# Service difficulty reports: N919VJ, cancelled Jan 30, 2003

A list on [N919VJ, cancelled Jan 30, 2003](https://openairdocs.org/deregistered/N919VJ-2003-01-30.md).

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

- [SDR USAAD01041](https://openairdocs.org/sdr/USAAD01041.md): Battery · discharged · Feb 28, 2001 · N919VJ · Doug DC931 · Emergency Lighting
  > PIT - FOUND THE COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD00061](https://openairdocs.org/sdr/USAAD00061.md): Battery · discharged · Apr 24, 2000 · N919VJ · Doug DC931 · Emergency Lighting
  > IND - THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)
- [SDR USAA991012](https://openairdocs.org/sdr/USAA991012.md): Skin · cracked · Aug 24, 1999 · N919VJ · Doug DC931 · Fuselage Main, Plate/Skin
  > PIT - DURING RON FOUND 3 CRACKS 2.5 INCH BY 1 INCH LONG AT STATION 58.750 LT, LONGERON 18/19. INSTALLED DOUBLER AND FILLER PER SRM 53-01 FIG 2 SHEET 3, PAGE 9. (M)
- [SDR USAA990222](https://openairdocs.org/sdr/USAA990222.md): Support · corroded · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND RIGHT LAV CENTER FLOOR SUPPORT CORRODED AND CRACKED.75 INCH AT STATION 965. CORROSION LEVEL 1, CORROSION TASK NR C58-5330. CLEANED CORROSION, TREATED AND PRIMED PER SRM. MANUFACTURED NEW FLOOR SUPPORT TAB FROM 7075-T6.040 PER
- [SDR USAA990201](https://openairdocs.org/sdr/USAA990201.md): Jamb · damaged · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND SMALL HOLE IN AFT CARGO DOOR JAMB WEB JUST ABOVE 29 RIGHT. REMOVED DAMAGED SECTION OF WEB, MANUFACTURED NEW WEB PIECE FROM C/C 109-5712. MADE SPLICES FROM 7075-T6.050 INCH AND INSTALLED PER EA NR 51599. (M)
- [SDR USAA990200](https://openairdocs.org/sdr/USAA990200.md): Frame · cracked · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Main, Frame
  > PIT - DURING Q-1 CHECK, FOUND.5 INCH LENGTH BY.21875 INCH WIDE BY.019 INCH DEEP CHAFE IN FRAME NR 1059 LONGERON 15L. INSTALLED DOUBLER PER SRM 53-01, FIG 2 SHEET 4 AND EA 51616. (M)
- [SDR USAA990199](https://openairdocs.org/sdr/USAA990199.md): Cusp · cracked · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN CUSP MEMBRANE LEFT BETWEEN STATION NR 935 AND 945. FABRICATED CUSP MEMBRANE AND INSTALLED PER EA 51628. (M)
- [SDR USAA990198](https://openairdocs.org/sdr/USAA990198.md): Bracket · cracked · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK ON TAIL INTERIOR ON VERTICAL ATTACH BRACKET FOR 'Y' DUT STATION 1087 BELOW 5R. REPLACED DEFECTIVE PART WITH IDENTICAL PART NUMBER. (M)
- [SDR USAA990197](https://openairdocs.org/sdr/USAA990197.md): Frame · chafed · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Main, Frame
  > PIT - DURING Q-1 CHECK, FOUND CHAF.372 INCH BY.196 INCH WIDE BY.029 INCH DEEP AT FRAME 1019 BELOW LONGERON 13R. CUT OUT DAMAGE AREA OF FRAME AND SPLICED IN A NEW SECTION OF FRAME AND SPLICED IN A NEW SECTION OF FRAME PER SRM 53-03 FIG 4. (M0
- [SDR USAA990196](https://openairdocs.org/sdr/USAA990196.md): Cusp · cracked · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND CRACKS 1.75 AND 3.5 INCH LEFT SIDE OF CABIN STATION 598 CUSP MEMBRANE. CUT OUT AND INSTALLED NEW SECTION PER EA 51628. (M)
