# Service difficulty reports: N926VJ, cancelled Oct 31, 2006 A list on [N926VJ, cancelled Oct 31, 2006](https://openairdocs.org/deregistered/N926VJ-2006-10-31.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAD01151](https://openairdocs.org/sdr/USAAD01151.md): Battery · inoperative · Aug 17, 2001 · N926VJ · Doug DC931 · Emergency Lighting > PIT - THE LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERATIONALLY CHECKED OK. (M) - [SDR USAA010406](https://openairdocs.org/sdr/USAA010406.md): Skin · cracked · Mar 16, 2001 · N926VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CRACKED 1 INCH, STATION 1095 LONGERON 4 RIGHT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 27. (M) - [SDR USAA010204](https://openairdocs.org/sdr/USAA010204.md): Skin · cracked · Feb 25, 2001 · N926VJ · Doug DC931 · Wing, Plate/Skin > PIT - FOUND SKIN CRACKED 2.5 INCHES, LEADING EDGE LT WING BOTTOM SIDE STATION XFS 126.438. CUT OUT DAMAGE, INSTALLED FLUSH REPAIR WITH INNER DOUBLER PER SRM 57-06A FIG 3. (M) - [SDR USAAD00145](https://openairdocs.org/sdr/USAAD00145.md): Strut · discharged · Sep 16, 2000 · N926VJ · Doug DC931 · Nose/Tail Landing Gear Strut/Axle > MSP-PIT - FLT 2247 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE GEAR STRUT WITH OIL AND NITROGEN AND COMPLETED A NOSE GEAR SWING. (M) - [SDR USAAD99178](https://openairdocs.org/sdr/USAAD99178.md): Engine · birdstrike · Dec 16, 1999 · N926VJ · Doug DC931 · Engine (Turbine/Turboprop) > IND-DCA - FLT 769 - AFTER TAKEOFF THE RIGHT ENGINE HAD A COMPRESSOR STALL THAT LASTED FOR ABOUT 3 SECONDS.. THIS WAS ACCOMPLISHED BY AN UNUSUAL ODOR IN THE CABIN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND EVIDENCE OF - [SDR USAAD99139](https://openairdocs.org/sdr/USAAD99139.md): Link · failed · Sep 23, 1999 · N926VJ · Doug DC931 · Landing Gear Door Retract Section > CLT-PIT - FLT 1230 - AFTER TAKEOF AND THE LANDING GEAR WAS RETRACTED, THERE WAS A NOISE IN THE NOSE GEAR WELL. A VIBRATION THEN OCCURRED. WHEN THE LANDING GEAR WAS LOWERED TO RETURN TO THE FIELD THE VIBRATION CEASED. THERE WERE NO ABNORMAL INDICATIONS. THE - [SDR USAAD99080](https://openairdocs.org/sdr/USAAD99080.md): Battery Pack · discharged · Jun 13, 1999 · N926VJ · Doug DC931 · Emergency Lighting > IND - THE TAILCONE OVERHEAD EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERIES. (M) - [SDR USAA990348](https://openairdocs.org/sdr/USAA990348.md): Support · corroded · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 6 INCH LONG CORROSION AT GALLEY FLOOR SUPPORT NR 2 CORROSION LEVEL 1. REPLACED FLOOR SUPPORT. (M) - [SDR USAA990347](https://openairdocs.org/sdr/USAA990347.md): Support · corroded · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 22 INCH LONG CORROSION AT CENTER FLOOR SUPPORT BETWEEN STATIONS 230 AND 252. CORROSION LEVEL 1. FABRICATED PART PER TYPICAL REPAIR 53-10-21A. (M) - [SDR USAA990346](https://openairdocs.org/sdr/USAA990346.md): Bracket · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK AT RIGHT LAV 965 INBOARD BEAM TRIM ATTACH BRACKET. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 4. (M) - [SDR USAA990345](https://openairdocs.org/sdr/USAA990345.md): Web · chafed · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND.25 INCH HOLE AND CHAFE MARK VENTRAL AREA FORWARD SIDE STATION 1038 WEB AT LT TEMP CONT VLV. INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M) - [SDR USAA990344](https://openairdocs.org/sdr/USAA990344.md): Angle · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND.25 INCH CRACK IN ANGLE RIGHT PYLON AT FORWARD WALL OF CANNON PLUG BAY. FABRICATED NEW ANGLE OUT OF 2024 T3.025. (M) - [SDR USAA990343](https://openairdocs.org/sdr/USAA990343.md): Web · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND TWO CRACKS.25 INCH AND.75 INCH AT RIGHT PYLON CANTED WEB IN CANNON PLUG BAY. INSTALLED DOUBLER PER SRM 54-01 FIG 2 SHEET 2. (M) - [SDR USAA990342](https://openairdocs.org/sdr/USAA990342.md): Bracket · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND.50 INCH CRACK IN MIDDLE LEFT DOOR BRACKET ON INSIDE DOOR JAMB. DEFECTIVE PART REPLACED WITH PART NR 3917624515. (M) - [SDR USAA990341](https://openairdocs.org/sdr/USAA990341.md): Bracet · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND.5 INCH CRACK AT UPPER RIGHT DOOR STOP BRACKET ON DOOR JAMB. REPLACED WITH NEW BRACKET. (M) - [SDR USAA990340](https://openairdocs.org/sdr/USAA990340.md): Ceiling · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK AND 1 INCH CRACK AT CABIN FLOOR CEILING AT STATION 154 AND 158 ABOVE RIGHT OUTBOARD PULLEY CABLE AROUND 2 CREWS. REMOVED AND REPLACED DEFECTIVE PART. (M) - [SDR USAA990339](https://openairdocs.org/sdr/USAA990339.md): Bulkhead · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Main, Bulkhead > PIT - DURING Q-4 CHECK, FOUND.5 INCH CRACKS (SEVERAL) AT FORWARD SIDE STATION 965 BULKHEAD FORWARD WALL OF LAV AT FLOOR LEVEL. REPAIRED PER SRM 53-03 FIG 19. (M) - [SDR USAA990338](https://openairdocs.org/sdr/USAA990338.md): Cusp · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 3 INCH LONG CRACK AT RIGHT SIDE CUSP AT STRINGER NR 18 STATION 617. REMOVED AND REPLACED DEFECTIVE PART. (M) - [SDR USAA990337](https://openairdocs.org/sdr/USAA990337.md): Window Frame · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND.25 INCH CRACK IN WINDOW FRAME AT UPPER FORWARD CORNER OF WINDOW FRAME AT STATION 598 RIGHT. STOP DRILLED, DOUBLER INSTALLED PER TYPICAL REPAIR 533006A. (M) - [SDR USAA990336](https://openairdocs.org/sdr/USAA990336.md): Support · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 2 INCH CRACKS IN FLOOR SUPPORT AT STATION 965 AT 29R. STOP DRILLED PER TYPICAL REPAIR 53-2-08 PAGE 1. (M) - [SDR USAA990335](https://openairdocs.org/sdr/USAA990335.md): Bulkhead Web · cracked · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Main, Bulkhead > PIT - DURING Q-4 CHECK, FOUND TWO CRACKS IN SKIN AT BULKHEAD WEB STATION 965 AT RIGHT FLOOR LINE. REPLACED DAMAGED AREA WITH NEW SPLICED WEB PER SRM 53-03 FIG 119. (M) - [SDR USAA990334](https://openairdocs.org/sdr/USAA990334.md): Ceiling · cracks · Mar 30, 1999 · N926VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 2 CRACKS 1 INCH LONG ON CABIN FLOOR CEILING STATION 154 AND 158 OUTBOARD SIDE RIGHT. INSTALLED DOUBLER PER SRM 53-01 PAGE 9. (M) - [SDR USAAD98134](https://openairdocs.org/sdr/USAAD98134.md): Water Separator · contaminated · Aug 5, 1998 · N926VJ · Doug DC931 · Humidity Control System > IND - FLT 1242 - AFTER TAKEOFF A STRONG FUEL SMELL WAS EVIDENT IN BOTH THE CABIN AND COCKPIT. THE FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN BOTH ENGINES AND THE