N958VJ, cancelled Feb 7, 2005

Service difficulty reports · 31

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 = 'N958VJ' AND deregistration_id = 'N958VJ-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 USAAD01012Light · inoperativeIND - THE PORTABLE EMERGENCY LIGHT AT THE MAIN ENTRANCE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT. (M)Jan 19, 2001 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD00063Battery · dischargedDAY - THE MAIN ENTRANCE DOOR EMERGENCY EVACUATION SLIDE ACTIVATED LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Apr 27, 2000 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD00050Light · brokenPHL - THE ENTRY DOOR EMERGENCY LIGHT ASSEMBLY BRACKET WAS BROKEN. MAINTENANCE REPLACED THE ENTRY DOOR EMERGENCY LIGHT ASSEMBLY. (M)Apr 3, 2000 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD00024Coalescer Bag · contaminatedDTW-PIT - FLT 2201 - ON APPROACH INTO PIT, AN OIL LIKE SMELL IN THE CABIN WAS REPORTED COMING FROM BOTH PACKS WITH SMOKE DETECTORS IN LAVATORY SOUNDING OFF. FLIGHT LANDED AT PIT WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED INTAKES AND TURBINES OF BOTH ENGFeb 3, 2000 · N958VJ · Doug DC931 · Humidity Control SystemSDR USAAD99112Battery · dischargedIND - THE MAIN ENTRANCE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Aug 14, 1999 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD99087Engine · failedATL/PIT - FLT 7880 - AFTER ROTATION, THE LEFT ENGINE EGT CONTINUED TO CLIMB TO 600 DEGREES CELSIUS BEFORE ROLLING BACK. THE CREW REDUCED POWER WHEN THE ENGINE EXPERIENCED A COMPRESSOR STALL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAJun 30, 1999 · N958VJ · Doug DC931 · Engine (Turbine/Turboprop)SDR USAAD99033Power Supply · failedIND - THE RIGHT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT POWER SUPPLY. (M)Mar 1, 1999 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD98185Power Supply · inoperableDAY - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERABLE. MAINTENANCE REPLACED THE RIGHT NACELLE EMERGENCY LIGHT POWER SUPPLY. (X)Oct 6, 1998 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD98174Battery · dischargedPIT - THE LEFT AND RIGHT NACELLE EMERGENCY LIGHTS WERE INOPERABLE. MAINTENANCE REPLACED THE NACELLE LIGHT EMERGENCY LIGHT BATTERY PACKS. (X)Oct 6, 1998 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD98161Slide · failedPIT - THE AFT ESCAPE SLIDE MECHANISM FAILED TO DEPLOY THE SLIDE DURING FUNCTIONAL TEST. MAINTENANCE REPLACED THE SLIDE ASSY. (M)Sep 15, 1998 · N958VJ · Doug DC931 · Escape SlideSDR USAA980172Frame · corrodedPIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT FOUND CORROSION LEVEL 1 AT LOWER F/O EYEBROW WINDOW FRAME 3.25 INCH BY 9.5 INCH. INSTALLED TEMPORARY WINDOW PANEL AND INTERNAL AND EXTERNAL DOUBLERS PER EA 49467. (M)Apr 21, 1998 · N958VJ · Doug DC931 · Fuselage Main, FrameSDR USAAD97206O-Ring · failedPIT - FL 1006 - AIRCRAFT RETURNED TO FIELD UPON RECEIVING A NOSE GEAR UNSAFE WARNING LIGHT ON GEAR RETRACTION. MAINTENANCE REPLACED THE O-RING ON THE NOSE LANDING GEAR SCHRADER VALVE AND SERVICED THE STRUT. (M)Nov 8, 1997 · N958VJ · Doug DC931 · Nose/Tail Landing Gear Strut/AxleSDR USAAD97184Batery · dischargedPHL - SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY. (M)Oct 10, 1997 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD97080Power Supply · inoperativeDAY - FOUND THAT THE LAST THREE EMERGENCY LIGHTS STAY ON WHEN A/C IS POWERED DOWN. REPLACED BATTERY PACK FOR AFT CENTER AISLE OVERHEAD EMERGENCY LIGHTS. (M)Apr 29, 1997 · N958VJ · Doug DC931 · Emergency LightingSDR USAA960735T-Cap · corrodedPIT - DURING Q-4/C-6 CHECK, FOUND LEVEL 1 CORROSION AT T-CAP AT FS 996 AFT T-CAP BETWEEN LONGERON L29 TO R29. SPLICE IN SECTION OF T-CAP PER SRM 53-03 FIG 37 AND EA 33802A. CORROSION LEVEL 1. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA960710Floor Beam · corrodedPIT - DURING Q-4/C-6 CHECK, FOUND LEVEL 2 CORROSION AT STATION 996 FLOOR BEAM. INSTALLED NEW BEAM AND MFG DOUBLERS PER SRM 53-05 PAGE 212A FIG 72. CORROSION LEVEL 2. CORROSION TASK NR C58-53300. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Floor BeamSDR USAA960709Skin · corrodedPIT - DURING Q-4/C-6 CHECK, FOUND LEVEL II CORROSION AT NR 1 SLAT TRACK CUT OUT OUTBOARD LEADING EDGE OF LEFT WING. CUT OUT CORRODED AREA AND INSTALLED DOUBLER 9 INCH BY 7.5 INCH PER SRM 57-06 FIG 4. CORROSION LEVEL 2, COROSION TASK NR C11-57300. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Wing, Plate/SkinSDR USAA960708Skin · crackedPIT - DURING Q-4/C-6 CHECK, FOUND 1 INCH CRACK IN FUSELAGE SKIN LEFT FS 2095 LONGERON L3/L4. INSTALLED DOUBLER REPAIR PER EA 33693. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA960707Skin · crackedPIT - DURING Q-4/C-6 CHECK, FOUND .75 INCH CRACK IN RIGHT FUSELAGE SKIN FS 1038 LONGERON R14. INSTALLED DOUBLER PER SRM 53-04 FIG 18. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA960706Angle · crackedPIT - DURING Q-4/C-6 CHECK, FOUND 1.5 INCH CRACK IN LEFT DRAG ANGLE AT FS 1095 LEFT VERTICAL FIN. INSTALLED DOUBLER PER SRM 53-05 FIG 23B. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Vertical StabilizerSDR USAA960705Skin · crackedPIT - DURING Q-4/C-6 CHECK, FOUND .75 INCH CRACK IN FUSELAGE SKIN RIGHT FS 1095 BETWEEN LONGERON R3/R4. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA960704Angle · crackedPIT - DURING Q-4/C-6 CHECK, FOUND 1.5 INCH CRACK IN LEFT VERTICAL FIN DRAG ANGLE AT FS 1132. INSTALLED REPAIR DOUBLERS PER SRM 53-05 FIG 23 AND 23A. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Vertical StabilizerSDR USAA960703Angle · crackedPIT - DURING Q-4/C-6 CHECK, FOUND 1.25 INCH CRACK IN RIGHT DRAG ANGLE AT FS 1132 VERTICAL FIN DRAG ANGLE. INSTALLED DOUBLERS PER SRM 53-05 FIG 23 AND 23A. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Vertical StabilizerSDR USAA960702Skin · crackedPIT - DURIGN Q-4/C-6 CHECK, FOUND 4 INCH CRACK RIGHT WING AT XRS 214 OUTBOARD NR 5 SLAT TRACK CUT OUT RIGHT WING LEADING EDGE. 12 INCH BY 7 INCH DOUBLER REPAIR INSTALLED PER SRM 57-06 FIG 4. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Wing, Plate/SkinSDR USAA960701Cusp · crackedPIT - DURING Q-4/C-6 CHECK, FOUND 4 INCH CRACK IN CUSP MEMBRANE AT STATION 598 18R. REPLACED SECTION OF METAL REMOVED AT FACTORY SPLICE PER EA 33707. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA960700Longeron · crackedPIT - DURING Q-4/C-6 CHECK, FOUND 1 INCH CRACK AT FASTENERS AT STATION 522, 17L LONGERON. REPLACED 20 INCH PIECE OF LONGERON AND DOUBLERS INSTALLED PER SRM 53-10-17 TYPICAL REPAIR. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA960699Longeron · crackedPIT - DURING Q-4/C-6 CHECK, FOUND SEVERAL CRACKS BETWEEN STATION 639 AND STATION 737. SPLICED IN LONGERON FROM STATION 639 TO STATIO N737 PER SRM 53-02 FIG 2. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA960698Longeron · crackedPIT - DURING Q-4/C-6 CHECK, FOUND LONGERON CRACKED AT 23R AT STATION 229. INSTALLED SPLICE PER SRM 53-02 FIG 2. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA960697Cusp · damagedPIT - DURING Q-4/C-6 CHECK, FOUND HOLE MADE IN CUSP MEMBRANE BETWEEN STATION 658-680 (20 INCH) SECTION. REPLACED SECTION OF SKIN AREA FROM FACTORY SPLICE TO FACTORY SPLICE. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA960696Skin · crackedPIT - DURING Q-4/C-6 CHECK, FOUND .375 INCH CRACK IN SKIN AT DOOR JAMB FS 427 R27. INSTALLED DOUBLERS PER SRO DWG 9530117. (M)Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950035Vor Receiver · inoperativeCLT - FLT 8028 - THE NR 1 NAV IS 45 PERCENT OFF. IT IS TO TTHE RIGHT OF THE NR 2 NAV. MAINTENANCE REPLACED THE VOR REC SYSTEM. OPERATIONS CHECK GOOD. (Z)Jan 20, 1995 · N958VJ · Doug DC931 · Visual Omnirange (VOR) System
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