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 ABXA20140806278Support Fitting · corrodedLEFT WING OTBD & INBD ROTARY ACT SUPPORT HOLE AT 9 O`CLOCK LOOKING INBD SHOWS DEFECT INDICATION HFEC. SEE REA NR B657-61118-MR. SDR INFO CORRODED L2, PN 113T1345-43, SN NSN, PART NAME NR 1 FLAP SUPPORT FITTING, STRINGER & WS LOC ON ACFT 792.2. ACFT WAS GNDESDR ABXA20140806276Support Fitting · corrodedRIGHT WING OTBD ROTARY FLAP SUPPORT NR 8 HOLE LOOKING INBD SHOWS DEFECT INDICATION HFEC. SDR INFO CORRODED L2, PN 113T1345-44, SN NSN, PART NAME NR 8 FLAP SUPPORT FITTING, STRINGER & WS LOC ON ACFT ROWS 798.2. ACFT WAS GNDED.SDR ABXA20140806263Stringer · corrodedSTRINGER 36R CORRODED BETWEEN STATION 566 & 588. REPAIRED STRINGER 36 IAW REA B653-61115-MR. SDR INFO CORRODED LEVEL 2, PN 143T3001-70, PART NAME STRINGER, SN NSN, FS & BS LOC STATION 566 TO 588 STRINGER 36R. ACFT WAS GNDED.SDR ABXA20140805274Floor Support · crackedBULK CARGO FLOOR PANEL ATTACH STRINGER AT STATION 1504 LBL 32 CRACKED AT NUTPLATE HOLE. CUT OUT & REMOVED CRACKED AREA ON FLOOR PANEL SUPPORT STRINGER & INSTALLED REPAIR IAW SRM 51-70-11 FIG 1. FABRICATED REPAIR FROM 7075T6 063. SDR INFO CRACKED 1/4 INCHES,SDR ABXA20140805267Support Fitting · corrodedRIGHT WING TE PANEL SUPPORT TEE CORRODED IN 2 PLACES NEAR PANEL 652FB. INSTALLED NEW SUPPORT, TEC CHORD, SRM 51-40-02 & REINSTALLED. REMOVED TE PANEL IAW SRM 51-40-02. SDR INFO CORRODED L2, PN 113T1407-6, PART NAME CHORD, SN N/A, EXACT FS & BS FROM WS 431 -SDR ABXA20140805266Stringer · corrodedSTRINGER 33R BETWEEN STATION 412 & 434 CORRODED. REPAIRED STRINGER 33R AT STATION 403 - 431 IAW REA NR B653-6115 MR. SDR INFO CORRODED L2, PN 143T3001-70, SN NSN, PART NAME STRINGER, FS & BS LOC ON ACFT STATION 403 - 431 STRINGER 33R. ACFT WAS GNDED.SDR ABXA20140801262Keelbeam · corrodedKEEL BEAM RT LOWER CHORD HAS CORROSION AT STATION 920. REMOVED CORROSION IAW B767-200 SRM 53-50-12, DETAIL III, ALLOWABLE DAMAGE 1. SDR INFO CORRODED L2, PN 146T3223, SN NSN, PART NAME KEEL BEAM, FS & BS LOC ON ACFT 920. ACFT WAS GNDED.SDR ABXA20130604452Inertia Reel · defectiveDURING LANDING 1 INERTIAL ESCAPE REELS FELL DOWN. R & R INERTIAL REEL ASSY IAW AMM 25-61-03-14, OPS NORMAL.SDR ABXA2011051045Spar · damagedRT SPAR SIDE FRAME STA 955 (PICKLE FORK) LEVELING COMPOUND SHRUNK, CRACKED AND LIFTED IN SEVERAL AREAS. CORROSION IS ALSO EVIDENT IN AFT CENTER POCKET. REMOVED LEVELING COMPOUND FOUND SIDE FRAME (PICKLE FORK) CORRODED. REMOVED AND REPLACED SIDE FRAME IAW B7SDR ABXA2011051039Fitting · corrodedLEFT SIDE FRAME FITTING HAS CORROSION IN THE AFT CENTER AND AFT OUTBOARD POCKET. REMOVED CORROSION IAW B767 SRM 51-10-02. AREA REPAIRED IAW REA B653-59259-MR.SDR ABXA2011051040Tee Fitting · corrodedLT T-FITTING CORRODED (FAIL SAFE STRAP AREA). REMOVED T-FITTING, DRILLED NEW REPLACEMENT FITTING IAW B767 SRM 51-40-05. NEW FITTING TO BE RE-INSTALLED PER REA B653-59247-SB.SDR ABXA2011041536Fitting · corrodedDURING AIRCRAFT HEAVY MAINTENANCE VISIT TO ILN, MAINTENANCE & ENGINEERING SERVICES, MAINTENANCE REPORTED CORROSION FINDINGS LOCATED IN POCKET AREAS OF THE AFT FACE AND FLANGES OF THE LEFT FUSELAGE SIDE FRAME FITTING AT STA 955. THE CORROSION JUST FORWARD OF TSDR ABXA2011051042Keelbeam · corrodedRT KEEL BEAM LOWER SURFACE AT APPROX STA 1014 IS CORRODED. RT KEEL BEAM LWR