# Service difficulty reports: N914TW, cancelled Sep 6, 2012

A list on [N914TW, cancelled Sep 6, 2012](https://openairdocs.org/deregistered/N914TW-2012-09-06.md).

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

- [SDR ZW0A0208203](https://openairdocs.org/sdr/ZW0A0208203.md): B-Nut · loose · Aug 3, 2002 · N914TW · Doug DC982 · Pneumatic Distribution System
  > DURING TAKEOFF HIGH TEMP LIGHT IN TAIL COMPARTMENT RESULT IN UNSCHEDULED LANDING/RETURN TO STL. PNEUMATIC PRESS REGULATOR RELIEF LINE LOOSE HEAT EXCHANGE VENTING TO TAIL COMPARTMENT RT HEAT EXCHANGE PERRY SEAL LEAKING. TIGHTENED B-NUT ON LT PRESS REGULATOR R
- [SDR ZW0A0204604](https://openairdocs.org/sdr/ZW0A0204604.md): Connector · loose · Apr 23, 2002 · N914TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTING ROWS 7 TO 15 WERE INOPERATIVE. RESET THE CONNECTORS.
- [SDR ZW0A0204102](https://openairdocs.org/sdr/ZW0A0204102.md): Battery · discharged · Apr 5, 2002 · N914TW · Doug DC982 · Emergency Lighting
  > THE EMERGENCY EVACUATION LIGHTS IN THE CABIN WERE ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. REPLACED THE BATTERIES IN THE POWER SUPPLY.
- [SDR ZW0A0203901](https://openairdocs.org/sdr/ZW0A0203901.md): Power Supply · Apr 1, 2002 · N914TW · Doug DC982 · Emergency Lighting
  > DURING CLIMB AND DESCENT THE FIRST CLASS CABIN EGRESS LIGHTS ILLUMINATED. REPLACED THE POWER SUPPLY. CHECK-C 3-4-01 STL. --CLOSED--
- [SDR ZW0A0203303](https://openairdocs.org/sdr/ZW0A0203303.md): Frame · corroded · Mar 14, 2002 · N914TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT THE FORMER RING AND REPAIR WERE CORRODED AT STA 1309, LONGERON 27R TO 27L. REMOVED AND INSTALLED NEW FRAME AND INSTALLED REPAIR SPLICES PER SRM 53-03, FIG 2A.
- [SDR ZW0A0203302](https://openairdocs.org/sdr/ZW0A0203302.md): Cargo Track · corroded · Mar 14, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT THE LT FLOOR TRACK IN THE AFT CARGO COMPARTMENT WAS CORRODED FROM STA 1211 TO 1320. INSTALLED NEW TRACK IN CARGO COMPARTMENT, LT SIDE, AND INSTALLED SPLICE PLATE PER SRM 53-05, FIG 4G.
- [SDR ZW0A0203301](https://openairdocs.org/sdr/ZW0A0203301.md): Intercostal · corroded · Mar 14, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE INTERCOSTAL WAS CORRODED AT STA 1308 TO 1322, BETWEEN LONGERON 27 AND 28, LT SIDE. DRILLED NEW INTERCOSTAL AND END FITTINGS AND INSTALLED PER SRM 51-30-2 AND 5, AND SPM 6-70-01.
- [SDR ZW0A0203102](https://openairdocs.org/sdr/ZW0A0203102.md): Floor Support · corroded · Mar 12, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN AFT CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 1320, LONGERON 23L TO 23R. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01, 4B.
- [SDR ZW0A0203104](https://openairdocs.org/sdr/ZW0A0203104.md): Floor Support · corroded · Mar 8, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION ON CAPTAINS KICKPLATE BULKHEAD AND FLOOR PANEL SUPPORT. REMOVED CORROSION PER SPM 6-80-01. FABRICATED NEW SUPPORT AND INSTALLED PER SRM 51-30-5.
- [SDR ZW0A0203103](https://openairdocs.org/sdr/ZW0A0203103.md): Seat Track · corroded · Mar 8, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND PILOTS AFT INBD SEAT TRACK WAS CORRODED. REMOVED AND REPLACED TRACK PER SRM 51-01, PAGE 1, ITEM C.
