# Service difficulty reports: N997VJ, cancelled Feb 7, 2005 A list on [N997VJ, cancelled Feb 7, 2005](https://openairdocs.org/deregistered/N997VJ-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 USAA000975](https://openairdocs.org/sdr/USAA000975.md): Door Frame · cracked · Jun 28, 2000 · N997VJ · Doug DC931 · Passenger/Crew Doors > PIT - FOUND FRAME CRACKED 2 INCHES, VENTRAL DOOR FRAME RIGHT SIDE ABV TOP LIGHTENING HOLE. INSTALLED ANGLE DOUBLERS AND Z DOUBLERS PER SRM 53-05 FIG 27. (M) - [SDR USAAD99081](https://openairdocs.org/sdr/USAAD99081.md): Battery · discharged · Jun 15, 1999 · N997VJ · Doug DC931 · Emergency Lighting > IND - THE FORWARD ENTRY DOOR EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE BATTERY FOR THE FORWARD ENTRY DOOR EMERGENCY LIGHT. (M) - [SDR USAAD99079](https://openairdocs.org/sdr/USAAD99079.md): Valve · leaking · Jun 12, 1999 · N997VJ · Doug DC931 · Pneumatic Distribution System > PIT-DAY - FLT 827 - AFTER TAKEOFF THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE THROTTLE WAS REDUCED, BUT WITH INCREASE IN POWER THE LIGHT CAME BACK ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENA - [SDR 99ZZZM383](https://openairdocs.org/sdr/99ZZZM383.md): Duct · leaking · Jun 12, 1999 · N997VJ · Doug DC931 · Pneumatic Distribution System > PIT-DAY - FLT 827 - AFTER TAKEOFF THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE THROTTLE WAS REDUCED, BUT WITH INCREASE IN POWER THE LIGHT CAME BACK ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENA - [SDR USAAD99058](https://openairdocs.org/sdr/USAAD99058.md): Battery · discharged · Apr 25, 1999 · N997VJ · Doug DC931 · Emergency Lighting > THE TAIL CONE ACTIVATED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD98207](https://openairdocs.org/sdr/USAAD98207.md): Link · failed · Nov 18, 1998 · N997VJ · Doug DC931 · Landing Gear Door Retract Section > LGA-GSO - FLT 1621 - UPON LANDING GEAR RETRACTION AFTER TAKEOFF THE NOSE GEAR DOOR DID NOT CLOSE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT NOSE GEAR DOOR LOCK LINK. (M) - [SDR USAA980360](https://openairdocs.org/sdr/USAA980360.md): Pan · corroded · Aug 17, 1998 · N997VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING UNSCHEDULED MAINTENANCE, FOUND 2 INCH BY 10 INCH AREA OF CORROSION AT E/E COMPARTMENT DOOR PAN AND LT INTERCOSTAL. DEFECTIVE PART REPLACED WITH INDENTICAL PART NR 1199671 AND 1095915. (M) - [SDR 98ZZZM716](https://openairdocs.org/sdr/98ZZZM716.md): Intercostal · corroded · Aug 17, 1998 · N997VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING UNSCHEDULED MAINTENANCE, FOUND 2 INCH BY 10 INCH AREA OF CORROSION AT E/E COMPARTMENT DOOR PAN AND LT INTERCOSTAL. DEFECTIVE PART REPLACED WITH INDENTICAL PART NR 1199671 AND 1095915. (M) - [SDR USAA980393](https://openairdocs.org/sdr/USAA980393.md): Frame · cracked · Jul 1, 1998 · N997VJ · Doug DC931 · Fuselage Main, Frame > PIT - DURING C-2 CHECK, FOUND 4 INCH FWD POCKET CRACK AND 4 INCH AFT POCKET CRACK TO TRAPAZOIDAL HOLE AT FS 718 FRAME. REMOVED AND REPLACED MAIN FRAME 718 PER DWG 392031. (M) - [SDR USAAD98109](https://openairdocs.org/sdr/USAAD98109.md): Battery · discharged · Jun 17, 1998 · N997VJ · Doug DC931 · Emergency Lighting > PIT - THE AFT FUSELAGE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT FUSELAGE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD98107](https://openairdocs.org/sdr/USAAD98107.md): Battery · discharged · Jun 7, 1998 · N997VJ · Doug DC931 · Emergency Lighting > CMH - THE RIGHT