# Service difficulty reports: N922TW, cancelled Sep 19, 2017

A list on [N922TW, cancelled Sep 19, 2017](https://openairdocs.org/deregistered/N922TW-2017-09-19.md).

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

- [SDR ZW0A0303202](https://openairdocs.org/sdr/ZW0A0303202.md): Battery Pack · inoperative · Mar 17, 2003 · N922TW · Doug DC982 · Emergency Lighting
  > THE OVERHEAD EMERGENCY LIGHTS AT THE LEFT SIDE NUMBER 2 CABIN DOOR AND JUST BEHIND THE DOOR, AND THE LEFT AND RIGHT EMERGENCY LAMPS IN TAIL AREA, WERE INOPERATIVE. RESEATED THE BATTERIES IN THE BATTERY PACK FOR L2 DOOR LIGHTS, AND REPLACED THE LAMPS P/N 1315
- [SDR ZW0A0203701](https://openairdocs.org/sdr/ZW0A0203701.md): Apu · Mar 27, 2002 · N922TW · Doug DC982 · APU Core Engine
  > SMOKE IN CABIN FROM AIR CONDITIONING. REMOVED AND REPLACED APU. LAST CHECK C PERFORMED 23AUG2001 MCI --CLOSED--
- [SDR ZW0A0107205](https://openairdocs.org/sdr/ZW0A0107205.md): Channel · cracked · Aug 17, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND L-2 HAT SECTION CRACKED AT STA 1418, LT SIDE. REPAIRED PER 53-02 FIG 18. PRIMED AND PAINTED PER SRM 51-10-03. INSTALLED FASTENERS PER SRM 51-30-05.
- [SDR ZW0A0106301](https://openairdocs.org/sdr/ZW0A0106301.md): Structure · damaged · Aug 6, 2001 · N922TW · Doug DC982 · Cargo/Baggage Doors
  > DURING MAINTENANCE A DEEP GROOVE WAS FOUND IN THE CUT OUT FOR THE MID CARGO DOOR HANDLE DUE TO WEAR. REPLACED DOOR HANDLE CUTOUT PER SPM 6-70-01.
- [SDR ZW0A0105506](https://openairdocs.org/sdr/ZW0A0105506.md): Longeron · cracked · Jul 20, 2001 · N922TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT FOUND CRACK IN LONGERON 20L ABOVE FLAP BUS CABLE PULLEYS, STA 1003. REPAIRED LONGERON 20L PER ARA 17776.
- [SDR ZW0A0105505](https://openairdocs.org/sdr/ZW0A0105505.md): Longeron · cracked · Jul 20, 2001 · N922TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT LONGERON 20R HAD TWO CRACKS, ABOVE FLAP BUS CABLE PULLEYS, STA 1003. REPAIRED LONGERON 20R PER ARA 17777.
- [SDR ZW0A0105703](https://openairdocs.org/sdr/ZW0A0105703.md): Fitting · broken · Jul 19, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND BROKEN FITTING, P/N 5956034-552, AT STA 788 BETWEEN LONGERON 27R AND 28R. REPLACED BROKEN FITTING. TREATED AND PRIMED AND INSTALLED PER SRM 51-10-3. INSTALLED PER SRM 51-30-5 AND SRM 51-30-1.
- [SDR ZW0A0105409](https://openairdocs.org/sdr/ZW0A0105409.md): Floorbeam · corroded · Jul 17, 2001 · N922TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT IN THE AFT CABIN FOUND TOP OF FLOORBEAM STA 1322 WAS CORRODED AT LBL 15 TO SIDEWALL. REMOVED CORROSION MECHANICALLY PER SPM 6-80-1. INSTALLED REPAIR PER SRM 53-05, FIG 20A.
- [SDR ZW0A0105408](https://openairdocs.org/sdr/ZW0A0105408.md): Doubler · corroded · Jul 17, 2001 · N922TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT FOUND FINGER DOUBLER CORRODED ON OTBD SIDE OF LONGERON 26L, STA 788, MID CARGO COMPT. REPLACED FINGER DOUBLER PER SPM 6-80-01 AND FASTENERS PER SRM 51-30-0.