- [SDR ZW0A0203106](https://openairdocs.org/sdr/ZW0A0203106.md): Seat Track · corroded · Mar 6, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 6 RH O/B SEAT TRACK, FROM STA 256 TO 313. REPLACED SECTION OF SEAT TRACK USING SEAT TRACK SPLICE AT STA 421. TRACK CHANGED FROM STA 214 TO 421, PER SRM 53-05, PAGE 104.
- [SDR ZW0A0203105](https://openairdocs.org/sdr/ZW0A0203105.md): Frame · corroded · Mar 6, 2002 · N914TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT IN THE AFT CABIN AND CARGO BIN, THE FORMER RING WAS CORRODED AT STA 1271, LONGERON 27L TO 29R. INSTALLED NEW Z FRAME FROM LBL 37 TO RBL 11, PER SRM 53-02, FIG 2.
- [SDR ZW0A0202401](https://openairdocs.org/sdr/ZW0A0202401.md): Web · corroded · Feb 25, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C FOUND LT AFT LAV AT STA 1338 TO 1350, STRINGER 18L TO 17L, LBL 50 TO 56, THE FLOORBEAM FRAME AT FUSELAGE SKIN AREA, WEB HAD CORROSION. REMOVED CORROSION PER SRM 51-10-3. REPLACED DAMAGED WEB SECTION PER 51-70-4. INSTALLED NEW CHORD FITTING.
- [SDR ZW0A0202402](https://openairdocs.org/sdr/ZW0A0202402.md): Angle · corroded · Feb 20, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE LEFT SIDE MOST FORWARD CABIN DOOR JAMB, 2 ANGLES HAD CORROSION AT STA 180 TO 200. FABRICATED AND INSTALLED PER SRM 1-10-02, 1-10-03, 51-30-02, 51-14-01, AND SPM 6-10-01.
- [SDR ZW0A0202204](https://openairdocs.org/sdr/ZW0A0202204.md): Trunnion · cracked · Feb 14, 2002 · N914TW · Doug DC982 · Main Landing Gear Attach Section
  > DURING CHECK-C MAINT IN THE LT WHEEL WELL, FOUND CRACK IN LT GEAR SUPPORT CASTING ABOVE THE LT INBOARD FLAP TRACK, AND ABOVE THE LT FLAP BUSS CABLE BRACKET. REPAIRED GEAR SUPPORT CASTING PER ARA 18090.
- [SDR ZW0A0202006](https://openairdocs.org/sdr/ZW0A0202006.md): Bracket · cracked · Feb 13, 2002 · N914TW · Doug DC982 · Cargo/Baggage Doors
  > DURING CHECK-C MAINT THE MID CARGO DOOR BOTTOM INBOARD BRACKET WAS CRACKED, LOWER SIDE FOR AFT BOTTOM DOOR STOP. FABRICATED NEW BRACKET AND INSTALLED.
- [SDR ZW0A0202005](https://openairdocs.org/sdr/ZW0A0202005.md): Bracket · cracked · Feb 13, 2002 · N914TW · Doug DC982 · Cargo/Baggage Doors
  > DURING CHECK-C MAINT IN THE MID CARGO COMPARTMENT, THE AFT BOTTOM DOOR STOP BRACKET WAS CRACKED INSIDE THE DOOR, ON THE FWD FACE. REMOVED AND REPLACED CRACKED BRACKET WITH NEW PER SRM 51-01, AND SPM 6-70-01.
- [SDR ZW0A0201807](https://openairdocs.org/sdr/ZW0A0201807.md): Cargo Track · corroded · Feb 13, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT IN CARGO COMPT FOUND CORROSION ON TIE DOWN TRACK AT STA 785, RT SIDE. REPLACED TRACK WITH NEW AT STA 693 TO 788 PER SPM 6-70-01.
- [SDR ZW0A0201806](https://openairdocs.org/sdr/ZW0A0201806.md): Tie Clip · corroded · Feb 12, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE AFT CABIN STA 1338 TIE CLIP HAD CORROSION AT RBL 57 AREA. INSTALLED NEW CLIP PER SPM 6-70-01.
