# Service difficulty reports: N912VJ, cancelled Feb 7, 2005 A list on [N912VJ, cancelled Feb 7, 2005](https://openairdocs.org/deregistered/N912VJ-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 USAAD00115](https://openairdocs.org/sdr/USAAD00115.md): Light · inoperative · Jul 15, 2000 · N912VJ · Doug DC931 · Emergency Lighting > IND - THE SERVICE DOOR EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE BETWEEN THE LIGHT ASSEMBLY AND THE SWITCH. (M) - [SDR USAAD00037](https://openairdocs.org/sdr/USAAD00037.md): Power Supply · failed · Mar 1, 2000 · N912VJ · Doug DC931 · Emergency Lighting > 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.md): Light · discharged · Jun 1, 1999 · N912VJ · Doug DC931 · Emergency Lighting > 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.md): Frme · cracked · Apr 7, 1999 · N912VJ · Doug DC931 · Fuselage Main, Frame > 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.md): Frame · cracked · Apr 7, 1999 · N912VJ · Doug DC931 · Fuselage Main, Frame > 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.md): Valve Pulley · blocked · Jul 20, 1998 · N912VJ · Doug DC931 · Landing Gear Retraction/Extension System > 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 WITHOUT INCIDENT. MAINTENANCE REPOSITIONED A TEMPORARY HYDRAULIC LINE IN THE RIGHT WHEEL WELL TH - [SDR USAAD97123](https://openairdocs.org/sdr/USAAD97123.md): Control Handle · jammed · Jul 20, 1997 · N912VJ · Doug DC931 · Cabin Pressure Control System > PIT - FLT 1266 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE PRESSURIZATION CONTROL HANDLE JAMMED AND FREED IT. (X) - [SDR USAAD97112](https://openairdocs.org/sdr/USAAD97112.md): Downlock Switch · failed · Jun 30, 1997 · N912VJ · Doug DC931 · Landing Gear Position and Warning > 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. REPLACED DOWNLOCK SWITCH. (X) - [SDR USAA970173](https://openairdocs.org/sdr/USAA970173.md): Angle · gouged · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Miscellaneous Structure > 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.md): Bulkhead · chafed · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Main, Bulkhead > 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 PER EA 46859. (X) - [SDR USAA970171](https://openairdocs.org/sdr/USAA970171.md): Belt Frame · chafed · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Main, Frame > 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. (X) - [SDR USAA970170](https://openairdocs.org/sdr/USAA970170.md): Bulkhead · gouge · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Main, Bulkhead > 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.md): Bulkhead · gouge · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Main, Bulkhead > 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. (X) - [SDR USAA970168](https://openairdocs.org/sdr/USAA970168.md): Cusp Membrane · cracked · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Miscellaneous Structure > 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.md): Cusp Membrane · cracked · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Miscellaneous Structure > 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.md): Skin · cracked · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Main, Plate/Skin > 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.md): Longeron · cracked · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > 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.md): Longeron · cracked · Apr 24, 1997 · N912VJ · Doug DC931 · Fuselage Main, Longeron/Stringer > 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, LONGERON 17R PER SRM 53-02 FIG 2. (X) - [SDR USAA970044](https://openairdocs.org/sdr/USAA970044.md): Skin · cracked · Jan 31, 1997 · N912VJ · Doug DC931 · Vertical Stabilizer, Plate/Skin > 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 EA 46218. (M) - [SDR USAA970043](https://openairdocs.org/sdr/USAA970043.md): Angle · cracked · Jan 31, 1997 · N912VJ · Doug DC931 · Vertical Stabilizer > 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 DOUBLERS PE EA 46217. (M) - [SDR USAAD97008](https://openairdocs.org/sdr/USAAD97008.md): Press Controller · failed · Jan 11, 1997 · N912VJ · Doug DC931 · Cabin Pressure Controller > 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.md): Switch · failed · Jan 5, 1997 · N912VJ · Doug DC931 · Engine Oil Pressure > 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 MINUTE BEFORE LANDING, SO THE ENGINE WAS SHUT DOWN. FOUND LEFT ENGINE OIL PRESSURE SWITCH FAILED. RE - [SDR USAAD96184](https://openairdocs.org/sdr/USAAD96184.md): Latch · worn · Dec 22, 1996 · N912VJ · Doug DC931 · Landing Gear Door Retract Section > 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 DOOR LATCH ASSEMBLY. (M) - [SDR USAAD96112](https://openairdocs.org/sdr/USAAD96112.md): Battery Pack · discharged · Aug 10, 1996 · N912VJ · Doug DC931 · Emergency Lighting > FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (M) - [SDR USAAD96069](https://openairdocs.org/sdr/USAAD96069.md): Battery Pack · discharged · May 30, 1996 · N912VJ · Doug DC931 · Emergency Lighting > LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X) - [SDR USAAD96066](https://openairdocs.org/sdr/USAAD96066.md): Battery Pack · discharged · May 30, 1996 · N912VJ · Doug DC931 · Emergency Lighting > LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X) - [SDR USAA960260](https://openairdocs.org/sdr/USAA960260.md): Angle · cracked · Feb 14, 1996 · N912VJ · Doug DC931 · Vertical Stabilizer > 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 53-05 PG 506. (M) ## 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 = 'N912VJ' AND deregistration_id = 'N912VJ-2005-02-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N912VJ-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.