# Service difficulty reports: N927VJ, cancelled Aug 26, 2002

A list on [N927VJ, cancelled Aug 26, 2002](https://openairdocs.org/deregistered/N927VJ-2002-08-26.md).

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

- [SDR USAAD00179](https://openairdocs.org/sdr/USAAD00179.md): Charger · failed · Nov 21, 2000 · N927VJ · Doug DC931 · Emergency Lighting
  > PIT - THE AFT SECTION OF THE FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT FLOOR EMERGENCY LIGHTS CHARGER. (M)
- [SDR USAAD00175](https://openairdocs.org/sdr/USAAD00175.md): Charger · failed · Nov 12, 2000 · N927VJ · Doug DC931 · Emergency Lighting
  > IND - THE AFT SECTINO OF THE FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)
- [SDR USAAD00155](https://openairdocs.org/sdr/USAAD00155.md): Power Supply · failed · Sep 28, 2000 · N927VJ · Doug DC931 · Emergency Lighting
  > PHL - SEVERAL FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR TRACK EMERGENCY LIGHT BATTERY AND POWER SUPPLY. (M)
- [SDR USAAD00142](https://openairdocs.org/sdr/USAAD00142.md): Battery · discharged · Sep 6, 2000 · N927VJ · Doug DC931 · Emergency Lighting
  > IND - THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 9 THROUGH 12 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD00110](https://openairdocs.org/sdr/USAAD00110.md): Power Supply · failed · Jul 9, 2000 · N927VJ · Doug DC931 · Emergency Lighting
  > IND - THE CEILING EMERGENCY LIGHTS BETWEEN SEAT ROWS 5 AND 9 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)
- [SDR USAAD00080](https://openairdocs.org/sdr/USAAD00080.md): Battery · discharged · May 22, 2000 · N927VJ · Doug DC931 · Emergency Lighting
  > DAY - THE AFT FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LEVEL EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD00028](https://openairdocs.org/sdr/USAAD00028.md): Manifold · leaking · Feb 11, 2000 · N927VJ · Doug DC931 · Fuel Heater
  > CLT-DAY FLT 860 - AFTER TAKEOFF, THE RIGHT ENGINE FIRE INDICATION ACTIVATED. THE THROTTLE WAS REDUCED AND THE INDICATION STOPPED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE THE RIGHT ENGINE FUEL HEAT MANIFOLD. (M)
- [SDR USAA000100](https://openairdocs.org/sdr/USAA000100.md): Keel Beam · chafed · Feb 1, 2000 · N927VJ · Doug DC931 · Fuselage Main, Keel
  > PIT - STA 917 A/C CENTERLINE. BEAM CAP HAD 1 INCH BY 2 INCH CHAFE MARK. KEEL BEEM FOUND CRACKED AT BS 917. BLENDED OUT WEAR MARKS AND INSTALLED.025 INCH SS WEAR STRIP PER SRM 53-05 FIG 20 PAGE 30A. (X)
- [SDR USAA000094](https://openairdocs.org/sdr/USAA000094.md): Beam · corroded · Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - FOUND BEAM CORRODED IN 2 AREAS, 1 INCH BY 1 INCH. CORROSION LEVEL 1. CUT OUT CORRODED AREAS AND INSTALLED NESTED ANGLE. (M)
- [SDR USAA000096](https://openairdocs.org/sdr/USAA000096.md): Seat Track · corroded · Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - LEFT INBOARD SEAT TRACK STATION 237 HAS CORROSION 2 INCH BY 4 INCH. CORROSION LEVEL 1. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M)
- [SDR USAA000095](https://openairdocs.org/sdr/USAA000095.md): Floor Support · corroded · Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - STATION 160 A/C CENTERLINE RIGHT FLOOR SUPPORT HAS 2 INCH BY 36 INCH CORROSION. LEVEL 1. MANUFACTURE NEW SUPPORT AND INSTALLED. (M)
- [SDR USAA000101](https://openairdocs.org/sdr/USAA000101.md): Frame · cracked · Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Main, Frame