- [SDR ZW0A0201805](https://openairdocs.org/sdr/ZW0A0201805.md): Web · corroded · Feb 12, 2002 · N914TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE AFT CABIN STA 1338, RBL 57, WEB HAD HEAVY CORROSION 6 INCHES BELOW FLOORBEAM RT LAV. INSTALLED FILLER DOUBLER PER SRM 51-70-4.
- [SDR ZW0A0202002](https://openairdocs.org/sdr/ZW0A0202002.md): Stop Fitting · cracked · Feb 8, 2002 · N914TW · Doug DC982 · Cargo/Baggage Doors
  > DURING CHECK-C MAINT IN MID CARGO COMPT THE AFT BOTTOM DOOR STOP BRACKET, INSIDE THE DOOR, IS CRACKED ON AFT SIDE. REMOVED AND REPLACED CRACKED BRACKET AND REPLACED WITH NEW PER SRM 51-01, PAGE 1.
- [SDR ZW0A0202001](https://openairdocs.org/sdr/ZW0A0202001.md): Floorbeam · corroded · Feb 8, 2002 · N914TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT FOUND CORROSION IN RT FLOORBEAM BETWEEN STA 636 AND 693. REMOVED CORROSION PER SPM 6-80-01. INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-05, FIG 20A.
- [SDR ZW0A0201804](https://openairdocs.org/sdr/ZW0A0201804.md): Bracket · cracked · Feb 7, 2002 · N914TW · Doug DC982 · Cargo/Baggage Doors
  > DURING CHECK-C MAINT THE FORWARD CARGO COMPARTMENT DOOR HAD A SMALL BRACKET CRACKED LOCATED INSIDE THE SECOND LIGHTENING HOLE FROM THE AFT END, AT LOWER EDGE OF THE FWD CARGO COMPARTMENT DOOR. CONFIRMED WITH EDDY CURRENT. INSTALLED FITTING.
- [SDR ZW0A0201803](https://openairdocs.org/sdr/ZW0A0201803.md): Cargo Track · corroded · Feb 7, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT FOUND CORROSION ON FLOOR TRACK AT STA 1211 TO 1320, RT TRACK. REPLACED TRACK PER SPM 6-70-01-4B, AND SRM 51-30-01.
- [SDR ZW0A0201802](https://openairdocs.org/sdr/ZW0A0201802.md): Cargo Track · corroded · Feb 7, 2002 · N914TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT FOUND CORROSION ON THE LT TIE DOWN TRACK FROM STA 1003 TO 1231. INSTALLED NEW TIE DOWN TRACK PER SPM 6-70-01-4B, AND SRM 51-30-01.
- [SDR ZW0A0201602](https://openairdocs.org/sdr/ZW0A0201602.md): Keelbeam · cracked · Feb 7, 2002 · N914TW · Doug DC982 · Fuselage Main, Keel
  > DURING CHECK-C IN LT WHEEL WELL, FOUND ANGLE CRACKED FWD OF HINGE CASTING AT KEEL BEAM. REMOVED AND REPLACED CRACKED ANGLE PER SPM 6-70-01.
- [SDR ZW0A0201601](https://openairdocs.org/sdr/ZW0A0201601.md): Frame · corroded · Feb 7, 2002 · N914TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C FOUND CABIN STA 1338 LONGERON 18R, FRAME HAS CORROSION FROM FLOOR LEVEL TO 6 INCHES UP THE FWD SIDE. CORROSION WAS REMOVED PER SPM 6-80-01.
- [SDR TWAA0104605](https://openairdocs.org/sdr/TWAA0104605.md): Battery Pack · discharged · Mar 10, 2001 · N914TW · Doug DC982 · Emergency Lighting
  > THE EMERGENCY LIGHTS CAME ON DURING FLIGHT AT ROW 5 THRU 15. REPLACED THE BATTERY PACK. CHECK-C 2-13-01 STL.
