# N913VJ: 1967 Douglas DC-9-31, registration cancelled 2005-02-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 7, 2005 - Status when cancelled: Valid registration - Airframe: [Douglas DC-9-31](https://openairdocs.org/model/douglas-dc-9-31) (registry code 3022065) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 45846 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: None - Airworthiness: Standard, transport - Airworthiness date: June 27, 1988 - Certificate issued: May 2, 2002 - Last registry action: January 10, 2003 - Mode S code: ACA3B4 - Owner when cancelled: [Alameda Corp Trustee](https://openairdocs.org/faa-owner/ALAMEDA%20CORP%20TRUSTEE) - Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio) - Owner type: Corporation - Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N913VJ - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=913VJ - Page: https://openairdocs.org/deregistered/N913VJ-2005-02-07 From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Douglas DC-9-31: https://openairdocs.org/model/douglas-dc-9-31.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA000733](https://openairdocs.org/sdr/USAA000733), May 16, 2000: PAN. CRACKED. PIT - C-5 - PAN HAD LONG CRACK, 0.250 INCH, DOOR PAN AT CENTER AFT STOP. INSTALLED DOUBLER PER DC-9 SRM 52-15, FIG 51. (X) - [SDR USAA991458](https://openairdocs.org/sdr/USAA991458), Dec 19, 1999: SKIN. CORRODED. PIT - DURING RON, FOUND NUMEROUS AREAS AFFECTED OVER LISTED SKIN AREA CORROSION ALONG FRAMES, LONGERONS AND AT ANTENNA DOUBLERS AT STATION 230 TO STATION 579, L - [SDR USAA991457](https://openairdocs.org/sdr/USAA991457), Dec 19, 1999: SKIN. CORRODED. PIT - DURING VISUAL (RON CHECK) FOUND CORROSION ON, UNDER AND AROUND PREVIOUS REPAIR (5 INCH BY 7 INCH) ON SKIN ON DOUBLER AT STATION 579-604 LONGERON 28L TO 28 - [SDR USAA991456](https://openairdocs.org/sdr/USAA991456), Dec 19, 1999: FITTING. CRACKED. PIT - DURING SHEET METAL REPAIR OPEN UP, FOUND 4 INCH CRACK AND 1.5 INCH BY 2 INCH CORRODED AREA (INTERGRANUAR) AT LONGERON 30 AFT END FORWARD CARGO AT T-CAP. R - [SDR USAAD99123](https://openairdocs.org/sdr/USAAD99123), Sep 9, 1999: BATTERY. DISCHARGED. IND - THE FORWARD PASSENGER CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD PASSENGER CABIN OVERHEAD EMERGENCY LIGHT BATTERIE - [SDR USAAD990092](https://openairdocs.org/sdr/USAAD990092), Jul 9, 1999: LIGHT. FAILED. IND - THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LIGHT AND THE EMERGENCY LIGHT ABOVE THE TAILCONE SLIDE WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY FO - [SDR 99ZZZX2828](https://openairdocs.org/sdr/99ZZZX2828), Jul 9, 1999: BATTERY. DISCHARGED. IND - THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LIGHT AND THE EMERGENCY LIGHT ABOVE THE TAILCONE SLIDE WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY FO - [SDR USAAD99063](https://openairdocs.org/sdr/USAAD99063), May 7, 1999: BATTERY. DISCHARGED. IND - THE SERVICE DOOR SLIDE LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR SLIDE LIGHT BATTERY. (M) - [SDR USAA990190](https://openairdocs.org/sdr/USAA990190), Mar 5, 1999: SKIN. CRACKED. PIT - DURING MAINTENANCE WALK AROUND, FOUND 3 INCH CRACK AND 9 INCH VERTICAL CRACK ON FUSELAGE SKIN BETWEEN STATION 1155.335 AND STATION 1168.895 LEFT SIDE. INS - [SDR