- [SDR ZW0A0105407](https://openairdocs.org/sdr/ZW0A0105407.md): Seat Track · corroded · Jul 17, 2001 · N922TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR TRACK, LBL 44, STA 1136 TO 1174, AND 1174 TO 1231. CLEANED MINOR CORROSION STA 1200 TO 1231 PER SPM 6-80-01. TREATED PER SRM 51-10-3. REMOVED TRACK AT STA 1080 TO 1200 AND REPLACED WITH NEW TRACK SECTION.
- [SDR ZW0A0105406](https://openairdocs.org/sdr/ZW0A0105406.md): Intercostal · cracked · Jul 17, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE INTERCOSTAL BETWEEN FLOOR SUPPORTS AT STA 782, ZERO BL WAS CRACKED AND BROKEN. INSTALLED DOUBLER ON INTERCOSTAL. USED 4-5, 5-6, AND 5-7 AD RIVETS PER SRM 53-10-104, PAGE 201 FIG 201.
- [SDR ZW0A0105305](https://openairdocs.org/sdr/ZW0A0105305.md): Longeron · cracked · Jul 13, 2001 · N922TW · Doug DC982 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT ON LT SIDE OF CABIN FOUND CRACKS AT STA 160, LONGERON 3L AND 4L. REPAIRED PER SRM 53-02 FIG 18.
- [SDR ZW0A0105304](https://openairdocs.org/sdr/ZW0A0105304.md): Web · damaged · Jul 13, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND HOLE IN MEMBRANE UNDER CABIN FLOOR, STA 1090 AND LBL 45. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 2.
- [SDR ZW0A0105303](https://openairdocs.org/sdr/ZW0A0105303.md): Floorbeam · cracked · Jul 13, 2001 · N922TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT FOUND CABIN FLOORBEAM FITTING CRACKED AT STA 1308, LBL 35. REMOVED AND REPLACED FITTING PER SRM 51-30-5.
- [SDR ZW0A0105111](https://openairdocs.org/sdr/ZW0A0105111.md): Floor Support · corroded · Jul 12, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 170 TO 200, RBL 7. FOUND CORRODED BEYOND LIMITS AND FABRICATED NEW FLOOR SUPPORT.
- [SDR ZW0A0105110](https://openairdocs.org/sdr/ZW0A0105110.md): Floor Support · corroded · Jul 12, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 194 TO 202, LBL 15. REMOVED OLD SUPPORT AND MADE NEW SUPPORT.
- [SDR ZW0A0105109](https://openairdocs.org/sdr/ZW0A0105109.md): Floor Support · corroded · Jul 12, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, LBL 7. REMOVED OLD FLOOR SUPPORT AND MADE NEW.
- [SDR ZW0A0105108](https://openairdocs.org/sdr/ZW0A0105108.md): Floor Support · corroded · Jul 12, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 200, LBL 6 TO RBL 6. REMOVED OLD SUPPORT AND MADE NEW SUPPORT FROM STOCK. PAINTED AND ALODINED PER SRM 51-10-3 ITEM 30 AND 23. INSTALLED WITH RIVETS PER SRM 51-30-2. SEALED SUPPORT PER SRM 51-20-
- [SDR ZW0A0105006](https://openairdocs.org/sdr/ZW0A0105006.md): Fitting · cracked · Jul 12, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE NOSE GEAR WHEEL WELL FOUND CRACK IN FITTING AT STA 69, LBL 16, THE INBD FITTING AT PRESSURE PANEL. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING, P/N 4912385-501N, PER SPM 6-70-01, SECTION B.2.
- [SDR ZW0A0105004](https://openairdocs.org/sdr/ZW0A0105004.md): Floor Support · corroded · Jul 12, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 185 TO 190, RBL 44. MADE AND INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2.
- [SDR ZW0A0105003](https://openairdocs.org/sdr/ZW0A0105003.md): Floor Support · corroded · Jul 12, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 190 TO 194, RBL 44. MADE AND INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2.
- [SDR ZW0A0105002](https://openairdocs.org/sdr/ZW0A0105002.md): Floor Support · corroded · Jul 12, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 183, RBL 44. MADE AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2.
- [SDR ZW0A0105107](https://openairdocs.org/sdr/ZW0A0105107.md): Seat Track · corroded · Jul 11, 2001 · N922TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 2 FLOOR TRACK AT RBL 22, STA 1080 TO 1250. REPLACED TRACK PER SPM 6-70-01 AND SRM 53-05, FIG 4. PRIMED PER SRM 51-10-3. REMOVED CORROSION PER SPM 6-80-01.
