N783AX
Service difficulty reports · 119
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 = 'N783AX' 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 = 'N783AX' 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 ABXA20250813175Manifold · crackedON TAXI R ENG HAD VIBRATIONS FROM 2.8 TO 3.3. WHEN ADDING TAXI THRUST VIBRATION INDICTIONS UP NTO 4.9 AND STARTED BEING VARIABLE- VIBRATION FELT IN AIRFRAME. AIRCRAFT RETURNED TO BLOCKS. (BTB). PERFORMED D.V.I OF RT ENG & FOUND UPPER & LOWER LPT COOLING AIR SDR ABXA2025081167Warning Message · illuminatedDURING TAXI, LEFT INBOARD AILERON POSITION DISAGREEMENT WITH THE INDICATOR ON THE LOWER STATUS PAGE. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE DEFERRED IAW MEL C ABX-27-08-1. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20250512094Compressor · stalledDURING CLIMB, LT ENG COMPRESSOR STALL AT APPROX FL 310 WITH CLIMB AND THRUST. STOPPED WHEN APPROX BELOW 93% N1. NO EICAS EXCEEDANCES. NO FURTHER STALLS IN CRUISE OR DESCENT. CONDUCTED STALL INSPECTION PER AMM 72-00-00/601, THEN CONDUCTED T/S PER FIM 71-05 FT SDR ABXA20250410073Controller · malfunctionedDURING CLIMBOUT CABIN AUTO INOP ALT 2 APPEARED, CREW DECLARED EMERGANCY AND PERFORMED (ATB) AND LANDED SAFLEY .MTX GROUNDED A/C AND TROUBLE SHOT. MTX PERFORMED BITE TEST OF #1 AND #2 CONTROLLERS, OPS CHECK GOOD IAW B767 AMM 21-31-00,. PRESSURIZED ACFT IAW SDR ABXA20250403068Warning Message · illuminatedON TAKEOFF ROLL L FWD ENTRY DOOR EICAS MESSAGE. TAKEOFF REJECTED @ 100 KT. A/C RETURNED TO BLOCKS (BTB). DEFERRED L1 DOOR INDICATION IAW MEL ABX 52-71-1-1. MAINTENANCE PROCEDURES C/W. PLACARDS INSTALLED. MBCB 04/13/2025. REPETITIVE INSPECTION REQUIRED BESDR ABXA20250228050Sensor · shortedDURING CLIMB, LIGHT COMES ON INDICATION BRAKE TEMP WITH BTMS INDICATION 8 5 6 6 TOP 0 1 1 9 BOTTOM COMPLETED NN CHECKLIST TEMPERATURE INITIALLY GOES UP THEN SLOWLY DOWN MADE LOW PASS REPORTED OK AFTER RETURNING TO FIELD (ATB)AND LANDING . MTX GROUNDED A/C AND SDR ABXA20241121230Controller · faultedDURING TAXI APU NOT PRODUCING BLEED AIR AC RETURNED TO BLOCK (BTB). MTX GROUNDED AC , RESET AND CLEANED FAULT ON APU CONTROLLER PER AMM 49-67-05 APU OPS CHECK GOOD. BLEED AIR CHECK TESTS GOOD AND RETURNED AC TO SERVICESDR ABXA20241011189Hot Water Pot · odorSMOKE AND BURNED ELECTRONICS COMING FROM HOT POT FULL OF WATER. MTX DEFERRED HOT POT FOR DEPARTURE AND DEACTIVATED IAW ABX-NEF-25-02-02. LATER FOUND AND REPLACED BURNT TERMIANL ENDS IAW B767 SWPM 20-30-11. REMOVED & REPLACED CREW HOT CUP BRACKET IAW B767 AMM SDR ABXA20240727144Flight Dir · faultedON TAXI OUT THE FO FLIGHT DIRECTOR CHANGED TO A TO/HDG MODE.PERFORMED RESETS AND WENT TO CORRECT TO/TO MODE .ON CLIMB OUT CAPTS AND FOS ADI'S WENT BLANK. A/C RETURNED TO FIELD AND LANDED WHEN RETURED TO GATE MTX GROUND A/C . AND DEFERRED THE THUST MANAGEMENT SSDR ABXA20240703130Module · leakingCOMPLETED ENGINE START CHECKLIST, GROUND CREW SAW HYDRAULIC LEAK. EICAS STATUS PG. HYDRAULIC CETER QUANTITY AT 0.58 ENGINES WERE SHUT DOWN AND MTX ENTERED FLIGHTDECK AND GROUNDED