# Service difficulty reports: N925TW, cancelled May 10, 2007

A list on [N925TW, cancelled May 10, 2007](https://openairdocs.org/deregistered/N925TW-2007-05-10.md).

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

- [SDR ZW0A0303907](https://openairdocs.org/sdr/ZW0A0303907.md): Skin · damaged · Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS DAMAGED AT STA 596 TO 605, LONGERON 26R AREA. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3. CHECK-C 8-15-02 STL.
- [SDR ZW0A0303906](https://openairdocs.org/sdr/ZW0A0303906.md): Skin · damaged · Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS DAMAGED AT STA 601 TO 604, ABOVE LONGERON 26R, 3.25 INCHES BY 2.625 INCH AND 0.070 DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 1. CHECK-C 8-15-02 STL.
- [SDR ZW0A0303908](https://openairdocs.org/sdr/ZW0A0303908.md): Skin · damaged · Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS DAMAGED AT STA 591 TO 596, BELOW LONGERON 26R, 6 INCHES BY 5 INCHES AND 0.074 DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3.
- [SDR ZW0A0303905](https://openairdocs.org/sdr/ZW0A0303905.md): Skin · damaged · Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS DAMAGED AT STA 588 TO 555, LONGERON 26R TO 26L. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 4. CHECK-C 8-15-02 STL.
- [SDR ZW0A0303904](https://openairdocs.org/sdr/ZW0A0303904.md): Skin · damaged · Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 603, LONGERON 26R TO 27R. SPLICED IN A NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3 OF ARA. CHECK-C 8-15-02 STL.
- [SDR ZW0A0303903](https://openairdocs.org/sdr/ZW0A0303903.md): Skin · damaged · Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 598, LONGERON 25R TO 26R. REPAIRED PER SRM 53-04, FIG 12C, AND AREA NUMBER 1 ON ARA 18438A. CHECK-C 8-15-02 STL.
- [SDR ZW0A0303902](https://openairdocs.org/sdr/ZW0A0303902.md): Skin · damaged · Apr 2, 2003 · N925TW · Doug DC982 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS DAMAGED AT STA 576 TO 579, ABOVE LONGERON 26R, 3.75 INCHES BY 3.75 INCHES AND 0.056 IN DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 2. CHECK-C 8-15-02 STL.
- [SDR ZW0A0301801](https://openairdocs.org/sdr/ZW0A0301801.md): Power Supply · discharged · Feb 8, 2003 · N925TW · Doug DC982 · Emergency Lighting
  > THE TAIL CONE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY.
- [SDR ZW0A0210101](https://openairdocs.org/sdr/ZW0A0210101.md): Power Supply · discharged · Sep 26, 2002 · N925TW · Doug DC982 · Emergency Lighting
  > THE EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED DURING FLIGHT IN FIRST CLASS CABIN. REPLACED EGRESS POWER SUPPLY NUMBER 2 AT ROWS 7 AND 8.
- [SDR ZW0A0210001](https://openairdocs.org/sdr/ZW0A0210001.md): Power Supply · discharged · Sep 25, 2002 · N925TW · Doug DC982 · Emergency Lighting
  > THE ESCAPE PATH LIGHTING IN THE FIRST CLASS SECTION CAME ON IN FLIGHT AND STAYED ON WITH SWITCH IN ARM POSITION. REPLACED THE POWER SUPPLY FOR FIRST CLASS.
- [SDR ZW0A0106503](https://openairdocs.org/sdr/ZW0A0106503.md): Power Supply · Aug 8, 2001 · N925TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHT STRIP ROWS 7 TO 14 CAME ON INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 7-29-01 STL. --CLOSED--