- [SDR TWAA0104603](https://openairdocs.org/sdr/TWAA0104603.md): Battery Pack · disconnected · Mar 10, 2001 · N914TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS AT ROW 5 THRU 15 CAME ON DURING FLIGHT. ALL THE LIGHTS WENT OUT WITH THE EMERGENCY LIGHT SWITCH TURNED OFF. RECONNECTED THE BATTERY PACK AT ROW 5. CHECK-C 2-13-01 STL.
- [SDR TWAA0104604](https://openairdocs.org/sdr/TWAA0104604.md): Battery · discharged · Mar 9, 2001 · N914TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS COME ON AT ROW 5 TO 15. REPLACED THE EMERGENCY LIGHT BATTERIES. CHECK-C 2-13-01 STL.
- [SDR TWAA0104501](https://openairdocs.org/sdr/TWAA0104501.md): Battery · discharged · Mar 8, 2001 · N914TW · Doug DC982 · Emergency Lighting
  > A SECTION OF EGRESS LIGHTING IN THE FIRST CLASS CABIN ILLUMINATED DURING TAXI AND WOULD NOT RESET. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 2-13-01 STL.
- [SDR TWAA0104403](https://openairdocs.org/sdr/TWAA0104403.md): Battery Pack · discharged · Mar 7, 2001 · N914TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS ON CABIN FLOOR AND AT THE LEFT SIDE NUMBER 2 CABIN DOOR OCCASIONALLY ILLUMINATED IN FLIGHT. REPLACED THE BATTERY PACK. CHECK-C 2-13-01 STL.
- [SDR TWAA0104402](https://openairdocs.org/sdr/TWAA0104402.md): Light · intermittent · Mar 7, 2001 · N914TW · Doug DC982 · Emergency Lighting
  > THE FIRST SECTION OF CABIN EGRESS LIGHTS REPORTED TO INTERMITTENTLY STAY ILLUMINATED. RESET THE EMERGENCY LIGHT ARM AND CHARGE CIRCUIT BREAKER AND LIGHTS OPERATED NORMALLY. CHECK-C 2-13-01 STL.
- [SDR TWAA0100902](https://openairdocs.org/sdr/TWAA0100902.md): Switch · inoperative · Jan 14, 2001 · N914TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTING WAS INOPERATIVE FROM CABIN ROWS 5 TO 14. RECYCLED THE EMERGENCY LIGHT SWITCH. CHECK-C 2-3-00 STL.
- [SDR TWAA0017001](https://openairdocs.org/sdr/TWAA0017001.md): Battery Pack · worn · Oct 31, 2000 · N914TW · Doug DC982 · Emergency Lighting
  > THE FIRST CLASS OVERHEAD EMERGENCY LIGHT AND ONE SECTION OF COACH FLOOR EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AT ROW 3 AND THE FEEDER STRIP IN THE FIRST CLASS DIVIDER. CHECK-C 2-3-00 STL.
- [SDR TWAA0015606](https://openairdocs.org/sdr/TWAA0015606.md): Compressor · fod · Oct 5, 2000 · N914TW · Doug DC982 · Turbine Engine Compressor Section
  > CREW ABORTED TAKEOFF AT 65 KTS DUE TO RT ENGINE STALL WITH VIBRATION ON RT FUEL CONTROL LEVER. ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO THE GATE. COMPRESSOR HAD FAILED WITH ENGINE CASE PENETRATION, INCLUDING ONE INSTANCE OF UNCONTAINED FAILURE AT 12 O''CL
- [SDR TWAA9917001](https://openairdocs.org/sdr/TWAA9917001.md): Vhf Radio · contaminated · Dec 15, 1999 · N914TW · Doug DC982 · VHF Communications System
  > THE NUMBER 1 AND 2 VHF COMM RADIOS WERE INOPERATIVE AFTER TAKEOFF. STATIC WAS TRANSMITTED ON ANY FREQUENCY SELECTED. FLIGHT RETURNED TO STL. FOUND MOISTURE IN THE CAPTAINS AUDIO SELECTOR PANEL AND REPLACED THE PANEL. CHECK-C 2-13-99 MCI.