AC . MTX FOUND (ADP CTR CASE DRAIN MODULE) LEAKING AND REPLACED MODULE INSTL-PRESSDR ABXA20240612111Apu · inoperativeDURING TAXI DURING #2 ENGINE START NO APU AIR ,ACFT RETURNED TO GATE AND MAINTENANCE GROUNDED ACFT . AND DEFERRED THE APU IAW ABX-MEL-49-11-1A AND RETURNED AC TO SERVICE FOR DEPARTURESDR ABXA20240530103Centering Mech · malfunctionedAILERONS DO NOT CENTER THEMSELVES, AILERON FEEL EXTREMELY LIGHT. MOVE LEFT/ RIGHT THEY STAY LEFT RIGHT AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED AC . TROUBLE SHOT AND REPLACED LATERAL CONTROL FEEL CENTERING AND TRIM MECHANISM IAW AMM 27-11-08 SYSTEM OPSDR ABXA2024053100414Trim System · failedAILERONS DO NOT CENTER THEMSELVES, AILERON FEEL EXTREMELY LIGHT. MOVE LEFT/ RIGHT THEY STAY LEFT RIGHT.SDR ABXA2024052499Module · malfunctionedDURING TAXI APU AIR INOP LIGHT ILLUMINATED .AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC AND DEFERRED APU IAW ABX MEL-49-11-1A . AND AC DEPARTED . BITE CHECK ECU SHOWS LAST FLIGHT FAULT "PT SENSOR" AND MINI FLAG 14. LINE TO PT SENSOR (TOTAL PRESSURE TRANSDSDR ABXA20240527499Warning Light · illuminatedDURING TAXI APU AIR INOP LIGHT ILLUMINATED. AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC AND DEFERRED APU IAW ABX MEL-49-11-1A . AND AC DEPARTED .SDR ABXA20231025207Unknown · unknownDURING TAXI C HYD DEM PIMP EICAS MESSAGE APPEARED , AC RETURN TIO BLOCK AC GROUNDED BY MAINTENANCE AND DEFERRED SYSTEM IAW ABX MEL 29-11-3 AC RETURNED TO SERVICESDR ABXA20231002194Panel · degradedDURING C3 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED A DEEP GOUGE DAMAGE ON THE LH WING INBOARD, AFT FLAP, LEADING EDGE PANEL SKIN AT THE INBOARD SIDE APPROXIMATELY AT [FS I 04. THE GOUGE ALMOST PENETRATED THE ENTIRE THICKNESS OF THE SKIN. AFFECSDR ABXA20231002193Skin · dentedDURING C3 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED A 25-INCH DENT DAMAGE ON THE SKIN APPROX. BETWEEN BS 1480 AND BS 1502, JUST BELOW S-24R. THE DENT IS A= 1.10 INCHES WIDTH, AND (Y) 0.038-INCH DEEP WITH A/Y RATIO IS 28.9. THE DENT IS OUT OF LISDR ABXA20231002192Web · corrodedDURING C3 MAINTENANCE CHECK AT HA ECO AMERICAS, MAINTENANCE REPORTED CORROSION AND SMALL DENT DAMAGE ON THE RH KEEL WEB, APPROXIMATELY AT BS 976, RBL5. CORROSION DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51- I 0-02, WITH A MINIMUM MATERIAL REMAININGSDR ABXA20231002191Web · corrodedDURING C3 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED LH KEEL WEB CORROSION DAMAGE APPROXIMATELY AT BS 999, LBL 5.0. POST BLEND REMAINING MATERIAL IS 0.027 INCHES (MINIMUM) FROM INITIAL THICKNESS OF 0.050 INCHES (AT CHEM-MILLED POCKET). THE MATERSDR ABXA20230622123Unknown · unknownGND CREW NOTED HYD LEAK FROM NOSE WHEEL WELL ON PUSHBACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE T/S AND FOUND B NUT LOOSE FOR NOSE GEAR DOWNLOCK ACTUATOR DOWN LINE TIGHTENED B NUT AND ACCOMP. LEAK CHECK IAW B767 AMM STANDARD PRACTICE SDR ABXA2022080490Bleed Air Sys · leakingRT ENG BLEED OFF EICAS ASSOCIATED DISCREET LIGHT DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED R/H PRSOV IAW MEL 36-11-1-1A. PLACARD INSTALLED. MX PROCEDURES COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20220601None · failedL BLD ISLN VAL RECEIVED AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LH ISLN VALVE IAW B767 AMM 36-11-04. OPS CHECK GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2022042145None · noneLEFT AOA EICAS ILLUMINATED AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND LH AOA CIRCUIT BREAKER POPPED RESET DUE TO PITOT STATIC WORK OVER WEEKEND PERFORMED P-61 MISC TEST FOR 30 SEC THEN 25 SEC LH AOA PROBE HEAT TSDR ABXA2022033037None · crackedDURING TAXI-OUT- RT HYD SUS PRESS EICAS FOLLOWED IMMEDIATELY BY RT HYD SYS QTY. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND LEFT GEAR NORMAL ANTI-SKID MODULE #2 BRAKE FUSE HOUSING CRACKED. REMOVED AND REPLACED SAME IAW B767 AMM 32-42-SDR ABXA2022013119Generator · faultyR GEN DRIVE EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE. RECONNECTED DRIVE. VERIFIED PROPER OIL SERVICE. VERIFIED IDG CHARGE PRESSURE SWITCH OPERATION. REPLACED GCU, REF B767 AMM 24-22-02. RAN ENGINE. ALL GENERATOR FUNCTIONS SDR ABXA2022010806None · noneDURING A LINE MAINTENANCE WORK PACKAGE A WIRING BUNDLE WAS DISCOVERED TO HAVE DAMAGE. THIS DAMAGE HAS BEEN ASSOCIATED WITH AUTOPILOT FAULTS AND VARIOUS FUEL PUMP ISSUES.WIRING BUNDLE IS LOCATED AT STA. 390 JUST BELOW THE FWD. RACK COOLING FAN. THE AFFECTED WIRSDR ABXA20211230134None · noneCTR L FUEL PUMP INOP DURING TAXI. AIRCRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPAIRED BROKEN WIRING IN FWD. LOWER CARGO IAW SWPM 20-30-12 AND WDM 22-11-21, 28-22-11. AIRCRAFT RETURNED TO SERVICESDR ABXA20211115112None · noneAFTER BLOCK OUT C IRS FAULT EICAS MESSAGE AND FAULT LIGHT ON OVERHEAD. AICRAFT RETURNED TO BLOCK AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED C IRS PER MEL 34-21-1C. ALL MX PROCEDURES C/W. PLACARDS INSTALLED. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2021810073Aileron · out of rigLH INB AILERON POSTION INDICATION SHOWS RETRACTED ,WHEN, FLAPS SELECTED TO 5. AIRCRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE. LEFT INBD AILERON IS IN CORRECTED POSITION AND THE RIGHT INBD AILERON IS NOT. PERFORMED A CHECK ON THE ANGLE GEARBOX INDEX MSDR ABXA20200803204Line · crackedINFLIGHT EMGERGENCY DECLARED FOR LOSS OF CENTER SYSTEM HYDRAULIC PRESSURE ON FINAL APPROACH. AIRCRAFT LANDED SAFELY AND WAS TOWED FROM RUNWAY. AIRCRAFT WAS GROUNDED BY MAINTENANCE. T/S & FOUND HYDRAULIC LINE IN RT WHEEL WELL CRACKED FOR SLAT SYSTEM AT S846 SDR ABXA20200803185Igniter · failedNO START ON RIGHT ENGINE WITH NR 1 IGNITER, HAD TO PULL BACK TO GATE FOR TRAFFIC. AIRCRAFT GROUNDED. REMOVED AND REPLACED RIGHT ENGINE NR 1 IGNITOR PLUG, IAW AMM 74-21-02. RAN ENGINE IAW AMM 71-00-00 TABLE 501 TEST 3. ENGINE OPERATION CHECK GOOD. DI CLEARSDR ABXA20200713125Actuator · failedR ENG FUEL VAL EICAS MSG. AIRCRAFT WAS GROUNDED.SDR ABXA2020051107058Warning System · activatedHOT BATT BUS FAILED IN-FLIGHT. CREW CALLED AND ADVISED THAT THEY HAD LEFT, RIGHT, AND CENTER IRSS FAIL, FIRE DETECTION AND PROTECTION FAIL, AND ALL SPAR VALVES FAIL. AIRCRAFT WAS GROUNDED.SDR ABXA2020054056Warning System · activatedFWD EQPT VAL EICAS MSG AND DISCRETE VALVE LIGHT ON EQUIP COOLING PANEL OVER HEAD. QRH PROCEDURE DID NOT CLEAR. AIRCRAFT WAS GROUNDED.SDR ABXA2019100199159Stringer · crackedCRACK IN STRINGER 24L AT FUSELAGE STATION 676. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA2019100129158Stringer · crackedCRACK IN STRINGER 22L AT FUSELAGE STATION 676. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA2019100129157Skin · corrodedCORROSION ON THE LOWER SKIN OF THE RIGHT OUTBOARD FLAP NEAR THE INBOARD HINGE. THE FLAP WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA2019100129156Panel · delaminatedDELAMINATION TO THE COMPOSITE STRUCTURE OF THE VERTICAL STABILIZER PANEL P/N 175T2001-2 AT FRONT SPAR STATION 15 AND FRONT SPAR STATION 50. THE PANEL WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201810053103Power Supply · inoperativeNR 3 EMERGENCY LIGHT INOP IN SUPERNUMERARY COMPARTMENT CEILING AND BOTH SPARE EMERGENCY LIGHTING BATTERY POWER SUPPLIES ARE INOP. WHILE THE AIRPLANE WAS GROUNDED, THE EMERGENCY LIGHTING BATTERY POWER SUPPLIES AT POSITIONS M734, M736, AND M737 WERE REPLACED. THSDR ABXA20180821095Engine · failedIN THE BEGINNING OF THE TAKEOFF ROLL WITH THRUST SELECTED, THE RIGHT ENGINE DID NOT RESPOND TO THROTTLE ADVANCEMENT & THE TAKEOFF WAS REJECTED. THEN DURING THE SECOND TAKEOFF ROLL WITH THE AUTO THROTTLE SELECTED OFF, THE RIGHT ENGINE FAILED TO ACCELERATE, CAUSSDR ABXA201806218071Skin · scratchedSCRATCH FOUND ON THE FUSELAGE SKIN AT BS 413, STRINGER 35L. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201806218070Skin · dentedFUSELAGE SKIN NEAR BS 463.5, STRINGER 35L WAS DENTED. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20171201142Stator Vane · out of adjustTHE RIGHT ENGINE HAD COMPRESSOR STALLS DURING CLIMB BETWEEN FL340 AND FL350. THE THROTTLE WAS RETARDED 10% AND THE COMPRESSOR STALLS STOPPED. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE RIGHT ENGINE'S VARIABLE STATOR VANE SYSTEM WAS INSPECTED AND SDR ABXA20170907117Shear Tie · corrodedCORROSION ON THE SHEAR TIE AT BS 434. THE SHEAR TIE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA20170907116Stringer · corrodedCORROSION ON THE LOWER SURFACE OF STRINGER 34L AT BS 434. THE STRINGER WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20170907115Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 39R, BS 434. THE THE STRINGER SPLICE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA20170907114Seat Track · corrodedCORROSION ON SEAT TRACK AT BS 347 - 350, RBL 54. THE SEAT TRACK WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20170907113Seat Track · corrodedCORROSION ON SEAT TRACK CROWN AT BS 332, RBL 33. THE SEAT TRACK WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20171003112Skin · corrodedCORROSION ON RIGHT WING TRAILING EDGE UPPER SKIN AT WING STATION 977. THE SKIN WAS REPAIRED. T AIRPLANE WAS GROUNDED.
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