# Service difficulty reports: N946VJ, cancelled Jul 17, 2003 A list on [N946VJ, cancelled Jul 17, 2003](https://openairdocs.org/deregistered/N946VJ-2003-07-17.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAD99007](https://openairdocs.org/sdr/USAAD99007.md): Battery · discharged · Jan 8, 1999 · N946VJ · Doug DC931 · Emergency Lighting > PHL - THE COCKPIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE COCKPIT EMERGENCY LIGHT. (M) - [SDR USAAD98191](https://openairdocs.org/sdr/USAAD98191.md): Power Supply · inoperative · Oct 28, 1998 · N946VJ · Doug DC931 · Emergency Lighting > DTW - THE GALLEY AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE GALLEY AREA EMERGENCY LIGHT POWER SUPPLY. (M) - [SDR USAAD98046](https://openairdocs.org/sdr/USAAD98046.md): Control Panel · failed · Mar 20, 1998 · N946VJ · Doug DC931 · AC Generation System > CMH - FLT 920 - ON TAKEOFF THE AC CROSSTIE LOCKOUT AND RIGHT GENERATOR OFF LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT GENERATOR CONTROL PANEL. (M) - [SDR USAAD97140](https://openairdocs.org/sdr/USAAD97140.md): Battery Pack · discharged · Aug 18, 1997 · N946VJ · Doug DC931 · Emergency Lighting > IND - FOUND GALLEY DOOR EMERGENCY DOOR LIGHT WEAK. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAA960370](https://openairdocs.org/sdr/USAA960370.md): Bulkhead · cracked · Apr 9, 1996 · N946VJ · Doug DC931 · Fuselage Main, Bulkhead > PIT - DURING C-4 CHECK INSPECTION, FOUND A 1.25 INCH AND 3 INCH CRACK IN REAR PRESSURE BULKHEAD Z-63 LEFT SIDE OF DOOR FRAME AT STATION 996. CUT OUT CRACKED AREAS AND INSTALLED FILLER AND DOUBLER PER USAIR EA NR 32410A. (M) - [SDR USAA970010](https://openairdocs.org/sdr/USAA970010.md): Bulkhead Doubler · cracked · Jan 9, 1996 · N946VJ · Doug DC931 · Fuselage Main, Bulkhead > PIT - DURING AGING VISIT 89K, FOUND 1.125 INCH CRACK IN 591013-13 BULKHEAD DOUBLER, 1.25 INCH CRACK IN 5910130-22 DOUBLER,.25 INCH CRACK IN 5910130-13 DOUBLER, 4.25 INCH CRACK IN THE RADIUS OF 5910130-13 DOUBLER. (M) - [SDR USAA950310](https://openairdocs.org/sdr/USAA950310.md): Skin · corroded · Mar 15, 1995 · N946VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION UNDER FWD BELLY AT MARKER BEACON ANTENNA. INSTALLED DOUBLER REPAIR PER USAIR EA 29959. (W) - [SDR USAA950311](https://openairdocs.org/sdr/USAA950311.md): Skin · corroded · Mar 7, 1995 · N946VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION STATION 912-996 SKIN PANEL 5919707 LONGERON 26R TO 26L SKIN PANEL 5911424 LONGERON 18R-26R. SPLICED IN 2 EACH SKIN PANELS PER USAIR EA 29955. (W) - [SDR USAA950312](https://openairdocs.org/sdr/USAA950312.md): Skin · corroded · Mar 6, 1995 · N946VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION LONGERON NR 1 AND SKIN LAP JOINT STATION 263-275 NR ADF LOOP AND STATION 300-308 NR 2 ADF LOOP ANTENNA. CLEANED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 29 AND USAIR EA 29614A. (W) - [SDR USAA950314](https://openairdocs.org/sdr/USAA950314.md): Skin · damaged · Feb 28, 1995 · N946VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR INSTALLED STATION 313-332 LONGERON 22-24 RIGHT. INSTALLED CLASS I REPAIR PER SRM 53-04 FIG 12B. (W) - [SDR USAA950318](https://openairdocs.org/sdr/USAA950318.md): Angle · cracked · Feb 24, 1995 · N946VJ · Doug DC931 · Nacelle/Pylon Structure > PIT - DURING Q-4 CHECK INSPECTION, FOUND ONE.5 INCH CRACK IN STATION 980 TOP PYLON TO FUSELAGE ATTACH ANGLE