# Service difficulty reports: N904TW, cancelled Aug 16, 2013

A list on [N904TW, cancelled Aug 16, 2013](https://openairdocs.org/deregistered/N904TW-2013-08-16.md).

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

Page 1 of 2 · 87 reports

- [SDR ZW0A0105401](https://openairdocs.org/sdr/ZW0A0105401.md): O-Ring · Jul 19, 2001 · N904TW · Doug DC982 · Hydraulic Power System
  > ON FINAL APPROACH, LOST RIGHT HAND HYD SYSTEM DUE TO FLUID LOSS. FOUND RIGHT HAND THRUST REVERSER CONTROL VALVE PRESSURE LINE FITTING HAD A FLAT TORN O-RING. REPLACED O-RING P/N NAS1612-6 DUE TO WEAR. LAST CHECK C 03/12/01 MCI ---CLOSED---
- [SDR ZW0A0104003](https://openairdocs.org/sdr/ZW0A0104003.md): Battery Pack · Jun 22, 2001 · N904TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS FROM ROW 15 THRU THE AFT CABIN ILLUMINATED WITH THE SWITCH ARMED. REPLACED THE BATTERY PACK. CHECK-C 5-18-01 MCI. --CLOSED---
- [SDR ZW0A0103203](https://openairdocs.org/sdr/ZW0A0103203.md): Power Supply · discharged · Jun 8, 2001 · N904TW · Doug DC982 · Emergency Lighting
  > THE EGRESS LIGHTS CAME ON INTERMITTENTLY IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 5-18-2001.
- [SDR ZW0A0101801](https://openairdocs.org/sdr/ZW0A0101801.md): Seat Track · corroded · May 8, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 1 CHAIR TRACK, STA 1174 TO 1250. INSTALLED NEW TRACK AT STA 1174 TO 1250 PER SRM 53-05, FIG 4.
- [SDR ZW0A0101302](https://openairdocs.org/sdr/ZW0A0101302.md): Seat Track · corroded · May 4, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON CABIN NUMBER 2 SEAT TRACK, STA 1117 TO 1250. REPLACED SECTION OF TRACK FROM STA 1117 TO 1250 PER SRM 51-30-2, 51-30-1, 51-10-3, AND SPM 6-70-1.
- [SDR ZW0A0101205](https://openairdocs.org/sdr/ZW0A0101205.md): Web · corroded · May 4, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE FWD CABIN, THE FLOOR MEMBRANE WAS CORRODED AT STA 160 TO 200, RBL 53 TO RBL 9. REPLACED MEMBRANE PER SPM 6-20-1 AND SRM 53-30-2.
- [SDR ZW0A0101113](https://openairdocs.org/sdr/ZW0A0101113.md): Web · cracked · May 3, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN RT FWD CABIN BETWEEN STA 218 AND 237, RBL 58 INCHES, MEMBRANE HAD CORRODED AND CRACKED AT NUMBER 6 FLOOR TRACK. SHOP FABRICATED NEW MEMBRANE AND INSTALLED PER SPM 6-70-01, PAGE 3 PARAGRAPH 4-B-2.
- [SDR ZW0A0101112](https://openairdocs.org/sdr/ZW0A0101112.md): Web · corroded · May 2, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CABIN FLOOR MEMBRANE CORRODED AT STA 151, RBL 5. REPAIRED PER SRM 53-01, FIG 4.
- [SDR ZW0A0101111](https://openairdocs.org/sdr/ZW0A0101111.md): Seat Track · corroded · May 2, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT CABIN FLOOR TRACK NUMBER 5 WAS CORRODED BETWEEN STA 200 AND 246. REPLACED TRACK PER SRM 53-05, FIG 4F.
- [SDR ZW0A0101110](https://openairdocs.org/sdr/ZW0A0101110.md): Floor Support · corroded · May 2, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 148 TO 160 RBL 7, STA 160 LBL 5 TO RBL 5, STA 200 LBL 9 TO RBL 49, AND STA 180 RBL 9 TO 43. INSTALLED NEW SUPPORTS PER SPM 6-70-01 AND SRM 51-30.
