N997VJ, cancelled Feb 7, 2005
Service difficulty reports · 33
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 = 'N997VJ' AND deregistration_id = 'N997VJ-2005-02-07' 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 = 'N997VJ' AND deregistration_id = 'N997VJ-2005-02-07' 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 USAA000975Door Frame · crackedPIT - FOUND FRAME CRACKED 2 INCHES, VENTRAL DOOR FRAME RIGHT SIDE ABV TOP LIGHTENING HOLE. INSTALLED ANGLE DOUBLERS AND Z DOUBLERS PER SRM 53-05 FIG 27. (M)SDR USAAD99081Battery · dischargedIND - THE FORWARD ENTRY DOOR EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE BATTERY FOR THE FORWARD ENTRY DOOR EMERGENCY LIGHT. (M)SDR USAAD99079Valve · leakingPIT-DAY - FLT 827 - AFTER TAKEOFF THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE THROTTLE WAS REDUCED, BUT WITH INCREASE IN POWER THE LIGHT CAME BACK ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENASDR 99ZZZM383Duct · leakingPIT-DAY - FLT 827 - AFTER TAKEOFF THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE THROTTLE WAS REDUCED, BUT WITH INCREASE IN POWER THE LIGHT CAME BACK ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENASDR USAAD99058Battery · dischargedTHE TAIL CONE ACTIVATED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)SDR USAAD98207Link · failedLGA-GSO - FLT 1621 - UPON LANDING GEAR RETRACTION AFTER TAKEOFF THE NOSE GEAR DOOR DID NOT CLOSE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT NOSE GEAR DOOR LOCK LINK. (M)SDR USAA980360Pan · corrodedPIT - DURING UNSCHEDULED MAINTENANCE, FOUND 2 INCH BY 10 INCH AREA OF CORROSION AT E/E COMPARTMENT DOOR PAN AND LT INTERCOSTAL. DEFECTIVE PART REPLACED WITH INDENTICAL PART NR 1199671 AND 1095915. (M)SDR 98ZZZM716Intercostal · corrodedPIT - DURING UNSCHEDULED MAINTENANCE, FOUND 2 INCH BY 10 INCH AREA OF CORROSION AT E/E COMPARTMENT DOOR PAN AND LT INTERCOSTAL. DEFECTIVE PART REPLACED WITH INDENTICAL PART NR 1199671 AND 1095915. (M)SDR USAA980393Frame · crackedPIT - DURING C-2 CHECK, FOUND 4 INCH FWD POCKET CRACK AND 4 INCH AFT POCKET CRACK TO TRAPAZOIDAL HOLE AT FS 718 FRAME. REMOVED AND REPLACED MAIN FRAME 718 PER DWG 392031. (M)SDR USAAD98109Battery · dischargedPIT - THE AFT FUSELAGE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT FUSELAGE EMERGENCY LIGHT BATTERIES. (M)SDR USAAD98107Battery · dischargedCMH - THE RIGHT NACELLE EVACUATION LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT NACELLE EVACUATION LIGHT BATTERY. (M)SDR USAAD98077Power Supply · failedCMH - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 4 AND 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (X)SDR USAAD98013Power Supply · failedDTW - CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 13 THROUGH 19. MAINTENANCE REPLACED THE POWER SUPPLY (M)SDR USAAD97215Battery · dischargedIND - TAILCONE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)SDR USAAD97166Dc Bus · malfunctionedSYR - FL 1629 - EN ROUTE YOW-PIT - CREW RECEIVED VARIOUS OFF FLAGS AND SYSTEM FAIL INDICATIONS, INCLUDING THE NR 2 GYRO FLAG, CAPTAINS COMPASS FLAG, AUTOPILOT INOP, MACH TRIM 'INOP' LIGHT ON, AND NAV INSTRUMENT FAILURE MONITOR LIGHT FLASHING, WHICH INDICATED TSDR USAAD97147Battery · dischargedBWI - FOUND OVERHEAD EMERGENCY LIGHTING IN ROWS 16 THROUGH 19 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)SDR USAAD97145Battery · dischargedIND - FOUND CEILING MOUNTED EMERGENCY LIGHTS IN ROWS 13 THROUGH 