- [SDR ZW0A0105106](https://openairdocs.org/sdr/ZW0A0105106.md): Floor Support · corroded · Jul 11, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT IN CABIN AT STA 180, RBL 8 TO 44. INSTALLED NEW SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-2.
- [SDR ZW0A0105105](https://openairdocs.org/sdr/ZW0A0105105.md): Floor Support · corroded · Jul 11, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION AT STA 198 AND RBL 44, AND AT STA 200 RBL 11. INSTALLED FLOOR SUPPORT AT BOTH LOCATIONS PER SPM 6-70-01 AND RIVETS PER SRM 51-30-2.
- [SDR ZW0A0105104](https://openairdocs.org/sdr/ZW0A0105104.md): Floor Support · corroded · Jul 11, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION IN CABIN AT RBL 11, STA 209. REMOVED SUPPORT AND MADE NEW PART PER DRAWING PL9936535 ITEM 57, AND INSTALLED WITH HI-LOKS PER SRM 51-30-0.
- [SDR ZW0A0105005](https://openairdocs.org/sdr/ZW0A0105005.md): Floor Support · corroded · Jul 11, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION AT RBL 15, STA 200. MADE AND INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2.
- [SDR ZW0A0105103](https://openairdocs.org/sdr/ZW0A0105103.md): Floor Support · corroded · Jul 10, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT, STA 1250, BETWEEN NUMBER 1 AND 2 CHAIR TRACKS, LBL 22 TO 44. FABRICATED AND INSTALLED NEW FLOOR SUPPORT FITTING FROM 7075-T6 EXTRUSION PER SPM 6-70-01.
- [SDR ZW0A0104904](https://openairdocs.org/sdr/ZW0A0104904.md): Floor Support · corroded · Jul 8, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT FITTINGS AT RBL 55, STA 202, 217, AND 208. REMOVED AND REPLACED FITTINGS PER SPM 6-70-01 AND SRM 51-30-05.
- [SDR ZW0A0104903](https://openairdocs.org/sdr/ZW0A0104903.md): Floor Support · corroded · Jul 8, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT AT STA 160 TO 200, LBL 55, WAS CORRODED. REMOVED CORRODED PART AND FABRICATED NEW SUPPORT AND INSTALLED PER SPM 6-70-01 AND SRM 51-30-5.
- [SDR ZW0A0104902](https://openairdocs.org/sdr/ZW0A0104902.md): Web · punctured · Jul 8, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND PUNCTURE IN FLOOR MEMBRANE AT STA 196, LBL 55. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 2.
- [SDR ZW0A0104704](https://openairdocs.org/sdr/ZW0A0104704.md): Angle · cracked · Jul 2, 2001 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CRACK IN LT MAIN GEAR WHEEL WELL FWD SHELF ATTACH ANGLE, FWD LOWER INBD CORNER OF WHEEL WELL. REMOVED AND REPLACED ANGLE WITH FABRICATED PART PER SPM 6-70-01, AND SRM 51-30-5.
- [SDR TWAA0106302](https://openairdocs.org/sdr/TWAA0106302.md): Wire · worn · Apr 8, 2001 · N922TW · Doug DC982 · Light System Wiring
  > THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 15 TO 21. REPLACED POWER FLEX CABLE. CHECK-C 6-10-00 JFK.
- [SDR TWAA0103801](https://openairdocs.org/sdr/TWAA0103801.md): Connector · dirty · Feb 27, 2001 · N922TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS FROM CABIN ROWS 29 THRU 33, AND THE EMERGENCY LIGHTS IN THE TAIL COMPARTMENT, WERE INOPERATIVE. FOUND RIBBON LIGHTS WITH MOISTURE AND DIRT AT CONTACTS. CLEANED RIBBON LIGHT CONNECTOR AND FEED CONNECTOR. CHECK-C 6-10-00 JFK.
- [SDR TWAA0101913](https://openairdocs.org/sdr/TWAA0101913.md): Bulkhead · bird strike · Jan 23, 2001 · N922TW · Doug DC982 · Fuselage Main, Bulkhead
  > ON TAKEOFF SUFFERED BIRD STRIKE AT THE RADOME AREA. THE RADOME BULKHEAD WEB AT STA 37 WAS DAMAGED. INSTALLED NEW BULKHEAD WEB WITH RIVETS AND HI-LOK''S PER SRM 51-30-2 AND SRM 51-30-5. CHECK-C 6-10-00 JFK.
