# Service difficulty reports: N958VJ, cancelled Feb 7, 2005 A list on [N958VJ, cancelled Feb 7, 2005](https://openairdocs.org/deregistered/N958VJ-2005-02-07.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAD01012](https://openairdocs.org/sdr/USAAD01012.md): Light · inoperative · Jan 19, 2001 · N958VJ · Doug DC931 · Emergency Lighting > IND - THE PORTABLE EMERGENCY LIGHT AT THE MAIN ENTRANCE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT. (M) - [SDR USAAD00063](https://openairdocs.org/sdr/USAAD00063.md): Battery · discharged · Apr 27, 2000 · N958VJ · Doug DC931 · Emergency Lighting > DAY - THE MAIN ENTRANCE DOOR EMERGENCY EVACUATION SLIDE ACTIVATED LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD00050](https://openairdocs.org/sdr/USAAD00050.md): Light · broken · Apr 3, 2000 · N958VJ · Doug DC931 · Emergency Lighting > PHL - THE ENTRY DOOR EMERGENCY LIGHT ASSEMBLY BRACKET WAS BROKEN. MAINTENANCE REPLACED THE ENTRY DOOR EMERGENCY LIGHT ASSEMBLY. (M) - [SDR USAAD00024](https://openairdocs.org/sdr/USAAD00024.md): Coalescer Bag · contaminated · Feb 3, 2000 · N958VJ · Doug DC931 · Humidity Control System > DTW-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 ENG - [SDR USAAD99112](https://openairdocs.org/sdr/USAAD99112.md): Battery · discharged · Aug 14, 1999 · N958VJ · Doug DC931 · Emergency Lighting > IND - THE MAIN ENTRANCE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD99087](https://openairdocs.org/sdr/USAAD99087.md): Engine · failed · Jun 30, 1999 · N958VJ · Doug DC931 · Engine (Turbine/Turboprop) > ATL/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. MA - [SDR USAAD99033](https://openairdocs.org/sdr/USAAD99033.md): Power Supply · failed · Mar 1, 1999 · N958VJ · Doug DC931 · Emergency Lighting > IND - THE RIGHT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT POWER SUPPLY. (M) - [SDR USAAD98185](https://openairdocs.org/sdr/USAAD98185.md): Power Supply · inoperable · Oct 6, 1998 · N958VJ · Doug DC931 · Emergency Lighting > DAY - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERABLE. MAINTENANCE REPLACED THE RIGHT NACELLE EMERGENCY LIGHT POWER SUPPLY. (X) - [SDR USAAD98174](https://openairdocs.org/sdr/USAAD98174.md): Battery · discharged · Oct 6, 1998 · N958VJ · Doug DC931 · Emergency Lighting > PIT - THE LEFT AND RIGHT NACELLE EMERGENCY LIGHTS WERE INOPERABLE. MAINTENANCE REPLACED THE NACELLE LIGHT EMERGENCY LIGHT BATTERY PACKS. (X) - [SDR USAAD98161](https://openairdocs.org/sdr/USAAD98161.md): Slide · failed · Sep 15, 1998 · N958VJ · Doug DC931 · Escape Slide > PIT - THE AFT ESCAPE SLIDE MECHANISM FAILED TO DEPLOY THE SLIDE DURING FUNCTIONAL TEST. MAINTENANCE REPLACED THE SLIDE ASSY. (M) - [SDR USAA980172](https://openairdocs.org/sdr/USAA980172.md): Frame · corroded · Apr 21, 1998 · N958VJ · Doug DC931 · Fuselage Main, Frame > PIT - 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) - [SDR USAAD97206](https://openairdocs.org/sdr/USAAD97206.md): O-Ring · failed · Nov 8, 1997 · N958VJ · Doug DC931 · Nose/Tail Landing Gear Strut/Axle > PIT - 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) - [SDR USAAD97184](https://openairdocs.org/sdr/USAAD97184.md): Batery · discharged · Oct 10, 1997 · N958VJ · Doug DC931 · Emergency Lighting > PHL - SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY. (M) - [SDR USAAD97080](https://openairdocs.org/sdr/USAAD97080.md): Power Supply · inoperative · Apr 29, 1997 · N958VJ · Doug DC931 · Emergency Lighting > DAY - 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) - [SDR USAA960735](https://openairdocs.org/sdr/USAA960735.md): T-Cap · corroded · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - 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) - [SDR USAA960710](https://openairdocs.org/sdr/USAA960710.md): Floor Beam · corroded · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Floor Beam > PIT - 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) - [SDR USAA960709](https://openairdocs.org/sdr/USAA960709.md): Skin · corroded · Oct 28, 1996 · N958VJ · Doug DC931 · Wing, Plate/Skin > PIT - 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) - [SDR USAA960708](https://openairdocs.org/sdr/USAA960708.md): Skin · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - 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) - [SDR USAA960707](https://openairdocs.org/sdr/USAA960707.md): Skin · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - 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) - [SDR USAA960706](https://openairdocs.org/sdr/USAA960706.md): Angle · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Vertical Stabilizer > PIT - 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) - [SDR USAA960705](https://openairdocs.org/sdr/USAA960705.md): Skin · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - 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) - [SDR USAA960704](https://openairdocs.org/sdr/USAA960704.md): Angle · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Vertical Stabilizer > PIT - 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) - [SDR USAA960703](https://openairdocs.org/sdr/USAA960703.md): Angle · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Vertical Stabilizer > PIT - 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) - [SDR USAA960702](https://openairdocs.org/sdr/USAA960702.md): Skin · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Wing, Plate/Skin > PIT - 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) - [SDR USAA960701](https://openairdocs.org/sdr/USAA960701.md): Cusp · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - 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) - [SDR USAA960700](https://openairdocs.org/sdr/USAA960700.md): Longeron · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - 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) - [SDR USAA960699](https://openairdocs.org/sdr/USAA960699.md): Longeron · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - 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) - [SDR USAA960698](https://openairdocs.org/sdr/USAA960698.md): Longeron · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4/C-6 CHECK, FOUND LONGERON CRACKED AT 23R AT STATION 229. INSTALLED SPLICE PER SRM 53-02 FIG 2. (M) - [SDR USAA960697](https://openairdocs.org/sdr/USAA960697.md): Cusp · damaged · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - 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) - [SDR USAA960696](https://openairdocs.org/sdr/USAA960696.md): Skin · cracked · Oct 28, 1996 · N958VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - 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) - [SDR USAA950035](https://openairdocs.org/sdr/USAA950035.md): Vor Receiver · inoperative · Jan 20, 1995 · N958VJ · Doug DC931 · Visual Omnirange (VOR) System > CLT - 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) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N958VJ-2005-02-07/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.