- [SDR ZW0A0106502](https://openairdocs.org/sdr/ZW0A0106502.md): Light · intermittent · Aug 8, 2001 · N925TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS ROWS 7 TO 14 CAME ON INTERMITTENTLY. OPERATIONAL TEST NORMAL.
- [SDR ZW0A0106501](https://openairdocs.org/sdr/ZW0A0106501.md): Battery Pack · Aug 7, 2001 · N925TW · Doug DC982 · Emergency Lighting
  > THE CENTER SECTION OF EGRESS LIGHTS ILLUMINATED WITH THE SWITCH IN EITHER ARMED OR ON POSITION. REPLACED THE BATTERY PACK. CHECK-C 7-29-01 STL. --CLOSED--
- [SDR TWAA0104101](https://openairdocs.org/sdr/TWAA0104101.md): Power Supply · malfunctioned · Mar 3, 2001 · N925TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS AT ROWS 16 TO 23 CAME ON IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 11-2-00 MCI.
- [SDR TWAA0017510](https://openairdocs.org/sdr/TWAA0017510.md): Panel · delaminated · Oct 1, 2000 · N925TW · Doug DC982 · Spoilers
  > DURING CHECK-C MAINT, THE LT WING UPPER OUTBOARD PANEL FWD OF GROUND SPOILER HAD DELAMINATION ABOUT 11 RIVETS AT OUTBOARD EDGE. REPLACED PANEL PER SRM 6-70-01.
- [SDR TWAA0011801](https://openairdocs.org/sdr/TWAA0011801.md): Rib · cracked · Jul 24, 2000 · N925TW · Doug DC982 · Leading Edge Devices
  > THE RT WING NUMBER 4 SLAT O/B NUMBER 12 SLAT RIB WAS CRACKED. REPLACED THE SLAT PER M99-27-02. CHECKK-C 8-21-99 STL.
- [SDR TWAA9914707](https://openairdocs.org/sdr/TWAA9914707.md): Splice · cracked · Oct 30, 1999 · N925TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING LS, FOUND STATION 240 LONGERON L19 SPLICE IS CRACKED. INSTALLED NEW SPLICE IN ACCORDANCE WITH SRM 53-02 FIG 18.
- [SDR TWAA9908003](https://openairdocs.org/sdr/TWAA9908003.md): Turbine · damaged · Jun 5, 1999 · N925TW · Doug DC982 · Turbine Section
  > THE RT ENGINE SHUT ITSELF DOWN WHILE EGT INDICATION INCREASED. CREW ACCOMPLISHED THE ENGINE SHUT DOWN PROCEDURE AND MADE UNSCHEDULED LANDING AT IND. FOUND TURBINE FAILURE AND REPLACED THE ENGINE. CHECK-C 8-24-98 STL. *S/D* FOUND FOD IMPACT TO 1 EACH 7TH S
- [SDR TWAA9816801](https://openairdocs.org/sdr/TWAA9816801.md): Deflector · out of position · Oct 19, 1998 · N925TW · Doug DC982 · Nose/Tail Landing Gear
  > NOSE GEAR FAILED TO RETRACT ON TAKEOFF. RECYCLED GEAR ONCE NO HELP. RETURNED TO STL. FOUND SOME HARDWARE MISSING FROM THE NLG SPRAY DEFLECTOR, ALLOWING THE DEFLECTOR TO ROTATE. REPLACED A NUT, MFG AN320-8, BOLT, NAS 6208-11D, WASHER, NAS1106-28D, AND PIN,
- [SDR TWAA9801406](https://openairdocs.org/sdr/TWAA9801406.md): Gyro · worn · Jan 26, 1998 · N925TW · Doug DC982 · Attitude Gyro and Indicating System
  > STL - FLT 455 - STARTING DESCENT INTO OMA, BOTH FLIGHT DIRECTORS FAILED. RETURNED TO FLIGHT ORIGINATION STATION, STL. REPLACED NR 1 VERTICAL GYRO. CHECK-C, 8-17-97 BFM. (X)
- [SDR TWAA9715401](https://openairdocs.org/sdr/TWAA9715401.md): Door · not closed · Dec 30, 1997 · N925TW · Doug DC982 · Cargo/Baggage Doors
  > STL - FLT 468 - AFTER TAKEOFF DURING CLIMB, AIRCRAFT WOULD NOT PRESSURIZE. FOUND MID-CARGO BEARER PIN HOLDING DOOR OPEN. REMOVED PIN AND SECURED DOOR. CK-C 2D 8-17-97. (X)

## 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 = 'N925TW' AND deregistration_id = 'N925TW-2007-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N925TW-2007-05-10/reports

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