# Service difficulty reports: N926TW, cancelled May 10, 2007

A list on [N926TW, cancelled May 10, 2007](https://openairdocs.org/deregistered/N926TW-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 ZW0A0202101](https://openairdocs.org/sdr/ZW0A0202101.md): Battery Pack · Feb 19, 2002 · N926TW · Doug DC982 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE (LS), PARTIAL EGRESS LIGHT FAILURE BETWEEN ROWS 14-19. REMOVED AND REPLACED BATTERY PACK PER MM 33-59-00. OPERATIONAL CHECK PERFORMED NORMAL. CHECK-C 10/19/01 MCI. --CLOSED--
- [SDR ZW0A0109203](https://openairdocs.org/sdr/ZW0A0109203.md): Seat Track · corroded · Sep 24, 2001 · N926TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT THE FLOOR SEAT TRACK NUMBER 1 FROM STA 1136 TO 1218 HAD CORROSION. REPLACED SEAT TRACK SECTION FROM STA 1136 TO 1218 WITH NEW TRACK PER SRM 53-05, FIG 4F.
- [SDR ZW0A0109202](https://openairdocs.org/sdr/ZW0A0109202.md): Sill · corroded · Sep 24, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON DOOR SILL MEMBRANE AT AFT SERVICE DOOR, STA 1138 TO 1179. REMOVED CORROSION PER SPM 6-80-01. INSTALLED SMALL DOUBLER REPAIR AT STA 1140 PER SRM 53-01, FIG 2.
- [SDR ZW0A0109201](https://openairdocs.org/sdr/ZW0A0109201.md): Attach Fitting · corroded · Sep 24, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE AFT SERVICE DOOR SILL PLATE ATTACH FITTINGS, FWD AND AFT, WERE CORRODED. REMOVED CORRODED FITTINGS AND INSTALLED NEW FITTINGS PER SPM 6-70-01.
- [SDR ZW0A0109105](https://openairdocs.org/sdr/ZW0A0109105.md): Skin · corroded · Sep 22, 2001 · N926TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT ON THE UPPER FUSELAGE, THE SKIN AT STA 226, LONGERON 5L, WAS OUT OF LIMITS AFTER REMOVAL OF CORROSION. INSTALLED EXTERNAL DOUBLER PER SRM 53-04, PAGE 60F.
- [SDR ZW0A0109106](https://openairdocs.org/sdr/ZW0A0109106.md): Seat Track · corroded · Sep 21, 2001 · N926TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT THE NUMBER 1 SEAT TRACK AT LBL 44.5 INCHES HAD CORROSION FROM STA 1218 TO 1302. SPLICED IN NEW SECTION OF TRACK PER SRM 53-05, FIG 4F.
- [SDR ZW0A0109104](https://openairdocs.org/sdr/ZW0A0109104.md): Flange · cracked · Sep 21, 2001 · N926TW · Doug DC982 · Cargo/Baggage Doors
  > DURING CHECK-C MAINT THE AFT CARGO DOOR AFT MID FLANGE WAS CRACKED AT FASTENER HOLES. REPAIRED CARGO DOOR CRACK PER SRM 52-05, PAGE 110A. INSTALLED RIVETS PER SRM 51-30-1.
- [SDR ZW0A0109103](https://openairdocs.org/sdr/ZW0A0109103.md): Seat Track · corroded · Sep 19, 2001 · N926TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON THE NUMBER 2 SEAT TRACK, STA 1041 TO 1309, AT UPPER AND LOWER SURFACES OF FLOOR PANEL BOLT HOLES. REPLACED TRACK PER SRM 53-24-0, FIG 6 WITH TRACK FROM STOCK. REINSTALLED BOLTS AND NUTS PER SRM 51-30-1. INSTALLED TRAC
- [SDR ZW0A0108901](https://openairdocs.org/sdr/ZW0A0108901.md): Web · corroded · Sep 17, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION AT UPPER SURFACE OF MEMBRANE LBL 54 INCHES, STA 1231. REMOVED CORROSION AND CUT OUT DAMAGED AREA. MADE DOUBLER AND INSTALLED PER SRM 51-30-4.
- [SDR ZW0A0108810](https://openairdocs.org/sdr/ZW0A0108810.md): Web · damaged · Sep 17, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND FLOOR MEMBRANE WAS TORN OUT AND ELONGATED HOLES FOR FASTENERS AT LBL 44 INCHES, STA 1175 TO 1191. INSTALLED MEMBRANE REPAIR PER SRM 53-05, FIG 96.
- [SDR ZW0A0108809](https://openairdocs.org/sdr/ZW0A0108809.md): Web · cracked · Sep 14, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE AFT CABIN UPPER SURFACE OF MEMBRANE HAD CORROSION AT STA 1249 FROM LBL 47 INCHES TO LBL 56 IN, THE FLOOR MEMBRANE WAS CRACKED AT STA 1246, LBL 55. THREE BLIND FASTENERS WERE INSTALLED AT MEMBRANE AT STA 1249 LBL 56 IN. UPPER SIDE OF
- [SDR ZW0A0108804](https://openairdocs.org/sdr/ZW0A0108804.md): Floor Support · corroded · Sep 13, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 1155, LBL 23 INCHES TO LBL 44 INCHES. REPLACED WITH NEW PART PER SAMPLE AND SPM 6-70-1 AND DOUGLAS DRAWING 5930544. INSTALLED PER SRM 51-30.
