# Service difficulty reports: N935L, cancelled Aug 27, 2008

A list on [N935L, cancelled Aug 27, 2008](https://openairdocs.org/deregistered/N935L-2008-08-27.md).

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

- [SDR TWAA9915701](https://openairdocs.org/sdr/TWAA9915701.md): Power Supply · inop · Nov 17, 1999 · N935L · Doug DC941 · Emergency Lighting
  > THE FWD SECTION OF COACH CABIN EGRESS LIGHTING WAS INOPERATIVE. REPLACED THE POWER SUPPLY FOR ROWS 8 THRU 14. CHECK-C 9-28-98 STL.
- [SDR TWAA9911301](https://openairdocs.org/sdr/TWAA9911301.md): Motor · failed · Aug 16, 1999 · N935L · Doug DC941 · Stabilizer Control System
  > LONGITUDINAL TRIM CONTROL WHEEL AND SUITCASE HANDLES INOP. REMOVED AND REPLACED LONGITUDINAL PRIMARY TRIM MOTOR TWA STK NR 80374. OPERATIONAL CHECK WAS NORMAL. CHECK C 9-28-98 STL.
- [SDR TWAA9902001](https://openairdocs.org/sdr/TWAA9902001.md): Battery Pack · discharged · Feb 2, 1999 · N935L · Doug DC941 · Emergency Lighting
  > JUST PRIOR TO DEPARTURE FOUND FLOOR EGRESS LIGHTS AT ROW 15 TO 19 REMAINED ON. REPLACED THE BATTERY PACK. CHECK-C 9-28-98 STL.
- [SDR TWAA9814101](https://openairdocs.org/sdr/TWAA9814101.md): Valve · worn · Sep 1, 1998 · N935L · Doug DC941 · Cabin Cooling System
  > CREW REPORTED SLOW PRESSURIZATION LOSS IN FLIGHT. REGAINED CABIN PRESSURIZATION IN DESCENT FROM BETWEEN 11000 AND 16000 FT. FLIGHT RETURNED TO STL. REPLACED RT PACK FLOW CONTROL VALVE, 2022014-2, AND PRESS RATIO SHUT OFF VALVE, 392714-1-1. CHECK-C 6-24-97
- [SDR TWAA9809503](https://openairdocs.org/sdr/TWAA9809503.md): Fan · malfunctioned · Jun 14, 1998 · N935L · Doug DC941 · Cabin Cooling System
  > STL - FLT 598 - AFATER TAKEOFF, THE RT PACK FILLED CABIN WITH SMOKE. THE PACK FAN WAS WORKING. RAN BOTH ENGINES AND RT PACK AND PACK FAN. NO SMOKE NOTED. GROUND CHECKS NORMAL. CHECK-C 3-23-98 MCI. (X)
- [SDR TWAA9714603](https://openairdocs.org/sdr/TWAA9714603.md): Power Supply · inoperative · Dec 13, 1997 · N935L · Doug DC941 · Emergency Lighting
  > STL - FLT 689 - DURING CRUISE, L1 AND R1 DOOR EMERGENCY LIGHTS CAME ON. NO FLOOR LIGHTS. REPLACED POWER SUPPLY AND BATTERIES FOR L1 AND R1 EMERGENCY LIGHTS. MFG P/N 58222-2 POWER SUPPLY. OP-15 06-24-97 STL. (X)
- [SDR TWAA9795003](https://openairdocs.org/sdr/TWAA9795003.md): Trap Panel · cracked · Aug 14, 1997 · N935L · Doug DC941 · Fuselage Miscellaneous Structure
  > STL - RIGHT TRAP PANEL HAS CRACK IN PREVIOUS REPAIR. REMOVED AND REPLACED ENTIRE TRAP PANEL. (M)
- [SDR TWAA9795002](https://openairdocs.org/sdr/TWAA9795002.md): Floorbeam · cracked · Aug 14, 1997 · N935L · Doug DC941 · Fuselage Main, Floor Beam
  > STL - REPAIRED 3 INCH CRACK IN FLOORBEAM AT STATION 237 BY PULLEY BRACKET. (M)
- [SDR TWAA9795001](https://openairdocs.org/sdr/TWAA9795001.md): Seat Track · corrosion · Aug 14, 1997 · N935L · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > STL - REPLACED NR 4 SEAT TRACK FROM STA 200 TO STA 256 DUE TO CORROSION. (X)
- [SDR TWAA9753001](https://openairdocs.org/sdr/TWAA9753001.md): Pump · failed · Apr 25, 1997 · N935L · Doug DC941 · Hydraulic Pump (Electric/Engine), Main
  > STL - FLT 563 - DURING CRUISE LOST RIGHT HYDRAULIC PRESSURE DUE TO WORN RIGHT ENGINE DRIVEN HYDRAULIC PUMP, MFG P/N 314195, MANUFACTURED BY VICKERS INC. OPERATIONAL CHECK NORMAL. (M)
