# Service difficulty reports: N922VJ, cancelled Dec 13, 2002

A list on [N922VJ, cancelled Dec 13, 2002](https://openairdocs.org/deregistered/N922VJ-2002-12-13.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR USAAD01114](https://openairdocs.org/sdr/USAAD01114.md): Downlock Sensor · corroded · May 21, 2001 · N922VJ · Doug DC931 · Landing Gear Position and Warning
  > PIT-CRW - FLT 1282 - DURING DESCENT, WHEN THE LANDING GEAR WAS EXTENDED THE RIGHT MAIN LANDING GEAR GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. THE LANDING GEAR WAS VERIFIED DOWN BY THE CONTROL TOWER. THE LANDING GEAR WAS CYCLED AND THE GREEN LIGHT ILLUM
- [SDR USAAD01026](https://openairdocs.org/sdr/USAAD01026.md): Piston · failed · Feb 9, 2001 · N922VJ · Doug DC931 · Nose/Tail Landing Gear
  > STL-PIT - FLT 742 - AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED THE NOSE GEAR UNSAFE LIGHT STAYED ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR PISTON AXLE ASSEMBLY. (M)
- [SDR USAAD01024](https://openairdocs.org/sdr/USAAD01024.md): Harness · shorted · Feb 8, 2001 · N922VJ · Doug DC931 · Landing Gear Position and Warning
  > AVP-PHL - FLT 1819 - AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON. THE FLIGHT CREW ACCOMPLISHED QRH PROCEDURES AND RECYCLED THE GEAR. THE FLIGHT LANDED AT PHL WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MLG PROXIMITY HARNESS. THE
- [SDR USAAD01006](https://openairdocs.org/sdr/USAAD01006.md): Power Supply · discharged · Jan 6, 2001 · N922VJ · Doug DC931 · Emergency Lighting
  > DAY - THE OVERHEAD EMERGENCY LIGHTS IN THE FIRST CLASS PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)
- [SDR USAAD00046](https://openairdocs.org/sdr/USAAD00046.md): Unknown · odor · Apr 3, 2000 · N922VJ · Doug DC931 · Air Distribution System
  > ORF-PIT - FLT 841 - ON TAKEOFF, THERE WAS A BURNING SMELL IN THE PASSENGER CABIN AND THE COCKPIT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. (M)
- [SDR USAAD00018](https://openairdocs.org/sdr/USAAD00018.md): Battery · discharged · Jan 19, 2000 · N922VJ · Doug DC931 · Emergency Lighting
  > IND - THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS DIM AND THE MAIN ENTRANCE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE SERVICE AND MAIN ENTRANCE DOORS. (M)
- [SDR USAAD99109](https://openairdocs.org/sdr/USAAD99109.md): Battery · discharged · Aug 6, 1999 · N922VJ · Doug DC931 · Emergency Lighting
  > THE CEILING EMERGENCY LIGHTS FOR ROWS 10-13 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE ROW 10-13 CEILING EMERGENCY LIGHTS. (M)
- [SDR USAA990333](https://openairdocs.org/sdr/USAA990333.md): Cusp · cracked · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 2 INCH CRACK AT STATION 965 LT CUSP MEMBRANE. ROUTED OUT CRACK AND INSTALLED DOUBLER PER EA (PENDING) 51752. (M)
- [SDR USAA990332](https://openairdocs.org/sdr/USAA990332.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 6 INCH CORROSION AT FLOOR SUPPORT AT STATION 200 INBOARD OF SERVICE DOOR. CORROSION LEVEL 1, CORROSION TASK NC C46-53303. FLOOR SUPPORT CUT FROM STOCK EXTRUSION 70 75-T6. (M)
- [SDR USAA990331](https://openairdocs.org/sdr/USAA990331.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 30 INCH CORROSION AT FLOOR SUPPORT AT STATION 160-200 JUST AFT EPC PANEL. CORROSION LEVEL 1, CORROSION TASK NR C46053303. REPLACED WITH ANGLE IN STOCK. (M)
- [SDR USAA990329](https://openairdocs.org/sdr/USAA990329.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 10 INCH CORROSION AT FLOOR SUPPORT AT STATION 218 TO 236 INBOARD OF LT OUTBOARD SEAT TRACK. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REPLACED WITH ANGLE IN STOCK. (M)
- [SDR USAA990328](https://openairdocs.org/sdr/USAA990328.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND.5 INCH BY 4 INCH CORROSION AT FLOOR SUPPORT AT STATION 160 CENTER LINE TO FORWARD SERVIEC DOOR. CORROSION LEVEL 1, CORROSION TASK NRC46-53303. CLEANED CORROSION, ALODINED, PRIMED, MFG FLOOR SUPPORT NR 36 AND INSTALLED SUPPORT.