NACELLE EVACUATION LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT NACELLE EVACUATION LIGHT BATTERY. (M) - [SDR USAAD98077](https://openairdocs.org/sdr/USAAD98077.md): Power Supply · failed · May 1, 1998 · N997VJ · Doug DC931 · Emergency Lighting > CMH - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 4 AND 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (X) - [SDR USAAD98013](https://openairdocs.org/sdr/USAAD98013.md): Power Supply · failed · Jan 12, 1998 · N997VJ · Doug DC931 · Emergency Lighting > DTW - CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 13 THROUGH 19. MAINTENANCE REPLACED THE POWER SUPPLY (M) - [SDR USAAD97215](https://openairdocs.org/sdr/USAAD97215.md): Battery · discharged · Nov 21, 1997 · N997VJ · Doug DC931 · Emergency Lighting > IND - TAILCONE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAD97166](https://openairdocs.org/sdr/USAAD97166.md): Dc Bus · malfunctioned · Sep 24, 1997 · N997VJ · Doug DC931 · AC Power Distribution System > SYR - FL 1629 - EN ROUTE YOW-PIT - CREW RECEIVED VARIOUS OFF FLAGS AND SYSTEM FAIL INDICATIONS, INCLUDING THE NR 2 GYRO FLAG, CAPTAINS COMPASS FLAG, AUTOPILOT INOP, MACH TRIM 'INOP' LIGHT ON, AND NAV INSTRUMENT FAILURE MONITOR LIGHT FLASHING, WHICH INDICATED T - [SDR USAAD97147](https://openairdocs.org/sdr/USAAD97147.md): Battery · discharged · Aug 29, 1997 · N997VJ · Doug DC931 · Emergency Lighting > BWI - FOUND OVERHEAD EMERGENCY LIGHTING IN ROWS 16 THROUGH 19 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) - [SDR USAAD97145](https://openairdocs.org/sdr/USAAD97145.md): Battery · discharged · Aug 22, 1997 · N997VJ · Doug DC931 · Emergency Lighting > IND - FOUND CEILING MOUNTED EMERGENCY LIGHTS IN ROWS 13 THROUGH 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) - [SDR USAAD97106](https://openairdocs.org/sdr/USAAD97106.md): O-Ring · failed · Jun 20, 1997 · N997VJ · Doug DC931 · Turbine Engine Oil System > DTW/PIT - FLT 992 - ON APPROACH, THE NR 1 OIL QUANTITY STARTED TO VARY AND OIL PRESSURE STARTED TO DROP. SHUT ENGINE DOWN. SINGLE ENGINE TIME 10 MINUTES. REPLACED LEFT ENGINE OIL FILTER CAVITY SLEEVE O-RING. (X) - [SDR USAAD96116](https://openairdocs.org/sdr/USAAD96116.md): Stall Warn Comp · failed · Aug 18, 1996 · N997VJ · Doug DC931 · Stall Warning System > FLT 844 - PIT-DTW - AFTER ROTATION, THE STALL WARNING INDICATION WENT OFF. RETURNED TO FIELD. REPLACED LEFT STALL WARNING COMPUTER. (M) - [SDR USAAD96065](https://openairdocs.org/sdr/USAAD96065.md): Battery Pack · discharged · May 16, 1996 · N997VJ · Doug DC931 · Emergency Lighting > COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (X) - [SDR USAA960346](https://openairdocs.org/sdr/USAA960346.md): Longeron · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4/C-6 INSPECTION, FOUND.25 INCH CRACK IN FASTENER HOLES LONGERON 24L STATION 160 AND 200. REPLACED SECTION OF LONGERON BY SPLICING PER SRM 53-02 FIG 2. (M) - [SDR USAA960345](https://openairdocs.org/sdr/USAA960345.md): Pan · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Emergency Exits > PIT - DURING Q-4/C-6 INSPECTION, FOUND.5 INCH CRACK IN FORWARD LEFT OVERWING EMERGENCY EXIT IN DOOR PAN BOTTOM FORWARD NR 5 STOP. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03 AND SRM 52-05 FIG 51. (M) - [SDR USAA960344](https://openairdocs.org/sdr/USAA960344.md): Longeron · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4/C-6 INSPECTION, FOUND.25 INCH CRACK AT FASTENER HOLES STATION 160 LONGERON 25L. SPLICED IN NEW SECTION OF LONGERON STATION 150 TO 190 PER SRM 53-02 FIG 2. (M) - [SDR USAA960343](https://openairdocs.org/sdr/USAA960343.md): Longeron · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4/C-6 INSPECTION, FOUND.25 INCH CRACK IN LONGERON 12R AT ATTACH FASTENERS STATION 965. REPLACED SECTION OF LONGERON BY SPLICING PER USAIR TYPICAL REPAIR 53-10-17. (M) - [SDR USAA960342](https://openairdocs.org/sdr/USAA960342.md): Longeron · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4/C-6 INSPECTION, FOUND.25 INCH CRACK IN LONGERON 4L AT STATION 180. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) - [SDR USAA960341](https://openairdocs.org/sdr/USAA960341.md): Longeron · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4/C-6 INSPECTION, FOUND.25 INCH CRACKS AT FASTENER HOLES LONGERON 23L STATION 180 AND STATION 200. SPLICED IN SECTION OF LONGERON FROM STATION 160 TO STATION 230 PER SRM 53-02 FIG 2. (M) - [SDR USAA960340](https://openairdocs.org/sdr/USAA960340.md): Belt Frame · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Fuselage Main, Frame > PIT - DURING Q-4/C-6 INSPECTION, FOUND A.25 INCH CRACK AT FASTENER STA 180, BELT FRAME LONGERON 23L. INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-03, FIGURE 4. (X) - [SDR USAA960339](https://openairdocs.org/sdr/USAA960339.md): Longeron · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-4/C-6 INSPECTION, FOUND 1 INCH CRACK IN LONGERON 17L, AT STATION 945. SPLICED IN LONGERON SECTION PER USAIR TYPICAL REPAIR 53-10-17. (M) - [SDR USAA960338](https://openairdocs.org/sdr/USAA960338.md): Cusp Membrane · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4/C-6 INSPECTION, FOUND TWO 2 INCH CRACKS IN CUSP MEMBRANE STATION 617 RIGHT SIDE. REPLACED SECTION OF CUSP MEMBRANE FROM STATION 598 TO 637 PER SRM 53-05 FIG 97. (M) - [SDR USAA960337](https://openairdocs.org/sdr/USAA960337.md): Skin · cracked · Mar 28, 1996 · N997VJ · Doug DC931 · Horizontal Stabilizer, Plate/Skin > PIT - DURING Q-4/C-6 INSPECTION, FOUND 1.5 INCH CRACK UPPER LEADING EDGE SURFACE HORIZONTAL STABILIZER LEFT SIDE APPROXIMATELY 6 FEET OUTBOARD OF VERT STAB. INSTALLED DOUBLER REPAIR.071 2024TS ALU PER SRM 55-03 FIG 3 AND SRM 55-01 FIG 2. (M) - [SDR USAA960292](https://openairdocs.org/sdr/USAA960292.md): Skin · cracked · Mar 5, 1996 · N997VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING Q-4 INSPECTION DISCOVERED A CRACK 38.75 INCH LONG FORWARD FUSELAGE EXTERIOR SKIN FROM XPONDER ANT TO TCAS ANT STATION 247 TO 285 RUNNING ALONG LONGERON NR 1. AREA UNDER ADF CORRODED. (M) - [SDR USAA950255](https://openairdocs.org/sdr/USAA950255.md): Frame · cracked · Feb 13, 1995 · N997VJ · Doug DC931 · Fuselage Main, Frame > IND - DURING SCHEDULED CX-5 INSPECTION, FOUND.5 INCH CRACK IN FRAME AT STATION 389 AT LONGERON 17R. CUT OUT DAMAGED AREA, INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-04 FIG 35 AND USAIR EA 29574. (W) - [SDR USAA950114](https://openairdocs.org/sdr/USAA950114.md): Frame · cracked · Feb 13, 1995 · N997VJ · Doug DC931 · Fuselage Main, Frame > IND - DURING CX-5 CHECK INSPECTION ACCOMPLISHED SID INSPECTION PSE 53.09.001A, FOUND.5 INCH CRACK AT STATION 389 LONGERON 17R. (VISUAL INSPECTION). CUT OUT DAMAGED AREA, INSTALLED FILLER/DOUBLER TYPE REPAIR PER DAC SRM 53-04 FIG 35 AND USAIR EA 29574. (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 = 'N997VJ' AND deregistration_id = 'N997VJ-2005-02-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N997VJ-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.