# Service difficulty reports: N931VJ, cancelled Jul 17, 2003 A list on [N931VJ, cancelled Jul 17, 2003](https://openairdocs.org/deregistered/N931VJ-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 USAAD98203](https://openairdocs.org/sdr/USAAD98203.md): Transducer · failed · Nov 14, 1998 · N931VJ · Doug DC931 · Stall Warning System > CLT-PHL - FLT 937 - AFTER TAKEOFF AND THE FLAPS AND SLATS WERE RETRACTED THE STALL WARNING LIGHT ILLUMINATED ON THE CAPTAINS SIDE AND THE HORN SOUNDED. THE LIGHT AND HORN OPERATED INTERMITTENTLY AS THE AIRCRAFT RETURNED TO THE FIELD. THE AIRCRAFT LANDED WITH - [SDR USAA980531](https://openairdocs.org/sdr/USAA980531.md): Frame · cracked · Oct 17, 1998 · N931VJ · Doug DC931 · Fuselage Main, Frame > PIT - DURING C-4 CHECK, FOUND.5 INCH TO.75 INCH CRACKS AT STATION 1104 AT FRAME LONGERON 13R. REPLACED FROM STA 1104 FROM 11R-22R FLOOR, FACTORY SPLICE PER SRM 53-03 FIG 30. (M) - [SDR USAA980530](https://openairdocs.org/sdr/USAA980530.md): Frame · cracked · Oct 17, 1998 · N931VJ · Doug DC931 · Fuselage Main, Frame > PIT - DURING C-4 CHECK, FOUND.5 INCH CRACKS AT LONGERON 14L, STATION 1104 CANTED FRAME. REPLACED FRAME FROM 11L TO 22L FLOOR FACTORY SPLICE PER SRM 53-03 FIG 30. (M) - [SDR USAA980529](https://openairdocs.org/sdr/USAA980529.md): Frame · cracked · Oct 17, 1998 · N931VJ · Doug DC931 · Fuselage Main, Frame > PIT - DURING C-4 CHECK, FOUND.5 INCH CRACKS AT 3 LONGERONS AT STATION 1104 LONGERONS 3R, 4R, AND 6R. REPLACED FRAME ASSEMBLY PER SRM 53-03 FIG 30. (M) - [SDR USAAD98090](https://openairdocs.org/sdr/USAAD98090.md): Power Supply · inoperative · May 17, 1998 · N931VJ · Doug DC931 · Emergency Lighting > CMH - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 5 AND 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M) - [SDR USAAD98092](https://openairdocs.org/sdr/USAAD98092.md): Battery · discharged · May 13, 1998 · N931VJ · Doug DC931 · Emergency Lighting > CMH - THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD98066](https://openairdocs.org/sdr/USAAD98066.md): Socket · corroded · Apr 8, 1998 · N931VJ · Doug DC931 · Emergency Lighting > CMH - THE AFT SECTION OF THE CABIN FLOOR TRACK EMERGENCY LIGHTS AND THE CATWALK LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED A LIGHT SOCKET FOR THE CATWALK LIGHTS AND REPAIRED A SHORTED WIRE NEAR THE TAIL CONE RELEASE HANDLE. (M) - [SDR USAA98054](https://openairdocs.org/sdr/USAA98054.md): Battery · discharged · Mar 28, 1998 · N931VJ · Doug DC931 · Emergency Lighting > CMH - THE LEFT NACELLE EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD98019](https://openairdocs.org/sdr/USAAD98019.md): Battery · discharged · Jan 8, 1998 · N931VJ · Doug DC931 · Emergency Lighting > PHL - THE GALLEY DOOR ESCAPE SLIDE LIGHT AND THE CEILING EMERGENCY LIGHTS IN ROWS 13 THROUGH 18 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) - [SDR 98ZZZM207](https://openairdocs.org/sdr/98ZZZM207.md): Battery · discharged · Jan 8, 1998 · N931VJ · Doug DC931 · Emergency Lighting > PHL - THE GALLEY DOOR ESCAPE SLIDE LIGHT AND THE CEILING EMERGENCY LIGHTS IN ROWS 13 THROUGH 18 