  > PIT - STA 109.5 CANTED BELTRAME. WEB HAD 3.50 INCH CRACK. BELT FRAME FOUND CRACKED AT BS 109.5. REPAIRED PER EA 53797. (X)
- [SDR USAA000099](https://openairdocs.org/sdr/USAA000099.md): Angle · cracked · Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - LEFT VERTICAL STABILIZER DRAG ANGLE, STA 1104. DRAG ANGLE HAD 2 CRACKS,.75 INCH AND.3750 INCH. DRAG ANGLE FOUND CRACKED ON VERTICAL STABILIZER. CUT OUT DAMAGED AREA AND INSTALLED STRAP PER SRM 53-05 FIG 23A (DASH 505 CONFIG). (X)
- [SDR USAA000098](https://openairdocs.org/sdr/USAA000098.md): Angle · cracked · Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - REMOVED AND REPLACED VERTICAL STABILIZER DRAG ANGLE, STA 1104. DRAG ANGLE HAD 2 INCH CRACK. DRAG ANGLE FOUND CRACKED ON VERTICAL STABILIZER. STOP DRILLED CRACK ENDS AND INSTALLED REPAIR PER SRM 53-05 FIG 23 AND 23A. (X)
- [SDR USAA000097](https://openairdocs.org/sdr/USAA000097.md): Bulkhead · cracked · Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Main, Bulkhead
  > PIT - RIGHT SIDE STA 965 BULKHEAD WEB LOWER END, WEB HAD 2 INCH CRACK. BULKHEAD FOUND CRACKED AT BS 965. CUT OUT DAMAGED WEB SECTION AND INSTALLED NEW PER SRM 53-03 FIG 19. (X)
- [SDR USAA000093](https://openairdocs.org/sdr/USAA000093.md): Skin · cracked · Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Main, Plate/Skin
  > PIT - LONGERON 22L BELOW AIR STAIR, SKIN HAD.25 INCH CRACK. SKIN CRACKED AT BS 180 LONGERON 22L. PERMANENT REPAIR DOUBLER INSTALLED PER SRM 9530219 AND EO 53910467. (X)
- [SDR USAAD99145](https://openairdocs.org/sdr/USAAD99145.md): Charger · failed · Oct 2, 1999 · N927VJ · Doug DC931 · Emergency Lighting
  > IND - THE AFT CABIN AND TAIL COMPARTMENT FLOOR TRACK EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT CABIN AND TAIL COMPARTMENT FLOOR TRACK EMERGENCY LIGHT BATTERY CHARGER. (M)
- [SDR USAAD99140](https://openairdocs.org/sdr/USAAD99140.md): Supply · failed · Sep 25, 1999 · N927VJ · Doug DC931 · Emergency Lighting
  > THE ENTRANCE AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE ENTRANCE AREA EMERGENCY LIGHTS POWER SUPPLY AND BATTERIES. (M)
- [SDR USAAD99138](https://openairdocs.org/sdr/USAAD99138.md): Union · loose · Sep 23, 1999 · N927VJ · Doug DC931 · Engine Pressure Ratio (EPR)
  > PHL-ATL - FLT 1243 - DURING CLIMB-OUT, THE LEFT ENGINE REQUIRED HIGHER THROTTLE SETTINGS TO MAINTAIN EQUAL EPR READINGS. THE HIGHER THE ALTITUDE THE GREATER THE THROTTLE SPREAD BETWEEN THE TWO ENGINES. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT IN
- [SDR USAAD99136](https://openairdocs.org/sdr/USAAD99136.md): Wire · chafed · Sep 19, 1999 · N927VJ · Doug DC931 · Light System Wiring
  > PHL - THE LAST FOUR SEAT ROWS AND THE ENTIRE TAIL SECTION EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPAIRED A CHAFFED WIRE AT SEAT ASSEMBLY 21 E/F. (M)
- [SDR USAAD99135](https://openairdocs.org/sdr/USAAD99135.md): Engine · failed · Sep 17, 1999 · N927VJ · Doug DC931 · Engine (Turbine/Turboprop)
  > PHL-SYR - FLT 725 - AFTER TAKEOFF, THE LEFT ENGINE DEVELOPED COMPRESSOR STALLS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. (M)
- [SDR USAA990740](https://openairdocs.org/sdr/USAA990740.md): Frame · cracked · Jul 22, 1999 · N927VJ · Doug DC931 · Fuselage Main, Frame
  > PIT - PHL MAINTENANCE FOUND 3.5 INCH CRACK AT BELT FRAME WEB STATION 1095 LEFT SIDE. INSTALLED TEMPORARY DOUBLER PER EA 52499. (M)