- [SDR ZW0A0101109](https://openairdocs.org/sdr/ZW0A0101109.md): Floor Support · corroded · May 2, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 160 TO 200, RBL 5, RBL 43 AND RBL 53. INSTALLED NEW SUPPORTS PER SPM 6-70-01 AND SRM 51-30.
- [SDR ZW0A0101108](https://openairdocs.org/sdr/ZW0A0101108.md): Web · corroded · May 1, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE AFT CABIN AND CARGO COMPT, CABIN FLOOR MEMBRANE WAS CORRODED AT STA 1250, LBL 51. REMOVED CORRODED AREA AND REPAIRED PER SRM 53-01, FIG 4.
- [SDR ZW0A0101107](https://openairdocs.org/sdr/ZW0A0101107.md): Seat Track · corroded · May 1, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT IN THE FWD CABIN FOUND CORROSION AT FLOOR TRACK NUMBER 4, BETWEEN STA 200 AND 237. REMOVED AND REPLACED PORTION OF CHAIR TRACK, AS REQUIRED, PER SRM 53-21-037. TREATED AND PRIMED PER SRM 51-10-3.
- [SDR ZW0A0101306](https://openairdocs.org/sdr/ZW0A0101306.md): Cargo Track · corroded · Apr 30, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK HAD CORROSION FROM STA 1212 TO 1322. INSTALLED NEW TRACK FROM STA 1212 TO STA 1322.
- [SDR ZW0A0101004](https://openairdocs.org/sdr/ZW0A0101004.md): Fairing · damaged · Apr 30, 2001 · N904TW · Doug DC982 · Elevator, Plate/Skin
  > DURING CHECK-C MAINT ON RT ELEVATOR FOUND HOLE IN LINKAGE FAIRING ON LOWER SIDE, JUST FWD OF FWD HALF PANEL NUMBER 3616. REPAIRED AREA PER SRM 51-70-3 AND ARA 17747. BALANCE CALCULATION PER SRM 55-20-2 AND FOUND WITHIN LIMITS.
- [SDR ZW0A0101003](https://openairdocs.org/sdr/ZW0A0101003.md): Seat Track · corroded · Apr 30, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT IN FWD CABIN FOUND NUMBER 2 FLOOR TRACK AT STA 207 HAD CORROSION. CUT NUMBER 2 TRACK AT STA 247. REPLACED WITH NEW FROM STA 200 TO 247. SPLICED PER SRM 53-05-4F.
- [SDR ZW0A0101002](https://openairdocs.org/sdr/ZW0A0101002.md): Intercostal · corroded · Apr 27, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT, INTERCOSTAL AT STA 1237, BETWEEN LONGERON 24L AND 25L, HAD CORROSION. REMOVED CORROSION PER SPM 6-80-01. REINSTALLED INTERCOSTAL PER SRM 51-30-05 AND 51-30-02.
- [SDR ZW0A0101001](https://openairdocs.org/sdr/ZW0A0101001.md): Seat Track · corroded · Apr 27, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND NUMBER 1 CABIN SEAT TRACK WITH CORROSION, STA 1104 TO 1136. REPLACED SEAT TRACK PER SRM 53-05, FIG 4F.
- [SDR ZW0A0100815](https://openairdocs.org/sdr/ZW0A0100815.md): Seat Track · corroded · Apr 26, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND SEAT TRACK BOTTOM CORRODED AT STA 1155 TO STA 1308, AT LBL 22. TRACK REMOVED FROM STA 1136 TO 1308. NEW SECTION FABRICATED FROM EXTRUSION AND INSTALLED PER SPM 6-70-1.
- [SDR ZW0A0100826](https://openairdocs.org/sdr/ZW0A0100826.md): Floorbeam · corroded · Apr 25, 2001 · N904TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT FOUND CABIN FLOOR BEAM AT STA 1155 TO 1611 LBL HAD CORROSION. REMOVED OLD FLOOR SUPPORT AND FABRICATED NEW FROM EXTRUDED STOCK. INSTALLED WITH HI-LOKS PER SPM 6-70-01.