USAAD99023](https://openairdocs.org/sdr/USAAD99023), Feb 8, 1999: BATTERY. DISCHARGED. DTW - THE GALLEY DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE GALLEY DOOR SLIDE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD99028](https://openairdocs.org/sdr/USAAD99028), Feb 7, 1999: BATTERY. DISCHARGED. DTW - THE GALLEY SERVICE DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE BATTERY FOR THE GALLEY SERVICE DOOR SLIDE EMERGENCY LIGHT. (M) - [SDR USAAD98111](https://openairdocs.org/sdr/USAAD98111), Jun 20, 1998: BATTERY. DISCHARGED. IND - THE TAIL COMPARTMENT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE TAIL COMPARTMENT EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD98016](https://openairdocs.org/sdr/USAAD98016), Jan 23, 1998: CYLINDER. FAILED. CTL - FLT 369 - ON APPROACH, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WHEN THE LANDIG GEAR WAS LOWERED. THE FLT CREW RECYCLED THE GEAR BUT THE LIGHT REMAINED. THE - [SDR USAAD97212](https://openairdocs.org/sdr/USAAD97212), Nov 21, 1997: SEAL. OUT OF POSITION. BWI - FLT 1121 - AFTER TAKEOFF, CREW HEARD A LOUD BANGING SOUND AT THE R1 DOOR. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. LANDING WEIGHT WAS 101,000 L - [SDR USAAD97165](https://openairdocs.org/sdr/USAAD97165), Sep 18, 1997: POWER SUPPLY. INOPERATIVE. PHL - FOUND AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M) - [SDR USAAD97164](https://openairdocs.org/sdr/USAAD97164), Sep 18, 1997: BATTERIES. DISCHARGED. PHL - FOUND FORWARD OVERWING EMERGENCY LIGHTS WEAK. MAINTENANCE REPLACED THE BATTERIES. (M) - [SDR USAAD97098](https://openairdocs.org/sdr/USAAD97098), May 30, 1997: BATTERY PACK. FAILED. CMH - FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) - [SDR USAA970135](https://openairdocs.org/sdr/USAA970135), Apr 14, 1997: FRAME. CRACKED. PIT - DURING Q-1 CHECK, FOUND 4 INCH CRACK AT STA 718 RIGHT SIDE MAIN FRAME. REPLACED WITH MODIFIED PART NR C/C 1193213. REPLACED PER DACO DRAWING 5928626. (X) - [SDR USAA970134](https://openairdocs.org/sdr/USAA970134), Apr 14, 1997: FRAME. CRACKED. PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK AT LT SIDE STA 718 MAIN FRAME. INSTALLED MODIFIED PART NR 9919618-IN. (X) - [SDR USAA970133](https://openairdocs.org/sdr/USAA970133), Apr 14, 1997: SKIN. CORRODED. PIT - DURING Q-1 CHECK, FOUND FUSELAGE SKIN CORRODED AT ANTENNA DOUBLER 2 INCHES BY 3 INCHES, CRACKED AT 2 FASTENERS AT STA 503, LONGERON 30. REPAIRED CUT OUT D - [SDR USAA970132](https://openairdocs.org/sdr/USAA970132), Apr 14, 1997: FITTING. CRACKED. PIT - DURING Q-1 CHECK, FOUND .25 INCH CRACK AT STA 669 LT (APPROX 12 INCHES UPWARD OF LOWER KEEL T-ANGLE) AT FITTING. INSTALLED DOUBLERS AND REPAIR ANGLES PER - [SDR USAAD97068](https://openairdocs.org/sdr/USAAD97068), Apr 11, 1997: CONNECTOR. MISALIGNED. PHL/ATL - FLT 1073 LEFT OIL STRAINER CLOGGING LIGHT ILLUMINATED. RETURNED TO FIELD. REMOVED AND REPLACED OIL FILTER. FOUND PIN MIS-ALIGNED ON DIFFERENTIAL PRESS ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19950623028039I](https://openairdocs.org/incident/19950623028039I), Jun 23, 1995: Doug DC931 (N913VJ), Toledo, OH. Passenger was observed smoking in lavatory. Met by police on landing. No smoking light on, short flight. --- 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.