APU, NO OIL OR FUEL LEAKS WERE NOTED. THE TAIL COM - [SDR USAAD98053](https://openairdocs.org/sdr/USAAD98053.md): Battery · discharged · Mar 29, 1998 · N926VJ · Doug DC931 · Emergency Lighting > IND - THE CABIN CEILING EMERGENCY LIGHTS FOR ROWS 10-14 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD98020](https://openairdocs.org/sdr/USAAD98020.md): Strut · leaking · Jan 29, 1998 · N926VJ · Doug DC931 · Nose/Tail Landing Gear Strut/Axle > PIT - FLT 1712 - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CREW RECYCLED GEAR TO NO AVAIL. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR PISTON ASSEMBLY AND PERFORMED A GEAR SWING. ALL CHECKED NORM - [SDR USAAD98017](https://openairdocs.org/sdr/USAAD98017.md): Valve · leaking · Jan 23, 1998 · N926VJ · Doug DC931 · Nose/Tail Landing Gear Strut/Axle > CLT - FLT 7002 - AFTER TAKEOFF, THE NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR STRUT FLAT. THE SERVICING (SCHRADER) VALVE WAS REPLACED AND THE - [SDR USAAD97238](https://openairdocs.org/sdr/USAAD97238.md): Pressure Select · failed · Dec 23, 1997 · N926VJ · Doug DC931 · Cabin Pressure Control System > CLT - FLT 1287 - PASSING THROUGH 12,500 FEET ON CLIMB-OUT FROM CLT, CREW LOST AUTO PRESSURIZATION CONTROL. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CONTROL PANEL (PRESSURE SELECTOR). (M) - [SDR USAAD97142](https://openairdocs.org/sdr/USAAD97142.md): Fuel Press · failed · Aug 21, 1997 · N926VJ · Doug DC931 · Landing Gear Door Actuator > PIT - FL 1036 - LEFT ENGINE FULE FILTER PRESSURE DROP LIGHT CAME ON IN FLIGHT. CREW PERFORMED ABNORMAL PROCEDURES AND RETURN TO FIELD. PIT - A/C LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT ENGINE FUEL FILTER (OLD FILTER CLEAN) ANF REPLACED LEFT ENGINE FU - [SDR USAAD97105](https://openairdocs.org/sdr/USAAD97105.md): Battery Pack · discharged · Jun 21, 1997 · N926VJ · Doug DC931 · Emergency Lighting > DAY/RON - FOUND LEFT NACELLE LIGHT INOPERATIVE IN EMERGENCY MODE. REPLACED BATTERY PACK. (X) - [SDR USAAD96062](https://openairdocs.org/sdr/USAAD96062.md): Trim Motor · failed · May 24, 1996 · N926VJ · Doug DC931 · Stabilizer Actuator > PIT/EWR - FLT 936 - PRIMARY TRIM DOES NOT TRIM FORWARD. RETURNED TO FIELD. REPLACED PRIMARY TRIM MOTOR AND TRIM BRAKE RELAYS. (X) - [SDR USAAD96057](https://openairdocs.org/sdr/USAAD96057.md): Engine · failed · May 19, 1996 · N926VJ · Doug DC931 · Engine (Turbine/Turboprop) > FLIGHT NR 8001 - CLT-GSP - RIGHT ENGINE OIL TEMP DURING CRUISE WENT TO 130 DEGREES. WENT TO 155 DEGREES AT IDLE. SHUT DOWN ENGINE. REPLACED ENGINE. (M) - [SDR USAA950235](https://openairdocs.org/sdr/USAA950235.md): Link · damaged · Mar 10, 1995 · N926VJ · Doug DC931 · Landing Gear Door Retract Section > PIT - FLT 0590 - UPON GEAR RETRACTION, CREW HEARD A LOUD BANG FROM THE NOSE GEAR. THE RED UNSAFE LIGHT ILLUMINATED. THE GEAR WAS PUT DOWN, BUT THE LIGHT REMAINED. FLIGHT RETURNED TO PIT WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT NOSE GEAR FORWARD LINK ## 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 = 'N926VJ' AND deregistration_id = 'N926VJ-2006-10-31' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N926VJ-2006-10-31/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, except the copies of manufacturers’ service documents, which belong to their rights holders.