- [SDR USAA990327](https://openairdocs.org/sdr/USAA990327.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 18 INCH CORROSION AT FLOOR SUPPORT AT STATION 200 RIGHT SIDE CENTER LINE. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. CLEANED CORROSION, ALODINED, PRIMED, MFG NR 25 SUPPORT AND INSTALLED SUPPORT. (M)
- [SDR USAA990326](https://openairdocs.org/sdr/USAA990326.md): Seat Track · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 2 INCH CORROSION AT SEAT TRACK AT STATION 200 RIGHT INBOARD. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REMOVED AND SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M)
- [SDR USAA990325](https://openairdocs.org/sdr/USAA990325.md): Seat Track · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - DURING Q-1 CHECK, FOUND 3 INCH SECTION CORROSION WITH 1 INCH CRACK, LEVEL 1 SUSPECT LEVEL 2 AT RIGHT SIDE INBOARD TRACK STATION 270. CORROSION LEVEL 1. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M)
- [SDR USAA990324](https://openairdocs.org/sdr/USAA990324.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 15 INCH CORROSION ON FLOOR SUPPORT AT STATION 160 TO 200 FORWARD OF RIGHT OUTBOARD SEAT TRACK. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-1 PAGE 53. (M)
- [SDR USAA990323](https://openairdocs.org/sdr/USAA990323.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND.5 INCH BY 30 INCH CORROSION ON FLOOR SUPPORT AT STATION 160 TO 200 INBOARD OF MED. CORROSION LEVEL 1, CORROSION TASK NR C646-53303. DEFECTIVE PART REPLACED WTH IDENTICAL PART PER SRM 53-11-1 PAGE 53. (M)
- [SDR USAA990322](https://openairdocs.org/sdr/USAA990322.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 18 INCH CORROSION ON FLOOR SUPPORT AT STATION 200 LEFT SIDE CENTER LINE. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. DEFECTIVE PART REPLACED WITH IDENTICAL PART MANUFACTURED FROM STOCK EXTRUSION 171-9673. (M)
- [SDR USAA990321](https://openairdocs.org/sdr/USAA990321.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 8 INCH CORROSION ON GALLEY FLOORBEAM BETWEEN BEAMS NR 26 AND NR 36. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REMOVED AND REPLACED PART WITH IDENTICAL PART NUMBER PER SRM 53-11-1 PAGE 53. (M)
- [SDR USAA990320](https://openairdocs.org/sdr/USAA990320.md): Support · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 30 INCH CORROSION ON FLOOR SUPPORT AT STATION 160 TO 218 CENTER LINE. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REMOVED AND REPLACED FLOOR SUPPORT. (M)
- [SDR USAA990319](https://openairdocs.org/sdr/USAA990319.md): Beam · corroded · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND FORWARD CARGO DOOR FRAME CORRODED (2 INCH BY 3 INCH AREA) ON DOOR FRAME BETWEEN STATION 370-427. SPLICED IN NEW SECTION OF DOOR FRAME PER SRM 53-05 FIG 44. (M)
- [SDR USAA990273](https://openairdocs.org/sdr/USAA990273.md): Skin · cracked · Mar 30, 1999 · N922VJ · Doug DC931 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-1 CHECK, FOUND.25 INCH CRACK EMINATING FROM SHEAR TIE ATTACH FASTENER ON FUSELAGE SKIN AT STRINGER 14L STATION 965. INSTALLED PERMANENT CLASS 1 REPAIR PER DC-9 SRM 53-04 FIG 12B. (M)
- [SDR USAA990272](https://openairdocs.org/sdr/USAA990272.md): Skin · cracked · Mar 27, 1999 · N922VJ · Doug DC931 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-1 CHECK, FOUND TWO.25 INCH CRACKS AND TWO EACH 1.5 INCH CRACKS ON SKIN BETWEEN STATION 945 AND 965 AND BETWEEN L14R AND L15R. CUT OUT TWO CRACKS AND FILLED. STOP DRILLED TWO CRACKS AND INSTALLED TITANIUM DOUBLER PER EA 51658. (M)
- [SDR USAA990271](https://openairdocs.org/sdr/USAA990271.md): Longeron · cracked · Mar 27, 1999 · N922VJ · Doug DC931 · Fuselage Main, Longeron/Stringer
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH LONG CRACK AT LONGERON 4L STATION 160 (AROUND HI-LOCK HEAD). SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 18. (M)