- [SDR ZW0A0108803](https://openairdocs.org/sdr/ZW0A0108803.md): Floor Support · corroded · Sep 13, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT BRACKET AT RBL 10 TO RBL 42, STA 180. REPLACED FLOOR SUPPORT PER SPM 6-70-01.
- [SDR ZW0A0108607](https://openairdocs.org/sdr/ZW0A0108607.md): Skin · damaged · Sep 12, 2001 · N926TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT FOUND A CLASS III REPAIR ON THE FUSELAGE AT STA 237, BETWEEN LONGERON 17L AND 18L. SKIN INSTALLED WITH CHERRY MAX RIVETS AT LONGERON 18 TO 17, STA 235. REMOVED REPAIR AND CUT OUT DAMAGED AREA UNDER REPAIR. INSTALLED FLUSH PATCH PER SSRM
- [SDR ZW0A0108606](https://openairdocs.org/sdr/ZW0A0108606.md): Angle · corroded · Sep 12, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND ANGLE WITH CORROSION AT STA 200, LBL 45. REPLACED CORRODED ANGLE PER SRM 51-30-02.
- [SDR ZW0A0108605](https://openairdocs.org/sdr/ZW0A0108605.md): Seat Track · corroded · Sep 12, 2001 · N926TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CHAIR TRACK DAMAGED AT LBL 44 INCHES, STA 200 INSIDE TRACK. REMOVED CORROSION AND REPLACED CHAIR TRACK PER SPM 6-80-01 PAGE 2, AND SRM 51-30-02.
- [SDR ZW0A0108604](https://openairdocs.org/sdr/ZW0A0108604.md): Pulley Bracket · cracked · Sep 11, 2001 · N926TW · Doug DC982 · Trailing Edge Flap Control System
  > DURING CHECK-C MAINT IN RT WHEEL WELL FOUND CRACK IN MOUNT BRACKET FOR FLAP BUS CABLE PULLEY MOUNT AT STA 994 TO 1003, BETWEEN LONGERON 20R AND 21R. ACCOMPLISHED NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND CONFIRMED CRACK. REMOVED CRACKED PART. INSTA
- [SDR ZW0A0108403](https://openairdocs.org/sdr/ZW0A0108403.md): Frame · corroded · Sep 10, 2001 · N926TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT FOUND CORROSION ON FORMER FOOT AT LONGERON 29R TO LONGERON 29L, STA 1287. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PAINTED PER SRM 51-10-03. FABRICATED AND INSTALLED FORMER SPLICE PER SRM 53-03, FIG 3 AND SRM 51-30-02.
- [SDR ZW0A0108402](https://openairdocs.org/sdr/ZW0A0108402.md): Fitting · cracked · Sep 10, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND IN LT WHEEL WELL POSSIBLE CRACK AT STA 946, KEEL BEAM AREA BETWEEN GEAR DOORS AT RBL 5 INCHES, 3 INCHES ABOVE FAIRING SUPPORTS. ACCOMPLISHED NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6 AND CONFIRMED CRACK. REPLACED FITTING PER
- [SDR ZW0A0108401](https://openairdocs.org/sdr/ZW0A0108401.md): Support · corroded · Sep 10, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT A FWD CABIN FLOOR ANGLE HAD CORROSION AT RBL 5 INCHES TO LBL 5, STA 200. FOUND CORRODED BEYOND LIMITS AND FABRICATED NEW SUPPORT. INSTALLED SUPPORT PER SRM 51-30-2 PAGE 2, FABRICATED PARTS PER SPM 6-70-01, PAGE 1 TO 3.
- [SDR ZW0A0108208](https://openairdocs.org/sdr/ZW0A0108208.md): Web · cracked · Sep 6, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND FLOOR MEMBRANE CRACKED OTBD OF RT OTBD CHAIR TRACK, STA 1271-1287. REPAIRED PER SRM 53-05, PAGE 345.
- [SDR ZW0A0108207](https://openairdocs.org/sdr/ZW0A0108207.md): Floor Support · corroded · Sep 6, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE FLOOR SUPPORT HAD CORROSION AT STA 1212, LBL 14 TO RBL 6. REPLACED SUPPORT WITH NEW PART PER SPM 6-70-01 AND DOUGLAS DRAWING 5936597.
- [SDR ZW0A0108206](https://openairdocs.org/sdr/ZW0A0108206.md): Fitting · cracked · Sep 5, 2001 · N926TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE T FITTING BELOW KEEL BEAM, STA 875, WAS CRACKED. REMOVED FITTING. FABRICATED NEW FITTING AND INSTALLED PER SRM 51-10-4.
