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 ABXA070348Girt Bar · malfunctionedMAIN ENTRY DOOR SLIDE WOULD NOT ARM. FOUND GIRT BAR LOCK PANEL NOT TURNING. INSTALLED BUSTLE. OPERATED EMERGENCY ESCAPE SLIDE IAW B767 AMM 25-66-01-4-10. OPS CHECKED GOOD.SDR ABXA060313Blade · crackedTHRUST REVERSER 315T4725-25, S/N: 000042 HAD A CRACKED V-BLADE, P/N: 315T1206-3. REMOVED AND REPLACED THRUST REVERSER IAW B767 MM.SDR ABXA060304Fitting · crackedNR 2 ENGINE HAD CRACKED FITTING JUST FORWARD OF INBOARD THRUST REVERSER UPPER ATTACH POINT AREA. REMOVED ALL SEALS AND SEAL RETAINERS. REPAIRED FLANGE PER REA B672-55012. REINSTALLED ALL PARTS REMOVED PER SRM 51-40-2.SDR ABXA060303Stiffener · crackedSTIFFENER AT REAR OF NR 2 PYLON INBOARD SIDE CRACKED (DOUBLER ON STIFFENER). REMOVED AND REPLACED STIFFENER IAW B767 SRM 54-57-71 REF DWG 313T1380.SDR ABXA060302Stiffener · crackedSTIFFENER AT REAR OF NR 2 PYLON OUTBOARD SIDE CRACKED. REMOVED CRACKED STIFFENER. FABRICATED NEW STIFFENER IAW B767-200 DRAWING 313T3380. INSTALLED NEW ANGLE IAW B767-200 SRM 51-40-02.SDR ABXA060301Fitting · crackedFITTING CRACKED ON STA 168 CANTED BULKHEAD AT FORWARD NOSE LANDING GEAR ATTACH POINT LEFT SIDE. REPLACED FITTING IAW B767 SRM 51-40-02.SDR ABXA050207Battery · dischargedEMERGENCY LIGHTS INOPERATIVE. SWAPPED EMERGENCY LIGHT BATTERY WITH SPARE. OPS CHECKED GOOD IAW B767 AMM 33-00.SDR ABXA040346Panel · out of adjustMAIN CABIN DOOR GOT JAMMED, WOULD NOT GO ALL THE WAY CLOSED OR OPEN. MAINTENANCE FOUND DOOR PANEL OFF TRACK AT CEILING. PUT PANEL BACK ON TRACK. OPERATED DOOR THROUGH CYCLE, CHECKED OK IAW AMM 52-11-00.SDR ABXA040338Light · inoperativeOVERHEAD PANEL EMERGENCY LIGHTS BACKGROUND LIGHTING DIM/INOP. REPLACED EMERGENCY LIGHT AND CREW OXYGEN LIGHT PLATE. OPS CHECKED GOOD IAW B767 AMM 33-13-07.SDR ABXA030450Antenna · missingTCAS TEST SHOWED UPPER ANTENNA FAIL. DISCOVERED UPPER ANTENNA MISSING. MAINTENANCE INSTALLED TCAS ANTENNA IAW REA B634-47860.SDR ABXA040022Fitting · crackedRIGHT MAIN LANDING GEAR DOOR RETRACT FITTING CRACKED NEAR RIGHT SIDE KEEL BEAM. REMOVED AND REPLACED BELLCRANK FITTING IAW B767 MM 32-12.SDR ABXA030444Fitting · crackedRIGHT MAIN LANDING GEAR DOOR RETRACT FITTING CRACKED NEAR RIGHT SIDE KEELBEAM. CRACK LENGTH .7500 INCH FROM FASTNER HOLE TO EDGE OF FITTING. REPLACED BELLCRANK FITTING.SDR ABXA030208Engine · malfunctionedLEVELING AT FL39 M.8-AIRCRAFT EXPERIENCED AN UNUSUAL VIBRATION IN YAW/SHAKING, WITH A SLAPPING NOISE TO THE RIGHT OF THE COCKPIT. ALL NORMAL WHEN THRUST RETARDED FROM CLIMB THRUST, SOUNDED AND LEFT LIKE A DOOR OR PANEL WAS OPEN. REMOVED AND REPLACED THE NR 2SDR ABXA020050Skin · corrodedLEFT WING, FRONT SPAR, LOWER CHORD, JUST OUTBOARD OF THE NR 1 PYLON, WAS CORRODED AT APPROXIMATELY 0FSS 400. REPAIRED AREA IAW REA B657-43893.SDR ABXA020049FittingLEFT WING OUTBOARD PITCH LOAD FITTING HAD EXISTING SHORT E.D. REPAIRED AREA IAW REA B657-43882MR.SDR ABXA020051Skin · corrodedAFT CARGO, FORWARD BULKHEAD, F.S. 1065, LONGERON 37 LEFT, AT DRAIN VALVE WAS CORRODED. REPAIRED AREA IAW REA B653-43879.SDR ABXA010475Line · defectiveTHE RIGHT HYDRAULIC QUANTITY DECREASED TO .35 QT. THEN STABILIZED WITH THE ENGINE DRIVIN PUMP DEPRESSURIZED AND THE ALTERNATING CURRENT MOTOR PUMP OFF. MAINTENANCE INSPECTED AND FOUND A HOLE IN P/N AE705777-78 HYDRAULIC LINE. THE LINE WAS REPLACED IAW B767 MM.SDR ABXA010436Valve · defectiveFLIGHT DECK TEMP. CONTROL FAILED TO CONTROL DESIRED TEMP. IN AUTO OR MANUAL. ALSO NO TEMP. CONTROL WITH ANY SELECTOR. DURING APPROACH, NAV EQUIPMENT BEGAN ERONEOUS INDICATIONS, AUTO PILOT DISENGAGED, F/O'S DU-1 FAILED, THEN F/O'S DU-2 FAILED. F/O'S FMC FAILED,SDR ABXA9900693Relay · stickingDISCRETE FIRE LIGHT ILLUMINATED DURING TAKEOFF, WITH NO OTHER INDICATIONS. AIR TURNBACK TO ILN. FOUND RELAY K693 STICKING ON P37. REPLACED RELAY. SYSTEM OPS CHECKED GOOD IAW B767 AMM.
Back to N783AX