SURFACE AT APPROX STA 1014 CORRODED. REMOVED AND REPAIRED IAW B767 SRM 53-50-12 FIG 201.SDR ABXA2011051047Bulkhead · canningAPB OIL CAN EXTEND BEYONDS REPAIR RS 17-18 TS1-OE. REPAIRED IAW B767-200 SRM 53-80-08 FIG 201. REPEAT INSPECTION OF CRITICAL ROW AT 2,500 CYCLE INTERVAL.SDR ABXA2011051046Bulkhead · canningAPB OIL CAN EXTENDS BEYOND REPAIR RS 18-19, TS1-OE. REPAIRED OIL CAN IAW B767-200 SRM 53-80-08 FIG 201. REPEAT INSPECTION AT 3,000 CYCLE INTERVALS.SDR ABXA2011051044Stringer · crackedS18L CRACKED UNDER SPLICE AT FS 676. REPAIRED STRINGER 18L IAW REA B653-59243-MR.SDR ABXA2011051043Stringer · crackedS17L CRACKED UNDER SPLICE AT FS 676. REPAIRED STRINGER 17L IAW REA B653-59243-MR.SDR ABXA2011051041Door · damagedRT FWD CORNER OF MEC DOOR CHAFED AND BENT. FOUND DMG TO BE GREATER THAN .100 DEPTH IAW B767-200 SRM 52-40-01 FIG 101. FABRICATED REPAIR DOUBLER FROM 2024T3. INSTALLED REPAIR DOUBLER PER 767 SRM 52-40-012 FIG 201.SDR ABXA2011051048Angle · crackedNR 2 PYLON RT SIDE ANGLE LOCATED BETWEEN AFT STRUT FAIRING AND CORE COWL HINGE HAS 2 INCH CRACK. REMOVED NR 2 PYLON RT SIDE, ANGLE AND WELD REPAIRED IAW ABX PROCESS STANDARD MANUAL 900-7-2-1. RE-INSTALLED BRACKET IAW B767-200 SRM 51-40-02.SDR ABXA2011051049Bracket · crackedINBOARD CORE COWL T-BRACKET CRACKED AT FIRST RIB O/B OF 2ND FROM AFT END HINGE. REMOVED AND REPLACED T-BRACKET ON I/B COWL AT FIRST R.B O/B OF 2ND FROM AFT HINGE IAW 767 DRAWING 314T1210.SDR ABXA2011051050Structure · crackedSTA 287 RBL 25 CHORD IS CRACKED NOSE WHEEL WELL, CRACK IS ABOVE WL 159 AND IS .7" LONG. REPAIRED CHORD AT STA 287 RBL 25 IAW 51-70-12. MANUFACTURED FILLERS FROM AND 1033-2401, 7075T6511.SDR ABXA2011032716Structure · crackedSTA 287, RBL 25, CHORD IS CRACKED, NOSE WHEEL WELL, CRACK IS ABOVE WL 159 AND IS .7 INCH LONG. REPAIRED CHORD AT STA 287, RBL 25 IAW B767 SRM 51-70-12.SDR ABXA200911180067Warning System · malfunctionedDURING APPROACH WHEN FLAPS SELECTED TO FLAPS 1 THE LEADING EDGE SLAT DISAGREE LIGHT ILLUMINATED. FOLLOWED NON NORMAL AND LANDED WITH FLAP 20. RESET SYSTEM AND OPS CKD. FLAPS AND SLATS AND PERFORMED FIM 27-51-00. FOUND NO FAULTS SYSTEM OK.SDR ABXA200909290047Duct · brokenBODY DUCT LEAK EICAS MESSAGE AND DUCT LEAK DISCREET LIGHT ILLUMINATED ON TAXI IN - CABIN FILLED AIR COND SMOKE. FOUND APU AIR SUPPLY DUCT BROKEN. REMOVED AND REPLACED APU AIR SUPPLY DUCT BETWEEN STA 1064 AND 1088. ALSO REPLACED INSULATION BLANKET AT AFT CARSDR ABXA200902130011Power Supply · inoperativeLEFT EMERGENCY EXIT DOOR LIGHT L313 WAS INOPERATIVE. EXCHANGED EMERGENCY LIGHT POWER SUPPLY M735 WITH SPARE M734 IAW AMM 33-51-07. OPS CHECKS OK. DEFERRED SPARE EMERGENCY POWER SUPPLY FOR MAINT TRACKING IAW GMM 01.07.04. MPCW (RN) PLACARD INSTALLED. REPLACSDR ABXA200810270254Engine · defectiveLEFT FAN ENGINE VIBRATION HIGH 4.7. OTHER VIBRATION INDICATIONS WERE: AIRPLANE VIBRATION, AUDIBLE NOISE, VIBRATION FOLLOWS THRUST CHANGE. REPLACED NR 1 ENGINE PER WORK CARD NR 7010. OPS CHECK NORMAL.SDR ABXA080192Mec · defectiveRT ENG COMPRESSOR STALL AT LEVEL OFF 37000` ENG STABLE AT POWER REDUCTION. ENG PARAMETERS NORMAL EVENT RECORDED. RIGGED VSV, CHECKED FEEDBACK CABLE, WITHIN LIMITS. COMPLIED WTIH BOROSCOPE INSPECTION. NO DAMAGE NOTED IAW B767 MM 75-31-03-5-72-00-00-6. REMO
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