RT. INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10. (W) - [SDR USAA950319](https://openairdocs.org/sdr/USAA950319.md): Longeron · cracked · Feb 23, 1995 · N946VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4 CHECK INSPECTION, FOUND.25 INCH CRACK STATION 200 LONGERON 3 LEFT. SPLICED IN SECTION OF LONGERON PER SRM 53-02 FIG 2. (W) - [SDR USAA950317](https://openairdocs.org/sdr/USAA950317.md): Longeron · cracked · Feb 23, 1995 · N946VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4 CHECK INSPECTION, FOUND.25 INCH CRACK IN LONGERON 14 LEFT STATION 1038. SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17. (W) - [SDR USAA950315](https://openairdocs.org/sdr/USAA950315.md): Track · corroded · Feb 21, 1995 · N946VJ · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings > PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION RT INBOARD SEAT TRACK STATION 897 AND 965. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4E. (W) - [SDR USAA950323](https://openairdocs.org/sdr/USAA950323.md): Angle · cracked · Feb 16, 1995 · N946VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK INSPECTION, FOUND 2 INCH CRACK IN FUSELAGE EXT PYLON ATTACH ANGLE TOP RT PYLON STATION 1019. INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10. (W) - [SDR USAA950321](https://openairdocs.org/sdr/USAA950321.md): Web · corroded · Feb 15, 1995 · N946VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION RT LAV STATION 996 WEB. CLEANED CORROSION AND INSTALLED DOUBLER PER SRM 53-05 FIG 72. (W) - [SDR USAA950320](https://openairdocs.org/sdr/USAA950320.md): Seat Track · corroded · Feb 14, 1995 · N946VJ · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings > PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION STATION 896-965 LEFT OUTBOARD SEAT TRACK. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (W) - [SDR USAA950324](https://openairdocs.org/sdr/USAA950324.md): Corner Stop · cracked · Feb 13, 1995 · N946VJ · Doug DC931 · Emergency Exits > PIT - DURING Q-4 CHECK INSPECTION, FOUND.25 INCH CRACK LEFT FORWARD OVERWING EMERGENCY EXIT UPPER FORWARD CORNER DOOR STOP. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03. (W) - [SDR USAA950322](https://openairdocs.org/sdr/USAA950322.md): Seat Track · corroded · Feb 10, 1995 · N946VJ · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings > PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION FORWARD END OF LEFT OUTBOARD SEAT TRACK STATION 200. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (W) - [SDR USAA950316](https://openairdocs.org/sdr/USAA950316.md): Longeron · cracked · Feb 8, 1995 · N946VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4 CHECK INSPECTION, FOUND.25 INCH CRACK IN LONGERON 30 AT SPLICE BETWEEN BELTFRAMES AT STATION 465 AND 484. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 14. (W) - [SDR USAA950037](https://openairdocs.org/sdr/USAA950037.md): Windshield · cracked · Jan 22, 1995 · N946VJ · Doug DC931 · Flight Compartment Windows > DCA - FLT 545 - DURING CLIMB-OUT, THE FIRST OFFICER'S WINDSHIELD HAD AN ELECTRICAL ARCING WHICH IMMEDIATELY CAUSED APPROXIMATELY TWENTY CRACKS IN THE OUTSIDE WINDOW. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO DCA. MAINTENANCE REPLACED THE WINDSHIELD. ## 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 = 'N946VJ' AND deregistration_id = 'N946VJ-2003-07-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N946VJ-2003-07-17/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.