- [SDR TWAA9916901](https://openairdocs.org/sdr/TWAA9916901.md): Light · inoperative · Dec 14, 1999 · N914TW · Doug DC982 · Emergency Lighting
  > THE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROW 4 TO 16. FOUND FEEDER CABLE BROKEN AND SPLICED CABLE TOGETHER. CHECK-C 2-13-99 MCI.
- [SDR TWAA9906401](https://openairdocs.org/sdr/TWAA9906401.md): Turbine · failed · Apr 3, 1999 · N914TW · Doug DC982 · Turbine Section
  > DURING TAKEOFF, THERE WAS A LOUD NOISE FROM THE NUMBER 1 ENG FOLLOWED BY HIGH EGT INDICATION. THE ENG WAS SHUT DOWN AND THE FLIGHT RETURNED TO STL. FOUND THE TURBINE HAD FAILED. REPLACED THE ENGINE. CHECK-C 2-13-99 MCI.
- [SDR TWAA9819301](https://openairdocs.org/sdr/TWAA9819301.md): Coffeemaker · failed · Dec 4, 1998 · N914TW · Doug DC982 · Buffet/Galleys
  > THE NUMBER 3 GALLEY COFFEEMAKER CAUSED SPARKS. CREW PULLED CIRCUIT BREAKER. MAINT REPLACED THE COFFEEMAKER. CHECK-C 2-28-98 MCI.
- [SDR TWAA9812501](https://openairdocs.org/sdr/TWAA9812501.md): Boost Pump · worn · Aug 3, 1998 · N914TW · Doug DC982 · Fuel Boost Pump
  > ABOVE FL 300 COULD NOT PUMP FUEL FROM CENTER TANK. TURNED OFF LEFT TANK PUMPS AND DESCENDED IN ALTITUDE AND CENTER TANK STARTED FEEDING. RETURNED TO MCI. REPLACED BOTH CENTER TANK FUEL BOOST PUMPS. CHECK-C 2-28-98 MCI.
- [SDR 96ZZZM1202](https://openairdocs.org/sdr/96ZZZM1202.md): Bulb · failed · Jul 10, 1996 · N914TW · Doug DC982 · Landing Gear Position and Warning
  > SFO - DURING GEAR EXTENSION RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB IN LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. (M)
- [SDR 96ZZZM46](https://openairdocs.org/sdr/96ZZZM46.md): Strut Seals · failed · Dec 23, 1995 · N914TW · Doug DC982 · Nose/Tail Landing Gear Strut/Axle
  > TPA - DURING LANDING, UNABLE TO LOWER NOSE GEAR. CYCLED LANDING GEAR. NOSE STRUT SEALS REPLACED, REPACKED NOSE STRUT. CYCLED GEAR AND OPERATIONS ARE NORMAL.
- [SDR 95ZZZX3411](https://openairdocs.org/sdr/95ZZZX3411.md): Blade · failed · Jun 22, 1995 · N914TW · Doug DC982 · Turbine Engine Compressor Section
  > DEN - FLT 427 - DURING DESCENT, SHUT DOWN LEFT ENGINE DUE TO SPOOLED DOWN WITH INCREASING EGT. FOUND METAL PARTICLES IN TAILPIPE. CHANGED ENGINE, S/N 1205. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 21,594 HOURS; 10,979 CYCLES. OP-15 - 12-3-94 -
- [SDR 95ZZZW339](https://openairdocs.org/sdr/95ZZZW339.md): Retract Sys · req'd lube · Mar 20, 1995 · N914TW · Doug DC982 · Landing Gear Retraction/Extension System
  > BOS - AFTER TAKEOFF NOSE LANDING GEAR DID NOT RETRACT. CYCLED LANDING GEAR, AND NOSE LANDING GEAR RETRACTED. INSPECTED NOSE LANDING GEAR AND LUBRICATED. JACKED NOSE LANDING GEAR AND OPERATED NOSE LANDING GEAR SEVERAL TIMES AND ALL OPERATIONS WERE NORMAL.

## 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 = 'N914TW' AND deregistration_id = 'N914TW-2012-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N914TW-2012-09-06/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.