- [SDR TWAA9753004](https://openairdocs.org/sdr/TWAA9753004.md): Longeron · cracked · Apr 17, 1997 · N935L · Doug DC941 · Fuselage Main, Longeron/Stringer
  > STL - DURING SPECIAL CHECK, FOUND A.25 INCH CRACK IN LONGERON 4L, AT BELTRING STATION. INSTALLED REPAIR PER SRM 53-02, FIGURE 2. (M)
- [SDR TWAA9731002](https://openairdocs.org/sdr/TWAA9731002.md): Battery Pack · discharged · Mar 1, 1997 · N935L · Doug DC941 · Emergency Lighting
  > STL - FLT 696 - DURING CRUISE EMERGENCY EGRESS LIGHTS ILLUMINATED IN FORWARD CABIN. REMOVED AND REPLACED WEAK BATTERY PACK, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL. (M)
- [SDR 97ZZZM104](https://openairdocs.org/sdr/97ZZZM104.md): Battery Pack · discharged · Sep 27, 1996 · N935L · Doug DC941 · Emergency Lighting
  > STL - FLT 541 - DURING CRUISE, EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED AT ROWS 8 THROUGH 12. REMOVED AND REPLACED BATTERY PACK, MFG P/N 2013-1A. OPERATIONAL CHECK NORMAL. (M)
- [SDR 96ZZZM1469](https://openairdocs.org/sdr/96ZZZM1469.md): Battery Pack · discharged · Sep 27, 1996 · N935L · Doug DC941 · Emergency Lighting
  > STL - DURING CRUISE, EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED AT ROWS 8 THROUGH 12. REMOVED AND REPLACED BATTERY PACK, MFG P/N 2013-1A. OPERATIONAL CHECK NORMAL.
- [SDR 96ZZZM1465](https://openairdocs.org/sdr/96ZZZM1465.md): Power Supply · inoperative · Sep 24, 1996 · N935L · Doug DC941 · Emergency Lighting
  > STL - DURING CRUISE, EGRESS LIGHTING ILLUMINATED. FOUND WEAK BATTERIES IN POWER SUPPLY, MFG P/N 5822-2. REPLACED POWER SUPPLY. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL.
- [SDR 96ZZZX3624](https://openairdocs.org/sdr/96ZZZX3624.md): Power Supply · inoperative · May 7, 1996 · N935L · Doug DC941 · Emergency Lighting
  > STL - FLT 661 - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED. REMOVED AND REPLACED EMERGENCY EGRESS LIGHT POWER SUPPLY, MFG PN 5822-2. OPERATIONAL CHECK NORMAL. CHECK C - 8-27-95 - STL.
- [SDR 96ZZZM655](https://openairdocs.org/sdr/96ZZZM655.md): Battery Pack · discharged · Mar 11, 1996 · N935L · Doug DC941 · Emergency Lighting
  > STL - DURING CRUISE, EGRESS LIGHTS AT SEAT ROW 15 THROUGH 19 ILLUMINATED. FOUND LIGHTING SYSTEM BATTERIES, MFG P/N 3350-0026-21, WEAK. REPLACED BATTERIES AND EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. (M)
- [SDR 96ZZZX305](https://openairdocs.org/sdr/96ZZZX305.md): Battery Pack · discharged · Jan 4, 1996 · N935L · Doug DC941 · Emergency Lighting
  > STL - FLT 141 - DURING LANDING AND TAXI, THE EGRESS LIGHTS FLICKERED ON AND OFF. FOUND BATTERY PACK, MFG PN 5822-2, WEAK. REPLACED BATTERY PACK AND EGRESS LIGHT, OPERATION CHECKED NORMAL. CHECK C - 8-27-95 - STL.
- [SDR 95ZZZX3404](https://openairdocs.org/sdr/95ZZZX3404.md): Jamb · cracked · Jun 4, 1995 · N935L · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING CHECK C, FOUND A 1.25 INCH RADIAL CRACK AT TOP LEFT SIDE OF AFT VENTRAL DOOR JAMB, RUNNING CIRCUMFERENTIALLY IN RADIUS OF DASH 13 ANGLE. STOP DRILLED PER EMLR NR 65704 AND REPLACED FASTENERS PER SRM CHAPTER 51 AND TWA STANDARD PRACTICES. AIRCRAFT TOTA

## 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 = 'N935L' AND deregistration_id = 'N935L-2008-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N935L-2008-08-27/reports

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