- [SDR USAA990270](https://openairdocs.org/sdr/USAA990270.md): Angle · cracked · Mar 27, 1999 · N922VJ · Doug DC931 · Nacelle/Pylon Structure
  > PIT - DURING Q-1 CHECK, FOUND.375 INCH CRACK IN UPPER RIGHT PYLON ATTACH ANGLE AT VERT LEG OF ATTACH ANGLE AT STATION 1019 RIGHT. INSTALLED DOUBLER PER SRM 54-04 FIG 10. (M)
- [SDR USAA990269](https://openairdocs.org/sdr/USAA990269.md): Fitting · corroded · Mar 27, 1999 · N922VJ · Doug DC931 · Cargo/Baggage Doors
  > PIT - DURING Q-1 CHECK, FOUND CORROSION AT INERCOSTAL 'T' FITTINGS (1 INCH BY.5 INCH AREA) AT FORWARD CARGO DOOR LOWER AFT DOOR STOP, BOTH SIDES OF WEB. CORROSION TASK NR C51-53300, CORROSION LEVEL 1. CLEANED AND TREATED PER SRM 51-10-3. (M)
- [SDR USAA990268](https://openairdocs.org/sdr/USAA990268.md): Fitting · corroded · Mar 27, 1999 · N922VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND CORROSION AT INTERCOSTAL 'T' FITTINGS (1 INCH BY.5 INCH AREA) AT LOWER FORWARD CARGO DOOR STOP, BOTH SIDES OF WEB. CORROSION TASK NR C51-53300, CORROSION LEVEL 1. CLEANED AND TREATED PER SRM 51-10-3. (M)
- [SDR USAA990267](https://openairdocs.org/sdr/USAA990267.md): Skin · cracked · Mar 27, 1999 · N922VJ · Doug DC931 · Emergency Exits
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN SKIN COMING OUT FROM UNDER TOP AFT STOP AT AFT LEFT EMERGENCY EXIT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-20-03. (M)
- [SDR USAAD98190](https://openairdocs.org/sdr/USAAD98190.md): Unknown · odor · Oct 23, 1998 · N922VJ · Doug DC931 · Air Distribution System
  > GSO - FLT 990 - AFTER TAKEOFF, PASSENGERS NOTED A BURNING SMELL IN THE CABIN. FLIGHT RETURNED TO GSO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED FULL POWER RUN-UPS ON BOTH ENGINES AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS RELEASED
- [SDR USAAD98173](https://openairdocs.org/sdr/USAAD98173.md): Battery · discharged · Sep 29, 1998 · N922VJ · Doug DC931 · Emergency Lighting
  > DTW - THE AFT OVERHEAD EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD97023](https://openairdocs.org/sdr/USAAD97023.md): Battery Pack · failed · Jan 21, 1997 · N922VJ · Doug DC931 · Emergency Lighting
  > DAY - LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE BATTERY PACK. (M)
- [SDR USAAD96017A](https://openairdocs.org/sdr/USAAD96017A.md): Windshield · cracked · Feb 2, 1996 · N922VJ · Doug DC931 · Flight Compartment Windows
  > ORD FLI 979 - FIRST OFFICERS WINDSHIELD CRACKED. FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDOW HEAT CONTROLLER, P/N 9615059002, AND THE WINDOW. (M)
- [SDR USAAD96017](https://openairdocs.org/sdr/USAAD96017.md): Windshield · cracked · Feb 2, 1996 · N922VJ · Doug DC931 · Flight Compartment Windows
  > ORD - FL 979 - FIRST OFFICERS WINDSHIELD CRACKED. FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. (M)
- [SDR USAA951363](https://openairdocs.org/sdr/USAA951363.md): Skin · cracked · Dec 26, 1995 · N922VJ · Doug DC931 · Nacelle/Pylon, Plate/Skin
  > PIT - WHILE ACCOMPLISHING X-RAY INSPECTION OF PYLON AREA IN BOS, MAINTENANCE DISCOVERED A.25 INCH CRACK IN SKIN AT STA 965, LONGERON 14L. AIRCRAFT WAS MAINTENANCE FERRIED TO PIT FOR REPAIR. INTERIM EXTERNAL DOUBLER REPAIR INSTALLED PER USAIR EA NR 31838. A
- [SDR USAA950373](https://openairdocs.org/sdr/USAA950373.md): Windshield · lost sealant · Apr 14, 1995 · N922VJ · Doug DC931 · Flight Compartment Windows
  > CLT - THE CAPTAINS WINDSHIELD LOST TAPING AND SEALER AT 12,000 FEET. THE SEALANT OBSTRUCTED THE VIEW OF THE WINDSHIELD. FLIGHT RETURNED TO CLT. MAINTENANCE RESEALED THE CAPTAINS WINDSHIELD. (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 = 'N922VJ' AND deregistration_id = 'N922VJ-2002-12-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N922VJ-2002-12-13/reports

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