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) - [SDR USAAD97190](https://openairdocs.org/sdr/USAAD97190.md): Light · failed · Oct 29, 1997 · N931VJ · Doug DC931 · Emergency Lighting > DCA - EMERGENCY FLOOR EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE TAIL CONE JETTISON HANDLE FLOOR LIGHT ASSEMBLY. (M) - [SDR USAA970308](https://openairdocs.org/sdr/USAA970308.md): Skin · chafed · Oct 27, 1997 · N931VJ · Doug DC931 · Fuselage Main, Bulkhead > PIT - DURING C-3 CHECK, FOUND 1 INCH LONG BY.029 INCH DEEP CHAF IN SKIN AT LEFT AFT SIDE OF REAR PRESS BULKHEAD JUST BELOW RADIAL 12. INSTALLED DOUBLERS PER EA 33652A. (M) - [SDR USAAD97039](https://openairdocs.org/sdr/USAAD97039.md): Spray Deflector · torn · Feb 18, 1997 · N931VJ · Doug DC931 · Nose/Tail Landing Gear > CLT/SDF - FLT 689 - RED NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION, AND AIR NOISE WAS HEARD. RETURNED TO FIELD. FOUND CHAFE STRIP ON SPRAY DEFLECTOR TORN. REMOVED STRIP, AND SERVICED STRUT WITH NITROGEN. (X) - [SDR USAAD97038](https://openairdocs.org/sdr/USAAD97038.md): Downlock Switch · failed · Feb 15, 1997 · N931VJ · Doug DC931 · Landing Gear Position and Warning > PIT/SYR - FLT 918 - ON APPROACH, NOSE GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. REPLACED NOSE LANDING GEAR DOWNLOCK WARNING SWITCH. CHECKS GOOD. (X) - [SDR USAAD96132](https://openairdocs.org/sdr/USAAD96132.md): Tire · failed · Sep 24, 1996 · N931VJ · Doug DC931 · Tire > FLT 1544 - ABE-PIT - ON DEPARTURE, CREW BELIEVED A NOSE TIRE HAD BLOWN. DIVERTED TO PHL WITH GEAR DOWN. NO GREEN DOWN ADN LOCKED LIGHT WAS OBSERVED ON LEFT MAIN GEAR. FOUND LEFT MAIN INBOARD TIRE RECAP FAILED. ALSO, FOUND LEFT MAIN GEAR DOWNLOCK SWITCH HAR - [SDR USAA960628](https://openairdocs.org/sdr/USAA960628.md): Skin · cracked · Sep 23, 1996 · N931VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING C-2 CHECK, FOUND.5 INCH CRACK IN FUSELAGE SKIN AT STATION 354 LONGERON 6L. CUT OUT CRACKED AREA, INSTALLED A FILLER AND AN EXTERNAL DOUBLER WITH BLIND FASTENERS PER SRM 53-04 FIG 12B SHEET 16 (CLASS III REPAIR). (M) - [SDR USAA960627](https://openairdocs.org/sdr/USAA960627.md): Skin · cracked · Sep 23, 1996 · N931VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING C-2 CHECK, FOUND.4375 INCH CRACK IN FUSELAGE SKIN AT STATION 658 BETWEEN R1 AND R2. DETECTED BY EDDY CURRENT. CUT OUT CRACKED AREA. INSTALLED A FILLER AND AN EXTERNAL DOUBLER WITH BLIND FASTENER PER SRM 53-04 FIG 12B SHEET 16 (CLASS II REPAIR) - [SDR USAAD96113](https://openairdocs.org/sdr/USAAD96113.md): Oil Press Sw · leaking · Aug 10, 1996 · N931VJ · Doug DC931 · Turbine Engine Oil System > FLT 458 - LGA-ROC - DURING CRUISE, APPROXIMATELY 70 MILES SOUTHEAST OF ROC, THE NR 2 ENGINE OIL PRESSURE GAUGE BEGAN TO FLUCTUATE. OIL QUANTITY BEGAN TO DECREASE, AND OIL TEMPERATURE BEGAN TO RISE. THE ENGINE WAS SHUT DOWN, AND THE AIRCRAFT LANDED AT ROC. S - [SDR USAAD96108](https://openairdocs.org/sdr/USAAD96108.md): Relay · failed · Jul 16, 1996 · N931VJ · Doug DC931 · Landing Gear Position and Warning > FLT 845 - CLT-SDF - NOSE GEAR UNSAFE LIGHT ON WITH GEAR RETRACTION.RECYCLED GEAR WITH SAME RESULT. RETURNED TO FIELD. REPLACED R2-28 RELAY.GEAR SWING CHECKS GOOD.