- [SDR ZW0A0107303](https://openairdocs.org/sdr/ZW0A0107303.md): Stud · backed out · Aug 22, 2001 · N926TW · Doug DC982 · Turbine Engine Oil System
  > EXPERIENCED AN OIL LOSS ON THE NUMBER 1 ENGINE. SHUT DOWN THE ENGINE AND LANDED AT IND. FOUND OIL FILTER HOUSING STUDS HAD PULLED OUT. WAS NECESSARY TO REPLACE THE ENGINE DUE TO THE TIME THE ENGINE HAD RUN WITH NO OIL. CHECK-C 8-29-00 STL.
- [SDR ZW0A0105301](https://openairdocs.org/sdr/ZW0A0105301.md): Battery Pack · Jul 17, 2001 · N926TW · Doug DC982 · Emergency Lighting
  > DURING PREFLIGHT THE FIRST CLASS EGRESS LIGHTS WERE FOUND INOP. REMOVED MOISTURE FROM EGRESS LIGHT TRACK AND REPLACED BATTERY PACK P/N 5822-2. LAST CHECK C 08/29/00 STL. ---CLOSED---
- [SDR ZW0A0102501](https://openairdocs.org/sdr/ZW0A0102501.md): Battery · discharged · May 30, 2001 · N926TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS DID NOT COME ON FROM ROW 1 TO 7. REPLACED THE DISCHARGED BATTERY PACK P/N 5822-1, REPLACED ONE BURNED OUT LAMP P/N 36262-4, AND CLEANED MOISTURE FROM THE TRACK. CHECK-C 8-29-00 STL.
- [SDR TWAA0014002](https://openairdocs.org/sdr/TWAA0014002.md): Power Supply · inoperative · Sep 8, 2000 · N926TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS WERE ON ALL THE TIME AT ROW 16 TO 20. REPLACED THE POWER SUPPLY. CHECK-C 8-20-00 STL.
- [SDR TWAA0010702](https://openairdocs.org/sdr/TWAA0010702.md): Battery Pack · discharged · Jul 9, 2000 · N926TW · Doug DC982 · Emergency Lighting
  > THE FWD HALF OF THE CABIN HAD THE EGRESS LIGHTS FAIL. REPLACED BATTERY PACK. CHECK-C 8-28-99 JFK.
- [SDR TWAA0003605](https://openairdocs.org/sdr/TWAA0003605.md): Light · contaminated · Mar 6, 2000 · N926TW · Doug DC982 · Emergency Lighting
  > FIRST CLASS EGRESS FLOOR TRACK CONTAMINATED WITH FLUID. REMOVED FC FLOOR HARNESS ASSY, CLEANED CONTAMINATION. REINSTALLED FC FLOOR HARNESS ASSY. AC02 01-12-00 DFW.
- [SDR TWAA9908706](https://openairdocs.org/sdr/TWAA9908706.md): Light · malfunctioned · Jun 22, 1999 · N926TW · Doug DC982 · Emergency Lighting
  > THE CABIN EGRESS LIGHTS AT ROWS 6 TO 16 WERE ILLUMINATED REGARDLESS OF SWITCH POSITION. RECYLED THE EGRESS LIGHT SYSTEM. CHECK-C 10-18-98 STL.
- [SDR TWAA9908701](https://openairdocs.org/sdr/TWAA9908701.md): Battery Pack · discharged · Jun 22, 1999 · N926TW · Doug DC982 · Emergency Lighting
  > THE CABIN EGRESS LIGHTS FROM ROWS 6 TO 16 CAME ON IN FLIGHT. DURING TROUBLESHOOTING FOUND THE FORWARD CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE NUMBER 2 BATTERY PACK FOR THE LIGHTS ON IN FLIGHT, AND CLEANED MOISTURE FROM THE LIGHT TRACK FOR THE INOP
- [SDR TWAA9817503](https://openairdocs.org/sdr/TWAA9817503.md): Battery Pack · discharged · Oct 29, 1998 · N926TW · Doug DC982 · Emergency Lighting
  > THE FLOOR EGRESS LIGHTS AT ROW 29 FORWARD KEPT CYCLING ON AND OFF WITH SWITCH IN THE ARMED POSITION. REPLACED BATTERY PACK AT ROW 24. CHECK-C 10-10-98 STL. ----CLOSED----
- [SDR TWAA9817502](https://openairdocs.org/sdr/TWAA9817502.md): Connector · loose · Oct 29, 1998 · N926TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS AT CABIN ROW 29 FORWARD KEPT COMING ON AND OFF. TIGHTENED CONNECTOR AT THE POWER SUPPLY. CHECK-C 10-10-98 STL. ---CLOSED---
- [SDR TWAA9714903](https://openairdocs.org/sdr/TWAA9714903.md): Receiver · failed · Dec 17, 1997 · N926TW · Doug DC982 · Visual Omnirange (VOR) System
  > STL - FLT 284 - DURING CRUISE, NR 1 VOR FAILED. REPLACED FOR RECEIVER MFG PN 42-607-1. NEW AIRCRAFT. (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 = 'N926TW' AND deregistration_id = 'N926TW-2007-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N926TW-2007-05-10/reports

---
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