N913VJ, cancelled Feb 7, 2005

Service difficulty reports · 22

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 = 'N913VJ' AND deregistration_id = 'N913VJ-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.

SDR USAA000733Pan · crackedPIT - C-5 - PAN HAD LONG CRACK, 0.250 INCH, DOOR PAN AT CENTER AFT STOP. INSTALLED DOUBLER PER DC-9 SRM 52-15, FIG 51. (X)May 16, 2000 · N913VJ · Doug DC931 · Passenger/Crew DoorsSDR USAA991458Skin · corrodedPIT - DURING RON, FOUND NUMEROUS AREAS AFFECTED OVER LISTED SKIN AREA CORROSION ALONG FRAMES, LONGERONS AND AT ANTENNA DOUBLERS AT STATION 230 TO STATION 579, LONGERON 26L TO LONGERON 26R. CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (Dec 19, 1999 · N913VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA991457Skin · corrodedPIT - DURING VISUAL (RON CHECK) FOUND CORROSION ON, UNDER AND AROUND PREVIOUS REPAIR (5 INCH BY 7 INCH) ON SKIN ON DOUBLER AT STATION 579-604 LONGERON 28L TO 28R. CORROSION LEVEL 2. REPLACED REPAIR DOUBLERS WITH NEW, REMOVED CORROSION PER SRM 53-04 FIG 43 SHDec 19, 1999 · N913VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA991456Fitting · crackedPIT - DURING SHEET METAL REPAIR OPEN UP, FOUND 4 INCH CRACK AND 1.5 INCH BY 2 INCH CORRODED AREA (INTERGRANUAR) AT LONGERON 30 AFT END FORWARD CARGO AT T-CAP. REPLACED WITH IDENTICAL PART NUMBER. (M)Dec 19, 1999 · N913VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAAD99123Battery · dischargedIND - THE FORWARD PASSENGER CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD PASSENGER CABIN OVERHEAD EMERGENCY LIGHT BATTERIES. (M)Sep 9, 1999 · N913VJ · Doug DC931 · Emergency LightingSDR USAAD990092Light · failedIND - THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LIGHT AND THE EMERGENCY LIGHT ABOVE THE TAILCONE SLIDE WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY FOR THE MAIN ENTRANCE SLIDE LIGHT AND THE BATTERY FOR THE EMERGENCY LIGHT ABOVE THE TAILCONE SLIDE. Jul 9, 1999 · N913VJ · Doug DC931 · Emergency LightingSDR 99ZZZX2828Battery · dischargedIND - THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LIGHT AND THE EMERGENCY LIGHT ABOVE THE TAILCONE SLIDE WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY FOR THE MAIN ENTRANCE SLIDE LIGHT AND THE BATTERY FOR THE EMERGENCY LIGHT ABOVE THE TAILCONE SLIDE. Jul 9, 1999 · N913VJ · Doug DC931 · Emergency LightingSDR USAAD99063Battery · dischargedIND - THE SERVICE DOOR SLIDE LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR SLIDE LIGHT BATTERY. (M)May 7, 1999 · N913VJ · Doug DC931 · Emergency LightingSDR USAA990190Skin · crackedPIT - DURING MAINTENANCE WALK AROUND, FOUND 3 INCH CRACK AND 9 INCH VERTICAL CRACK ON FUSELAGE SKIN BETWEEN STATION 1155.335 AND STATION 1168.895 LEFT SIDE. INSTALLED EXTERNAL DOUBLER, CUTOUT DAMAGE PER SRM 53-04 FIG 12B CLASS II REPAIR. (M)Mar 5, 1999 · N913VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAAD99023Battery · dischargedDTW - THE GALLEY DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE GALLEY DOOR SLIDE EMERGENCY LIGHT BATTERY. (M)Feb 8, 1999 · N913VJ · Doug DC931 · Emergency LightingSDR USAAD99028Battery · dischargedDTW - THE GALLEY SERVICE DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE BATTERY FOR THE GALLEY SERVICE DOOR SLIDE EMERGENCY LIGHT. (M)Feb 7, 1999 · N913VJ · Doug DC931 · Emergency LightingSDR USAAD98111Battery · dischargedIND - THE TAIL COMPARTMENT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE TAIL COMPARTMENT EMERGENCY LIGHT BATTERIES. (M)Jun 20, 1998 · N913VJ · Doug DC931 · Emergency LightingSDR USAAD98016Cylinder · failedCTL - FLT 369 - ON APPROACH, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WHEN THE LANDIG GEAR WAS LOWERED. THE FLT CREW RECYCLED THE GEAR BUT THE LIGHT REMAINED. THE FLT CREW THEN PULLED THE MANUAL GEAR RELEASE LEVER IN THE COCKPIT. THE FLIGHT LANDED WITHOUT INCJan 23, 1998 · N913VJ · Doug DC931 · Landing Gear Retraction/Extension SystemSDR USAAD97212Seal · out of positionBWI - FLT 1121 - AFTER TAKEOFF, CREW HEARD A LOUD BANGING SOUND AT THE R1 DOOR. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. LANDING WEIGHT WAS 101,000 LBS. MAINTENANCE REMOVED INNER COSMETIC SEAL THAT WAS CAUGHT UNDER THE DOOR AND PROTRUDING OUTSIDENov 21, 1997 · N913VJ · Doug DC931 · Passenger/Crew DoorsSDR USAAD97165Power Supply · inoperativePHL - FOUND AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M)Sep 18, 1997 · N913VJ · Doug DC931 · Emergency LightingSDR USAAD97164Batteries · dischargedPHL - FOUND FORWARD OVERWING EMERGENCY LIGHTS WEAK. MAINTENANCE REPLACED THE BATTERIES. (M)Sep 18, 1997 · N913VJ · Doug DC931 · Emergency LightingSDR USAAD97098Battery Pack · failedCMH - FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M)May 30, 1997 · N913VJ · Doug DC931 · Emergency LightingSDR USAA970135Frame · crackedPIT - DURING Q-1 CHECK, FOUND 4 INCH CRACK AT STA 718 RIGHT SIDE MAIN FRAME. REPLACED WITH MODIFIED PART NR C/C 1193213. REPLACED PER DACO DRAWING 5928626. (X)Apr 14, 1997 · N913VJ · Doug DC931 · Fuselage Main, FrameSDR USAA970134Frame · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK AT LT SIDE STA 718 MAIN FRAME. INSTALLED MODIFIED PART NR 9919618-IN. (X)Apr 14, 1997 · N913VJ · Doug DC931 · Fuselage Main, FrameSDR USAA970133Skin · corrodedPIT - DURING Q-1 CHECK, FOUND FUSELAGE SKIN CORRODED AT ANTENNA DOUBLER 2 INCHES BY 3 INCHES, CRACKED AT 2 FASTENERS AT STA 503, LONGERON 30. REPAIRED CUT OUT DAMAGED AREA. INSTALLED INNER AND OUTER DOUBLERS PER SRM 53-04 FIG 44. CORROSION TASK NR C50-53300Apr 14, 1997 · N913VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA970132Fitting · crackedPIT - DURING Q-1 CHECK, FOUND .25 INCH CRACK AT STA 669 LT (APPROX 12 INCHES UPWARD OF LOWER KEEL T-ANGLE) AT FITTING. INSTALLED DOUBLERS AND REPAIR ANGLES PER SRM 53-03 FIG 11. (X)Apr 14, 1997 · N913VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAAD97068Connector · misalignedPHL/ATL - FLT 1073 LEFT OIL STRAINER CLOGGING LIGHT ILLUMINATED. RETURNED TO FIELD. REMOVED AND REPLACED OIL FILTER. FOUND PIN MIS-ALIGNED ON DIFFERENTIAL PRESSURE SWITCH. RE-ALIGNED PIN. RAN ENGINE AND PERFORMED LEAK CHECK. (X)Apr 11, 1997 · N913VJ · Doug DC931 · Engine Oil Indicating System
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