# N912VJ: 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: 47020 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: None - Airworthiness: Standard, transport - Airworthiness date: June 2, 1988 - Certificate issued: May 2, 2002 - Last registry action: January 10, 2003 - Mode S code: AC9FFD - 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/N912VJ - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=912VJ - Page: https://openairdocs.org/deregistered/N912VJ-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 (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAAD00115](https://openairdocs.org/sdr/USAAD00115), Jul 15, 2000: LIGHT. INOPERATIVE. IND - THE SERVICE DOOR EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE BETWEEN THE LIGHT ASSEMBLY AND THE SWITCH. - [SDR USAAD00037](https://openairdocs.org/sdr/USAAD00037), Mar 1, 2000: POWER SUPPLY. FAILED. IND - THE RIGHT NACELLE SCAN LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE RIGHT NACELLE SCAN LIGHT. (M) - [SDR USAAD99071](https://openairdocs.org/sdr/USAAD99071), Jun 1, 1999: LIGHT. DISCHARGED. PHL - THE GALLEY SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE GALLEY SERVICE DOOR EMERGENCY LIGHT ASSEMBLY. (X) - [SDR USAA990352](https://openairdocs.org/sdr/USAA990352), Apr 7, 1999: FRME. CRACKED. PIT - DURING C-6 CHECK, FOUND 2 INCH CRACK IN BELLFRAME AT STATION 1074 LONGERON 14R. INSTALLED A REPAIR DOUBLER PER SRM 53-03 FIG 30. (M) - [SDR USAA990351](https://openairdocs.org/sdr/USAA990351), Apr 7, 1999: FRAME. CRACKED. PIT - DURING C-6 CHECK, FOUND TWO 1 INCH CRACKS IN BELLFRAME STATION 1076 LONGERON 14L. STOP DRILLED CRACKS AND INSTALLED A DOUBLER PER EA 51889. (M) - [SDR USAAD98128](https://openairdocs.org/sdr/USAAD98128), Jul 20, 1998: VALVE PULLEY. BLOCKED. PIT - FLT 972 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE GEAR WAS CYCLED TWICE, BUT WOULD NOT RETRACT. THE FLIGHT RETURNED TO THE FIELD AND LANDED - [SDR USAAD97123](https://openairdocs.org/sdr/USAAD97123), Jul 20, 1997: CONTROL HANDLE. JAMMED. PIT - FLT 1266 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE PRESSURIZATION - [SDR USAAD97112](https://openairdocs.org/sdr/USAAD97112), Jun 30, 1997: DOWNLOCK SWITCH. FAILED. ATL/CLT - FLT 703 - ON FINAL INTO CLT, DID NOT RECEIVE NOSE DOWN AND LOCKED INDICATION. RECYCLED GEAR, NO CHANGE. VERIFIED DOWN AND LOCKED THROUGH VIEW PORT. RE - [SDR USAA970173](https://openairdocs.org/sdr/USAA970173), Apr 24, 1997: ANGLE. GOUGED. PIT - DURING Q1 CHECK, FOUND GOUGES AT LEFT LAV STA 984 CUST ANGLE. REPAIRED PER EA 46857 SRM 53-05 FIG 25. INSTALLED ANGLE AND STRAP. (X) - [SDR USAA970172](https://openairdocs.org/sdr/USAA970172), Apr 24, 1997: BULKHEAD. CHAFED. PIT - DURING Q1 CHECK, FOUND CHAFE .50 INCH LONG BY .016 INCH DEEP AFT SIDE OF REAR PRESSURE BULKHEAD JUST FWD AND ABOVE THE 'X' FEED VALVE. INSTALLED DOUBLERS - [SDR USAA970171](https://openairdocs.org/sdr/USAA970171), Apr 24, 1997: BELT FRAME. CHAFED. PIT - DURING Q1 CHECK, FOUND DEEP CHAFE IN BELT FRAME AT STA 332 ABOVE LONGERON 30. INSTALLED SPLICE BETWEEN LONGERON 28L AND LONGERON 26R PER SRM 53-03 FIG 2A. - [SDR USAA970170](https://openairdocs.org/sdr/USAA970170), Apr 24, 1997: BULKHEAD. GOUGE. PIT - DURING Q1 CHECK, FOUND .010 INCH DEEP GOUGE ON THE AFT PRESS BULKHEAD FWD FACE BEHIND THE RIGHT THRUST REVERSER PULLEY. INSTALLED DOUBLER PER EA 46791. (X - [SDR USAA970169](https://openairdocs.org/sdr/USAA970169), Apr 24, 1997: BULKHEAD. GOUGE. PIT - DURING Q1 CHECK, FOUND .018 INCH GOUGE ON THE AFT PRESS BULKHEAD FWD FACE BEHIND THE LEFT THRUST REVERSER PULLEY SECTOR. INSTALLED DOUBLER PER EA 46791. ( - [SDR USAA970168](https://openairdocs.org/sdr/USAA970168), Apr 24, 1997: CUSP MEMBRANE. CRACKED. PIT - DURING Q1 CHECK, FOUND CRACK IN CUSP MEMBRANE RIGHT SIDE STA 945 TO STA 965. REPLACED CUSP MEMBRANE WITH MANUFACTURED ONE PER EA 46691. (X) - [SDR USAA970167](https://openairdocs.org/sdr/USAA970167), Apr 24, 1997: CUSP MEMBRANE. CRACKED. PIT - DURING Q1 CHECK, FOUND CRACK IN CUSP MEMBRANE AT RT SIDE STA 589. REPLACED MEMBRANE WITH MANUFACTURED ONE PER EA 46691. (X) - [SDR USAA970166](https://openairdocs.org/sdr/USAA970166), Apr 24, 1997: SKIN. CRACKED. PIT - DURING Q1 CHECK, FOUND CRACK IN RIVET HOLE AT STA 719 SKIN CLIP RT SIDE OF LONGERON 1R. INSTALLED DOUBLER 6.50 INCHES BY 4.50 INCHES PER SRO 9530129. (X) - [SDR USAA970165](https://openairdocs.org/sdr/USAA970165), Apr 24, 1997: LONGERON. CRACKED. PIT - DURING Q-1 CHECK, FOUND CRACK IN LONGERON 17L AT STA 945. SPLICED IN NEW SECTION OF LONGERON BETWEEN STA 929 AND STA 970 PER 543-02 FIG 2. (X) - [SDR USAA970164](https://openairdocs.org/sdr/USAA970164), Apr 24, 1997: LONGERON. CRACKED. PIT - DURING Q-1 CHECK, FOUND 2 CRACKS .25 INCH LONG AT STA 389 AND STA 408, LONGERON 17R. SPLICED IN NEW SECTION OF LONGERON BETWEEN STA 389 AND STA 415, LONGE - [SDR USAA970044](https://openairdocs.org/sdr/USAA970044), Jan 31, 1997: SKIN. CRACKED. PIT - DURING B-CHECK, FOUND 1.5 INCH CRACK IN VETICAL SKIN PANEL AT LEFT SIDE, VERTICAL STABILIZER SKIN, BENEATH DRAG ANGLE. REPAIRED DOUBLER .032 TITANIUM PER - [SDR USAA970043](https://openairdocs.org/sdr/USAA970043), Jan 31, 1997: ANGLE. CRACKED. PIT - DURING B-CHECK, FOUND .75 INCH CRACK AT LEFT VERTICAL STABILIZER DRAG, DORSAL FIN, ANGLE JUST AFT OF STATION 1076. REPAIRED FOR MFG DRWG ANGLE AND DOUBLER - [SDR USAAD97008](https://openairdocs.org/sdr/USAAD97008), Jan 11, 1997: PRESS CONTROLLER. FAILED. FLT 536 - PIT-SYR - AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO FIELD. MEL'D PRIMARY PRESS CONTROL. REPLACED NR 2 PRESS CONTROLLER 1/12/97. (M) - [SDR USAAD97002](https://openairdocs.org/sdr/USAAD97002), Jan 5, 1997: SWITCH. FAILED. FLT 1146 - ATL-PIT - LEFT ENGINE OIL QTY STARTED A STEADY DECREASE 15 MINUTES AFTER TAKEOFF. DIVERTED TO TYS. OIL PRESSURE STARTED TO OSCILLATE RAPIDLY ONE MINU - [SDR USAAD96184](https://openairdocs.org/sdr/USAAD96184), Dec 22, 1996: LATCH. WORN. FLT 1035 - CLT-SAV - ON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ON. RETURNED TO CLT. FOUND LEFT MAIN STRIKER WORN ON DOOR LATCH MECHANISM. REPLACED DOO - [SDR USAAD96112](https://openairdocs.org/sdr/USAAD96112), Aug 10, 1996: BATTERY PACK. DISCHARGED. FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (M) - [SDR USAAD96069](https://openairdocs.org/sdr/USAAD96069), May 30, 1996: BATTERY PACK. DISCHARGED. LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X) - [SDR USAAD96066](https://openairdocs.org/sdr/USAAD96066), May 30, 1996: BATTERY PACK. DISCHARGED. LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X) - [SDR USAA960260](https://openairdocs.org/sdr/USAA960260), Feb 14, 1996: ANGLE. CRACKED. PIT - DURING C-3 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LEFT DORSAL FIN DRAG ANGLE AT STATION 1126. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 5 --- 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.