- [SDR ZW0A0100825](https://openairdocs.org/sdr/ZW0A0100825.md): Seat Track · corroded · Apr 25, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT SEAT TRACK BOTTOM FOUND CORRODED AT STA 1155 TO 1250, LBL 22 INCHES. NEW TRACK FABRICATED FROM EXTRUSION AND INSTALLED FROM STA 1136 TO 1309, PER SPM 6-70-01.
- [SDR ZW0A0100814](https://openairdocs.org/sdr/ZW0A0100814.md): Attach Angle · cracked · Apr 25, 2001 · N904TW · Doug DC982 · Vertical Stabilizer
  > DURING CHECK-C MAINT THE DORSAL FIN ATTACH ANGLE WAS CRACKED ON LT SIDE, STA 1405 TO 1427. REPLACED ATTACH ANGLE WITH NEW. INSTALLED RIVETS PER SRM 51-30-2.
- [SDR ZW0A0100813](https://openairdocs.org/sdr/ZW0A0100813.md): Cargo Track · corroded · Apr 25, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND CORROSION ON LT CARGO TRACK AT STA 1155 TO 1218. INSTALLED NEW TRACK AND INSTALLED FASTENERS PER SRM 51-30 FROM STA 1010 TO STA 1218, AND SRM 53-05 FIG 4.
- [SDR ZW0A0100812](https://openairdocs.org/sdr/ZW0A0100812.md): Floor Support · corroded · Apr 25, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND FLOOR ATTACH ANGLE CORRODED AT STA 351 TO 446, RBL 8. REPLACED FLOOR SUPPORT WITH NEW PER DRAWING 5936587. REPLACED BOLTS, NUTS AND WASHERS PER SRM 51-30-1. REINSTALLED RIVETS PER SRM 51-30-2.
- [SDR ZW0A0100811](https://openairdocs.org/sdr/ZW0A0100811.md): Frame · corroded · Apr 25, 2001 · N904TW · Doug DC982 · Fuselage Main, Frame
  > DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON FORMER AT STA 1231, LONGERON 27L TO 28L. REMOVED CORRODED FORMER AND SPLICED NEW PER SRM 53-03, FIG 2A.
- [SDR ZW0A0100810](https://openairdocs.org/sdr/ZW0A0100810.md): Seat Track · corroded · Apr 25, 2001 · N904TW · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT FOUND NUMBER 3 CABIN FLOOR TRACK WITH CORROSION ON FLANGE BETWEEN STA 1231 AND 1271. NEW TRACK FABRICATED FROM EXTRUSION AND INSTALLED FROM STA 1136 TO 1309 PER SPM 6-70-01.
- [SDR ZW0A0100824](https://openairdocs.org/sdr/ZW0A0100824.md): Angle · corroded · Apr 24, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT AT STA 1155 AND LONGERON 28R, BOTTOM OF CARGO DOOR JAM, FOUND ANGLE HAD CORROSION. INSTALLED NEW ANGLE PER SPM 6-70-01.
- [SDR ZW0A0100823](https://openairdocs.org/sdr/ZW0A0100823.md): Angle · corroded · Apr 23, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE AFT CARGO COMPT, AT STA 1211 AND LONGERON 28R, BOTTOM OF CARGO DOOR JAMB, FOUND ANGLE HAD CORROSION. INSTALLED NEW ANGLE PER SPM 6-70-01.
- [SDR ZW0A0100827](https://openairdocs.org/sdr/ZW0A0100827.md): Skin · dented · Apr 22, 2001 · N904TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT ON LT FUSELAGE SKIN FOUND DENT 2 IN BY 3 IN BY 0.125 INCHES AT STA 230, BETWEEN LONGERON 17L AND 18L. CUT OUT DAMAGED AREA AND REPAIRED BY INSTALLING DOUBLERS AND NEW SKIN PER SRM 53-04, FIG 12C.
- [SDR ZW0A0100822](https://openairdocs.org/sdr/ZW0A0100822.md): Support · cracked · Apr 22, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT ON THE AFTER BODY FOUND A CRACK AND INTERIM REPAIR IN RT CANTED WEB VENT BOX SUPPORT, STA 1465. FABRICATED NEW SUPPORT PER DRAWING 520923 AND INSTALLED PER SRM 51-30. TREATED PARTS PER SRM 51-10-3.