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)SDR USAAD97106O-Ring · failedDTW/PIT - FLT 992 - ON APPROACH, THE NR 1 OIL QUANTITY STARTED TO VARY AND OIL PRESSURE STARTED TO DROP. SHUT ENGINE DOWN. SINGLE ENGINE TIME 10 MINUTES. REPLACED LEFT ENGINE OIL FILTER CAVITY SLEEVE O-RING. (X)SDR USAAD96116Stall Warn Comp · failedFLT 844 - PIT-DTW - AFTER ROTATION, THE STALL WARNING INDICATION WENT OFF. RETURNED TO FIELD. REPLACED LEFT STALL WARNING COMPUTER. (M)SDR USAAD96065Battery Pack · dischargedCOCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (X)SDR USAA960346Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN FASTENER HOLES LONGERON 24L STATION 160 AND 200. REPLACED SECTION OF LONGERON BY SPLICING PER SRM 53-02 FIG 2. (M)SDR USAA960345Pan · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .5 INCH CRACK IN FORWARD LEFT OVERWING EMERGENCY EXIT IN DOOR PAN BOTTOM FORWARD NR 5 STOP. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03 AND SRM 52-05 FIG 51. (M)SDR USAA960344Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK AT FASTENER HOLES STATION 160 LONGERON 25L. SPLICED IN NEW SECTION OF LONGERON STATION 150 TO 190 PER SRM 53-02 FIG 2. (M)SDR USAA960343Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN LONGERON 12R AT ATTACH FASTENERS STATION 965. REPLACED SECTION OF LONGERON BY SPLICING PER USAIR TYPICAL REPAIR 53-10-17. (M)SDR USAA960342Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN LONGERON 4L AT STATION 180. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M)SDR USAA960341Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACKS AT FASTENER HOLES LONGERON 23L STATION 180 AND STATION 200. SPLICED IN SECTION OF LONGERON FROM STATION 160 TO STATION 230 PER SRM 53-02 FIG 2. (M)SDR USAA960340Belt Frame · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND A .25 INCH CRACK AT FASTENER STA 180, BELT FRAME LONGERON 23L. INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-03, FIGURE 4. (X)SDR USAA960339Longeron · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND 1 INCH CRACK IN LONGERON 17L, AT STATION 945. SPLICED IN LONGERON SECTION PER USAIR TYPICAL REPAIR 53-10-17. (M)SDR USAA960338Cusp Membrane · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND TWO 2 INCH CRACKS IN CUSP MEMBRANE STATION 617 RIGHT SIDE. REPLACED SECTION OF CUSP MEMBRANE FROM STATION 598 TO 637 PER SRM 53-05 FIG 97. (M)SDR USAA960337Skin · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND 1.5 INCH CRACK UPPER LEADING EDGE SURFACE HORIZONTAL STABILIZER LEFT SIDE APPROXIMATELY 6 FEET OUTBOARD OF VERT STAB. INSTALLED DOUBLER REPAIR .071 2024TS ALU PER SRM 55-03 FIG 3 AND SRM 55-01 FIG 2. (M)SDR USAA960292Skin · crackedPIT - DURING Q-4 INSPECTION DISCOVERED A CRACK 38.75 INCH LONG FORWARD FUSELAGE EXTERIOR SKIN FROM XPONDER ANT TO TCAS ANT STATION 247 TO 285 RUNNING ALONG LONGERON NR 1. AREA UNDER ADF CORRODED. (M)SDR USAA950255Frame · crackedIND - DURING SCHEDULED CX-5 INSPECTION, FOUND .5 INCH CRACK IN FRAME AT STATION 389 AT LONGERON 17R. CUT OUT DAMAGED AREA, INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-04 FIG 35 AND USAIR EA 29574. (W)SDR USAA950114Frame · crackedIND - DURING CX-5 CHECK INSPECTION ACCOMPLISHED SID INSPECTION PSE 53.09.001A, FOUND .5 INCH CRACK AT STATION 389 LONGERON 17R. (VISUAL INSPECTION). CUT OUT DAMAGED AREA, INSTALLED FILLER/DOUBLER TYPE REPAIR PER DAC SRM 53-04 FIG 35 AND USAIR EA 29574. (Z)
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