ON TAKE OFF PWR. CREW ABORTED TAKE OFF AT 70 KTS AND RETURNED TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED RH HIGH PRESSURE VALVE CONTROLLER IAW AMM 36-11-08. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2023050475Frame · crackedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE WAS REQUIRED TO INSPECT THE RIGHT INNER FRAME CHORD, LOCATED AT BS 883.5, LBL 89 PER ABX JOB CARD ABX-NEA-5350-0015-001 (AD 2012-22-17, SB 767- 53A0209 AND AD 2018-11-08, SB 767-53A0278). DURING INSPECTISDR ABXA2023050476Keelbeam · crackedDURING AN AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED CORROSION AND A CRACK ON THE R/H SIDE KEEL BEAM CHORD, UPPER FLANGE AT STA 792. AFTER LOCAL FASTENERS IN THE CHORD UPPER FLANGE HAD BEEN REMOVED, A 4.75” CRACK WAS DISCOVERED. A SURFASDR ABXA2022032848None · noneAPU PNEUMATICS INOP, AIRCRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENACE DEFERRED APU IAW MEL 49-11-1-1. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2022041142None · noneA/C BLOCKED OUT MX WAS TOLD CREW COULD NOT START LH ENGINE AC WAS RETURNING TO GATE MX ON BOARD TALKED TO CREW SAID NO APU PRESSURE. AIRCRAFT BLOCKED AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED APU AIR IAW MEL 49-11-1-1 MBCB 05/21/22, MX PROCEDURES C/WSDR ABXA2022030130Actuator · failedON LEFT ENGINE START, ENGINE VALVE DID NOT EXTINGUISH, ABORTED START. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE CONDITION MOTOR. IAW 76-11-01 OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ABXA202201503None · noneDURING TAXI OUT SHORT OF MIKE TAXIWAY ON SIERRA. MANUALLY TUNED FLM VOR MANUALLY IN BOTH VOR'S. CONFIRMED WITH ATC THAT THE FLM VOR IS OPERATIONAL! OFF FLAGS REMAINED IN VIEW . RETURNED TO GATE. AND GROUNDED BY MAINTENANCE. CONDUCTED TEST OF L/H AND R/H VOR, NSDR ABXA20211211129None · noneDURING RIGHT ENG START WHEN ADVANCING RT FUEL CONTROL , EICAS MESSAGE R ENG FUEL VALVE APPEARED AND DISAGREE ENGINE VALVE LIGHT ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND DAMAGED WIRING IN FORWARD CARGO COMPARTMENT. WIRISDR ABXA202109139090Cable · bindingON TAXI OUT, R ENG STARTED SURGE +/- 2% N2, +/- 100 FF, +/- 40 EGT, +/- 1% N1. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND R/H ENG VSV FEEDBACK CABLE TO HAVE HIGH PULL FORCE.R&R RH ENG VSV FEEDBACK CABLE IAW AMM 75-31-03. AIRCRAFT RETSDR ABXA2021830083Start Valve · bindingLH ENGINE START VALVE FAILED TO OPEN. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. FOUND L/H ENGINE START VALVE BINDING DURING MANUAL OPERATION. REMOVED OLD, THEN INSTALLED NEW L/H START CONTROL VALVE PER AMM 80-11-02. AICRAFT RELEASED FOR FLIGHT.SDR ABXA2021829080Starter · faultedLEFT ENGINE FAILED TO START, N2 NEVER GOT ABOVE 8.7 DUCT PRESSURE WAS NORMAL. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED THE #1 ENGINE STARTER IAW B767 AMM 80-11-0. AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA20210715066Pneumatic System · faultedAPU PNEUMATIC PRESSURE WENT TO ZERO AFTER PUSHBACK AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE, CYCLED APU. REGAINED DUCT PRESSURE AFTER RESTART. OPERATED BOTH PACKS. W/ PRESSURE BUILDING. IAW AMM 49-52-00. AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA202143023Shutoff Valve · stuckRT ENG BLEED OFF LIGHT ON WITH ALSO THE RT PACK OFF LIGHT ON DURING TAXI. AIRCRAFT LINED UP FOR TAKE OFF AND RT ENG. BLEED LIGHT DID NOT EXTINGUISH DURING ENGINE ACCELERATION. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE GROUNDED AIRCRAFT. REMOVESDR ABXA202112621Control Panel · defectiveAFTER PUSH BACK, LEFT ENGINE WOULD NOT START DUE TO NO PNEUMATIC AIR. AIRCRAFT BTB AND GROUNDED. REMOVED AND REPLACED BLEED AIR SUPPLY CONTROL PANEL, IAW B767 AMM 36-11-26. OPERATIONS CHECK NORMAL, AIRCRAFT RELEASED.SDR ABXA20200803228Apu · unknownAPU AUTO SHUTDOWN AFTER PUSH BACK, BTB AIRCRAFT GROUNDED BY MAINTENANCE. CHECKED APU ECU, IAW B767 FIM 49-11 FAULT TREE 958, AND FOUND NO MESSAGES. STARTED APU AND RAN FOR .75 HOURS, RAN BOTH PACKS, DRY MOTORED NR 1 ENGINE AND NO DISCREPANCIES NOTED, IAW B76SDR ABXA20200803207Valve · bindingAFT CARGO OVERHEAT LIGHT AND EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED. MAINTENANCE INSPECTED AND DEFERRED SYTEM AIRCRAFT WAS RELEASED FOR FLIGHT.SDR ABXA20200710123Duct · rupturedAFTER ENGINE START, OVERHEAT (OVERHEAD LIGHT) ILLUMINATED ON EQUIPMENT COOLING PANEL WITH ASSOCIATED EICAS MESSAGE FORWARD EQUIPMENT COOLING OVERHEAT. VERY LOW AIRFLOW THROUGH AC GASPERS. AIRCRAFT WAS GROUNDED.SDR ABXA2020061105066Warning Light · illuminatedAFTER ENG. START THE F/O PITOT DISCREET LIGHT REMAINED ILLUMINATED WITH F/O PITOT EICAS MESSAGE DISPLAYED. AIRCRAFT WAS GROUNDED.SDR ABXA2020062955104Stringer · corrodedSTR 38R CORRODED JUST FWD OF STA 434 FACTORY SPLICE. THE AIRPLANE WAS GROUNDED.SDR ABXA2020062914102Door Sill · crackedLEFT EMER. EXIT HATCH LOWER SILL FRAME IS CRACKED AT STA.889. THE AIRPLANE WAS GROUNDED.SDR ABXA2020062955105Stringer Splice · corrodedFLC STRINGER 39R APPROX. STA.752 CORROSION ON SPLICE PLATE. THE AIRPLANE WAS GROUNDED.SDR ABXA2020062951103Shear Tie · crackedFORWARD LOWER CARGO STA 368 BETWEEN S38L-S37L SHEAR TIE CRACKED FROM RIVET HOLE. THE AIRPLANE WAS GROUNDED.SDR ABXA2020062940101Longeron Splice · corrodedLONGERON EXTENSION FITTING AT KEEL AT STA.785 S38L CORRODED. THE AIRPLANE WAS GROUNDED.SDR ABXA2019080624130Controller · malfunctionedON TAKEOFF/POWER UP, THE RIGHT ENGINE BLEED DISCRETE LIGHT ILLUMINATED. THE LEFT & RIGHT ENGINE BLEED EICAS & MASTER CAUTION LIGHTS ILLUMINATED AND THERE WAS A SMELL OF SOMETHING BURNING. THE TAKEOFF WAS ABORTED AT A SPEED OF LESS THAN 60 KNOTS. THE AIRPLANE WSDR ABXA20180831100Support Beam · gougedGOUGE IN THE NR 7 FLAP SUPPORT BEAM NR 1 HOLE AT THE 12:00 POSITION. THE GOUGE DAMAGE WAS REMOVED BY REAMING THE HOLE BEYOND THE MAXIMUM PRODUCTION SIZE. THE AIRPLANE WAS GROUNDED.SDR ABXA20180831099Support Beam · corrodedCORROSION ON THE CHORD AFT OF THE MAIN LANDING GEAR SUPPORT BEAM AT RIGHT WING STATION 336. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA20180831098Web · corrodedCORROSION ON WEB AT RIGHT FORWARD WING TO BODY AREA AT FUSELAGE STATION 720. THE WEB WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA20180831097Support · corrodedCORROSION ON THE TRAILING EDGE PANEL SUPPORT UPPER CHORD AT RIGHT WING STATION 300. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA20170130005Failsafe · crackedRIGHT FAILSAFE STRAP BS 955 CRACKED AT LOWER ATTACH HOLE COMMON TO TEE FITTING. CRACKED AREA TRIMED OUT AND REPAIRED IAW SDR. AIRCRAFT WAS GROUNDED.SDR ABXA20170130004Failsafe · crackedLEFT FAILSAFE STRAP BS 955, CRACKED AT LOWER ATTACH HOLE COMMON TO TEE FITTING. REMOVED AND REPLACED THE FAILSAFE STRAP IAW JOB CARD EA 53500013-007 AND INSTALLED A NEW FAILSAFE AIRCRAFT WAS GROUNDED.SDR ABXA20170127010Frame · corrodedTWO HOLES IN LEFT HAND SIDE FRAME FITTING (PICKLE FORK) COMMON TO FUSELAGE SKIN SIZE .309" HAVE DEFECT INDICATION FROM HFEC HOLE SCAN. REAMED HOLES UP UNTIL NO FURTHER DEFECTS WERE NOTED REA WAS GIVEN TO REPAIR THE HOLES. HOLES REPAIRED IN ACCORDANCE WITH REA SDR ABXA20170127009Frame · corrodedCORROSION FOUND ON FORWARD LOWER FACE OF LEFT HAND SIDE FRAME FITTING (PICKLE FORK) AROUND SEVEN FASTENER HOLES COMMON TO MATING SURFACE OF REAR SPAR WEB PAD UP AREAS. REMOVED CORROSION SPOT FACED COMMOMON TO BOLT HOLES. NDT CHECKED NO DEFECTS REMAINING ROTO PSDR ABXA20170127008Structure · corrodedAFT SPAR WEB HAS CORROSION ON THE PAD UP AREA COMMON TO MULTIPLE HOLES. REMOVED CORROSION, SPOT FACED CORROSION NEAR HOLES NDT CHECKED NO FURTHER DEFECTS NOTED ROTO PEENED BLENDED AND SPOT FACED AREAS REPAIRED BLENDED AND SPOT FACED AREAS IN ACCORDANCE WITH RESDR ABXA20170119007Failsafe · crackedLEFT FAILSAFE STRAP AT BS 955 IS CORRODED AND CRACKED PAST TRIM OUT LIMITS. REPLACED THE FAILSAFE.SDR ABXA20160730126Bulkhead · corrodedFOUND UNACCOUNTED OIL CAN REPAIR NEAR THE OUTER EDGE STIFFENER. REMOVED UNACCOUNTED REPAIR STIFFENER IAW SRM 51-40-02, FABRICATED NEW STIFFENER IAW SRM 53-80-08, REPAIR 8, STEP 3, LOCATED IAW SRM 53-80-08. TREATED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40SDR ABXA20160730125Channel · crackedAFT FUSELAGE COMPARTMENT. REMOVED REPAIR CHANNEL IAW SRM 51-40-02. FABRICATED NEW REPAIR CHANNEL IAW SRM 53-80-08, REPAIR 3, PG 203, LOCATED CHANNEL IAW SRM 53-80-08. TREATED CHANNEL IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40-02 AND 53-80-08. REF REO G20SDR ABXA20160728119Keelbeam · corrodedCORROSION AT BS 990 - 1010 LEFT SIDE OF KEEL BEAM ALONG THE UPPER SIDE. FOUND TO BE OUT OF LIMITS IAW SRM 53-50-12. REPAIRED IAW SRM 53-50-12 REPAIR 1, REO-G20121 REV. A, AND REA B653-62037MR.SDR ABXA20160727123Bracket · crackedAFT CARGO STA 1087 UNDER STR 38L JUST AFT OF FORWARD BULKHEAD HAS EVALUATED BLEND ON STR 38L IN AFT CARGO STA 1087 AFT OF FORWARD BULKHEAD, ORIGINAL MATERIAL THICKNESS .125", REMOVED .048", REMAINING THICKNESS .077". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15SDR ABXA20160720124Beam · corrodedFORWARD CARGO DOOR LOWER SILL BEAM UPPER SURFACE CORRODED AT AFT REPAIRED FORWARD CARGO DOOR LOWER SILL BEAM UPPER SURFACE, HIGH FREQUENCY, NO CRACKS NOTED. INSTALLED NEW FASTENERS IAW SRM 51-40-02. INNER CHORD, PART LOCATION: FLC STA 624-628 AT RBL44, PN: 1SDR ABXA20170720121Skin · crackedCRACK INDICATION FOUND L-1 DOOR CUTOUT LOWER FORWARD CORNER. REPAIRED FUSELAGE SKIN STA 287 TO STA 347, S18L TO S24L BELOW L-1 DOOR IAW REO-G20052, REV B AND NR-B653-62038MR. SDR INFO: PART NAME: FUSELAGE SKIN, PN: 141T3331-5, SN: NSN, STA 287-347, LT BELOW
Back to N768AX