- [SDR TWAA9912102](https://openairdocs.org/sdr/TWAA9912102.md): Power Strip · inop · Sep 3, 1999 · N922TW · Doug DC982 · Emergency Lighting
  > DURING PRE-FLIGHT, FOUND EGRESS LIGHTS INOP AT ROW 7-15 AND 28 AFT. REPLACED POWER LIGHT STRIP. AC-12 STL 7-17-99.
- [SDR TWAA9911002](https://openairdocs.org/sdr/TWAA9911002.md): Power Supply · inop · Aug 8, 1999 · N922TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS WERE ON ALL THE TIME FROM CABIN ROWS 15 TO 31. REPLACED THE POWER SUPPLY. CHECK-C 7-17-99 STL.
- [SDR TWAA9910802](https://openairdocs.org/sdr/TWAA9910802.md): Power Supply · inop · Jul 30, 1999 · N922TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS ILLUMINATED IN FLIGHT WITH THE SWITCH IN THE ARM POSITION, FROM ROW 29 TO THE BACK OF THE CABIN. REPLACED THE POWER SUPPLY. CHECK-C 7-17-99 STL.
- [SDR TWAA9901505](https://openairdocs.org/sdr/TWAA9901505.md): Lamp · failed · Jan 24, 1999 · N922TW · Doug DC982 · Emergency Lighting
  > FOUND THE EVACUATION CHUTE LIGHT INOPERATIVE AT THE FORWARD LT AND RT CABIN DOORS. REPLACED LAMP IN EACH. CHECK-C 7-18-98 STL.
- [SDR TWAA9818904](https://openairdocs.org/sdr/TWAA9818904.md): Battery Pack · discharged · Nov 23, 1998 · N922TW · Doug DC982 · Emergency Lighting
  > DURING PREFLIGHT, FOUND EGRESS LIGHTING INOP BETWEEN ROWS 2 TO 15. REPLACED NR 2 EGRESS BATTERY PACK.
- [SDR TWAA9812301](https://openairdocs.org/sdr/TWAA9812301.md): Tail Cone · deformed · Jul 27, 1998 · N922TW · Doug DC982 · Aerodynamic Fairings
  > DURING C-CHECK, THE TAIL CONE FAILED TO RELEASE DURING ROUTINE CHECK. FOUND THE UPPER SECTION OF THE TAIL CONE WAS DISTORTED SO THAT THE FOUR ATTACH POINTS DID NOT ALIGN WITH THE ATTACHMENT PINS. WAS NECESSARY TO CUT BACK THE TOP OF THE TAIL CONE, DRAW THE P
- [SDR TWAA9812127](https://openairdocs.org/sdr/TWAA9812127.md): Attact Tee · damaged · Jul 18, 1998 · N922TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, FOUND APU RT SIDEWALL ATTACH T WITH END FLANGE CUT OFF WITH 3 ATTACH HOLES TO GAIN ACCESS. INSTALLED FILLERS AND DOUBLERS PER ARA 15416 AND 15416A.
- [SDR TWAA9812104](https://openairdocs.org/sdr/TWAA9812104.md): Bulkhead Fitting · damaged · Jul 14, 1998 · N922TW · Doug DC982 · Fuselage Main, Bulkhead
  > DURING CHECK-C MAINT, FOUND THE AFT BULKHEAD T-FITTING DAMAGED. CRACK WAS 2.5 BY 1.7 AT AREA OF AFT JACK POINT. REMOVED AND REPLACED T AS PER SRM 53-03, FIG 37A.
- [SDR TWAA9712403](https://openairdocs.org/sdr/TWAA9712403.md): Socket · failed · Oct 10, 1997 · N922TW · Doug DC982 · Passenger Compartment Lighting
  > JFK - FLT 780 - CABIN ATTENDANT REPORTED SMELL OF BURNING WIRE AT OVERWING AREA. OVERHEAD AND SIDE LIGHTS TURNED OFF AND SMELL DISSIPATED. LIGHT SOCKET WAS DEACTIVATED AND LATER REPLACED. OP-15 6-20-97 MZJ. (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 = 'N922TW' AND deregistration_id = 'N922TW-2017-09-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N922TW-2017-09-19/reports

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