- [SDR USAA990195](https://openairdocs.org/sdr/USAA990195.md): Intercostal · cracked · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FUOND 1.25 INCH CRACK IN INTERCOSTAL BETWEEN CABIN FLOORBEAMS NR 965-980, C/L OF A/C UPPER FLANGE. INSTALLED DOUBLER MANUFACTURED FROM 7075T6.032 INCH PER SRM 53-01, FIG 2. (M)
- [SDR USAA990194](https://openairdocs.org/sdr/USAA990194.md): Strap · corroded · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND CORROSION ON CARGO TIE DOWN STRAP.75 INCH DIAMETER BY.008 DEEP AT LEFT SIDE BETWEEN STATION 897-925 ON STRAP. CORROSION LEVEL 1, CORROSION TASK NR C57-53300. SPLICED IN NEW PART MANUFACTURED SPLICE ANGLES AND INSTALLED PER DRA
- [SDR USAA990193](https://openairdocs.org/sdr/USAA990193.md): Support · corroded · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FOUND 41.5 INCH LONG, LEVEL 1 CORROSION AT ENTRANCE FLOOR SUPPORT 39 EXTRUSION, LIGHT CORROSION FULL LENGTH. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REPLACED SUPPORT WITH MODIFIED PART NR 992348429. (M)
- [SDR USAA990192](https://openairdocs.org/sdr/USAA990192.md): Support · corroded · Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-1 CHECK, FUOND 4.5 INCH LONG, LEVEL 1 CORROSION AT ENTRANCE FLOOR SUPPORT 23 EXTRUSION, LIGHT CORROSION FULL LENGTH. CORROSION LEVEL 1, CORROSION TASK NR C46-533013. REPLACED SUPPORT WITH MODIFIED PART NR S265247912000. (M)
- [SDR USAAD98127](https://openairdocs.org/sdr/USAAD98127.md): Battery · discharged · Jul 20, 1998 · N919VJ · Doug DC931 · Emergency Lighting
  > PIT - THE FLOOR LEVEL EMERGENCY LIGHTS ROW 16 THROUGH ROW 21 AND THE CEILING EMERGENCY LIGHTS ROW 9 THROUGH ROW 12 WERE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN BUTT SPLICE FOR THE FLOOR LEVEL EMERGENCY LIGHTS AND REPLACED FLOOR LEVEL AND CEILING EMERGENCY
- [SDR USAAD98056](https://openairdocs.org/sdr/USAAD98056.md): Slide · inoperative · Mar 9, 1998 · N919VJ · Doug DC931 · Escape Slide
  > PIT - AFT ESCAPE SLIDE FAILED TO DEPLOY DURING OPERATIONAL TEST. MAINTENANCE REPLACED THE SLDIE ASSEMBLY. TWO ADDITIONAL OPERATIONAL TESTS WERE SCHEDULED. (M)
- [SDR USAAD97230](https://openairdocs.org/sdr/USAAD97230.md): Apu · smoking · Dec 4, 1997 · N919VJ · Doug DC931 · APU Core Engine
  > CMH - FL 818 - AFTER T/O THE CREW NOTICED THE SMELL OF BURNED OIL IN THE COCKPIT. THE FLT ATTENDANTS NOTICED SMOKE IN THE CABIN AND BOTH LAVATORY SMOKE DETECTORS WENT OFF. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MX INSPECTED BOTH LEF
- [SDR USAAD95005](https://openairdocs.org/sdr/USAAD95005.md): Retract Mech · malfunctioned · Oct 21, 1995 · N919VJ · Doug DC931 · Landing Gear Retraction/Extension System
  > CLT - FLT 880 - AFTER RETRACTING GEAR, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. THE CAPTAIN DECIDED TO RETURN TO CLT. THE FLT LANDED WITHOUT FURTHER INCIDENT. RECYCLED LEFT MAIN GEAR THROUGH 5 CYCLES ON GROUND. GEAR INDICATION NORMAL. AIRCRAFT OK FOR

## 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 = 'N919VJ' AND deregistration_id = 'N919VJ-2003-01-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N919VJ-2003-01-30/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.