- [SDR USAA980427](https://openairdocs.org/sdr/USAA980427.md): Longeron · cracked · Sep 23, 1998 · N927VJ · Doug DC931 · Fuselage Main, Longeron/Stringer
  > PIT - DURING C-6 CHECK, FOUND LONGEORN CRACKED ACROSS INTERSECTION.20 INCH AT STATION 639 LONGERON 4L. INSTALLED SPLICE PER SRM 53-02 PAGES 48-53. (M)
- [SDR USAAD98082](https://openairdocs.org/sdr/USAAD98082.md): Power Supply · failed · May 6, 1998 · N927VJ · Doug DC931 · Emergency Lighting
  > CMH - THE CEILING EMERGENCY EVACUATION LIGHTS FOR THE CENTER SECTION OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERENCY LIGHT POWER SUPPLY. (X)
- [SDR USAAD98068](https://openairdocs.org/sdr/USAAD98068.md): Valve · leaking · Apr 14, 1998 · N927VJ · Doug DC931 · Nose/Tail Landing Gear Strut/Axle
  > LGA - FL 475 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RAISE AND THERE WAS AN UNSAFE NOSE GEAR INDICATION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT AND REPLACED THE SCHRADER VALVE. (X)
- [SDR USAAD97233](https://openairdocs.org/sdr/USAAD97233.md): Power Supply · failed · Dec 13, 1997 · N927VJ · Doug DC931 · Emergency Lighting
  > CMH - AFT FLOOR TRACK EMERGENCY LIGHTING IS PARTIALLY INOPERATIVE AND PARTIALLY DIM. MAINTENANCE REPAIRED THE EMEREGENCY FLOOR TRACK WIRING AND REPLACED THE POWER SUPPLY AND BATTERY PACK. (M)
- [SDR 98ZZZM110](https://openairdocs.org/sdr/98ZZZM110.md): Battery Pack · discharged · Dec 13, 1997 · N927VJ · Doug DC931 · Emergency Lighting
  > CMH - AFT FLOOR TRACK EMERGENCY LIGHTING IS PARTIALLY INOPERATIVE AND PARTIALLY DIM. MAINTENANCE REPAIRED THE EMEREGENCY FLOOR TRACK WIRING AND REPLACED THE POWER SUPPLY AND BATTERY PACK. (M)
- [SDR USAAD97099](https://openairdocs.org/sdr/USAAD97099.md): Power Supply · failed · May 14, 1997 · N927VJ · Doug DC931 · Emergency Lighting
  > CMH - FOUND TAILCONE AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. (M)
- [SDR USAAD96143](https://openairdocs.org/sdr/USAAD96143.md): Power Supply · failed · Oct 5, 1996 · N927VJ · Doug DC931 · Emergency Lighting
  > RIGHT SIDE NACELLE EMERGENCY LIGHT INOP. MAINTENANCE REPLACED POWER PACK. (M)
- [SDR USAAD96054](https://openairdocs.org/sdr/USAAD96054.md): Rmi · failed · May 12, 1996 · N927VJ · Doug DC931 · Visual Omnirange (VOR) System
  > PIT - FL 1036 - UPON REACHING FL 180 OUT OF PIT, CREW NOTED BOTH RIM'S SPINNING AND COULD NOT FIX THE AIRCRAFT POSITION. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT RMI. (M)
- [SDR USAAD96025](https://openairdocs.org/sdr/USAAD96025.md): Slide · failed · Feb 25, 1996 · N927VJ · Doug DC931 · Escape Slide
  > FLT NR 517 - PHL - GALLEY EMERGENCY CHUTE PRESSURE IS 2500 PSI IN RED ZONE. REPLACED GALLEY EMERGENCY CHUTE. (M)
- [SDR USAA950105](https://openairdocs.org/sdr/USAA950105.md): Uplatch Roller · loose · Feb 3, 1995 · N927VJ · Doug DC931 · Landing Gear Retraction/Extension System
  > CAE - FLT 0253 - ON LANDING IN CAE, THE GEAR DOOR OPEN LIGHT WOULD NOT GO OUT. THE GEAR WAS RECYCLED THREE TIMES BUT THE LIGHT REMAINED ON. MAINTENANCE SECURED A LOOSE ROLLER ON THE RIGHT MAIN LANDING GEAR UPLATCH. CHECKED OTHER PORTIONS OF THE DOOR INDICAT

## 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 = 'N927VJ' AND deregistration_id = 'N927VJ-2002-08-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N927VJ-2002-08-26/reports

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