(M) - [SDR USAAD96099](https://openairdocs.org/sdr/USAAD96099.md): Manifold · cracked · Jul 6, 1996 · N931VJ · Doug DC931 · Pneumatic Distribution System > FLT 2398 - PHL-BOS - AFTER TAKEOFF, AT 1500 FEET, RIGHT FIRE WARNING LIGHT AND BELL CAME ON. PULLED RIGHT ENGINE BACK TO IDLE, AND WARNING CEASED. RETURNED TO FIELD. FOUND 13TH STAGE CROSSOVER MANIFOLD BLOWN, AND ANTI-ICE CROSSOVER LEAKING AND EXPANSION JOI - [SDR USAA951076](https://openairdocs.org/sdr/USAA951076.md): Beltframe · cracked · Sep 22, 1995 · N931VJ · Doug DC931 · Fuselage Main, Frame > PIT - DURING C-1 CHECK INSPECTION, FOUND TWO.5 INCH BY.5 INCH CRACKS, FRAME STATION 1076 AT BOTH LONGERON NR 12 ATTACH FITTINGS. REMOVED DAMAGED SECTION OF BELTFRAME AND INSTALLED FILLER AND DOUBLERS PER SRM 53-03 FIG 34 SHEET 4. (M) - [SDR USAA951075](https://openairdocs.org/sdr/USAA951075.md): Longeron · cracked · Sep 22, 1995 · N931VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING C-1 CHECK INSPECTION, FOUND.75 INCH CRACK AT STATION 680, LONGERON 6L. REMOVED DAMAGED SECTION OF LONGERON AND SPLICED IN A NEW SECTION PER SRM 53-02. (M) - [SDR USAA951071](https://openairdocs.org/sdr/USAA951071.md): Angle · cracked · Sep 22, 1995 · N931VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING C-1 CHECK INSPECTION, FOUND.5 INCH CRACK RIGHT FORWARD DORSAL FIN DRAG ANGLE AT APPROXIMATELY STATION 1059. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) - [SDR USAA951073](https://openairdocs.org/sdr/USAA951073.md): Doubler · cracked · Sep 19, 1995 · N931VJ · Doug DC931 · Wing Miscellaneous Structure > PIT - DURING C-1 CHECK INSPECTION, FOUND 2 INCH CRACK IN LEFT WEB AND 2 INCH CRACK IN DOUBLER WING STATION XCW 58.5 LEFT. REMOVED AND REPLACED DOUBLER AND WEB PLATES PER USAIR EO NR 5790D573. (M) - [SDR USAA951074](https://openairdocs.org/sdr/USAA951074.md): Doubler · cracked · Sep 13, 1995 · N931VJ · Doug DC931 · Wing Miscellaneous Structure > PIT - DURING C-1 CHECK INSPECTION, FOUND.625 INCH CRACK RIGHT SIDE WING DOUBLER STATION XCN 58.5. ROUTED OUT CRACKED AREA AND REPAIRED PER USAIR EO NR 5790D573. (M) - [SDR USAA951072](https://openairdocs.org/sdr/USAA951072.md): Web · cracked · Sep 13, 1995 · N931VJ · Doug DC931 · Wing Miscellaneous Structure > PIT - DURING C-1 CHECK INSPECTION, FOUND.875 INCH CRACK IN WEB WING STATION XCW 58.5 RIGHT SIDE. ROUTED OUT AREA AND REPAIRED PER USAIR EO 5790D573. (M) - [SDR USAA950581](https://openairdocs.org/sdr/USAA950581.md): Longeron · cracked · Jun 7, 1995 · N931VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > IND - DURING BX CHECK VISIT AND SCHEDULED PRODUCTION CONTROL ITEM USAIR EO NR 5388D292F EDDY CURRENT INSPECTION OF EXTERNAL FUSELAGE SKIN FOUND A CRACK IN LONGERON NR 3R STATION 756. REMOVED CRACKED SECTION OF LONGERON AND ACCOMPLISHED SPLICE REPAIR PER SRM 5 ## 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 = 'N931VJ' AND deregistration_id = 'N931VJ-2003-07-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N931VJ-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.