- [SDR ZW0A0100833](https://openairdocs.org/sdr/ZW0A0100833.md): Floor Support · corroded · Apr 20, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN FWD CABIN FOUND FLOOR AT STA 218, BL 0, HAD CORROSION. REMOVED CORRODED SUPPORT AND REPLACED WITH SERVICEABLE SUPPORT. INSTALLED WITH SAME TYPE FASTENERS AND TREATED PER SRM 51-10-3.
- [SDR ZW0A0100832](https://openairdocs.org/sdr/ZW0A0100832.md): Clip · cracked · Apr 20, 2001 · N904TW · Doug DC982 · Wing Miscellaneous Structure
  > DURING CHECK-C MAINT ON RT WING THE RIB JUST INBD OF JACKPAD HAD A 2 INCH CRACK IN ATTACH CLIP. REPAIRED PER SERVICE BULLETIN 57-170.
- [SDR ZW0A0100831](https://openairdocs.org/sdr/ZW0A0100831.md): Skin · cracked · Apr 20, 2001 · N904TW · Doug DC982 · Wing, Plate/Skin
  > DURING CHECK-C MAINT RT WING L/E SKIN HAD TEMPORARY REPAIR FOR SKIN CRACKS. INSTALLED PERMANENT REPAIR PER SERVICE BULLETIN 57-170.
- [SDR ZW0A0100830](https://openairdocs.org/sdr/ZW0A0100830.md): Clip · cracked · Apr 20, 2001 · N904TW · Doug DC982 · Wing, Rib/Bulkhead
  > DURING CHECK-C MAINT ON RT WING L/E RIB JUST FWD OF JACKPAD HAD A 2 INCH CRACK IN ATTACH CLIP. REPAIRED PER SERVICE BULLETIN 57-10.
- [SDR ZW0A0100829](https://openairdocs.org/sdr/ZW0A0100829.md): Rib · chipped · Apr 20, 2001 · N904TW · Doug DC982 · Wing, Rib/Bulkhead
  > DURING CHECK-C MAINT ON RT WING L/E THE AFT LOWER END OF RIB HAD METAL CHIP MISSING, JUST OTBD OF JACKPAD. INSTALLED DOUBLER PER SERVICE BULLETIN ENG TASK 57-10.
- [SDR ZW0A0100828](https://openairdocs.org/sdr/ZW0A0100828.md): Rib · cracked · Apr 20, 2001 · N904TW · Doug DC982 · Wing, Rib/Bulkhead
  > DURING CHECK-C MAINT ON RT WING THE L/E RIB JUST INBOARD OF JACK PAD HAD 1 INCH CRACK ON LOWER FWD END. INSTALLED DOUBLER PER SERVICE BULLETIN 57-10.
- [SDR ZW0A0100704](https://openairdocs.org/sdr/ZW0A0100704.md): Floor Support · corroded · Apr 20, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 1155, LONGERON 30 TO 29R. REPLACED FLOOR SUPPORT PER SPM 6-70-01.
- [SDR ZW0A0100708](https://openairdocs.org/sdr/ZW0A0100708.md): Skin · corroded · Apr 19, 2001 · N904TW · Doug DC982 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT IN THE AFT ACCY COMPT, FOUND CORROSION AND RUSTED FASTENERS BETWEEN SKIN AND FORMERS AT STA 1437, BETWEEN LONGERON 19R AND 17R. REMOVED CORROSION PER SRM 51-10-3 AND SPM 6-80-01. INSTALLED DOUBLER REPAIR PER SRM 53-01, PAGE 9 FIG 2.
- [SDR ZW0A0100707](https://openairdocs.org/sdr/ZW0A0100707.md): Web · cracked · Apr 19, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND A 1.5 INCH CRACK IN WEBBING AT STA 1266, LONGERON 18L, ONE INCH OTBD OF NUMBER 1 CHAIR TRACK. INSTALLED WEB DOUBLER PER SRM 53-01, FIG 2 AND SRM 51-30-2.
- [SDR ZW0A0100706](https://openairdocs.org/sdr/ZW0A0100706.md): Attach Angle · cracked · Apr 19, 2001 · N904TW · Doug DC982 · Fuselage, Stabilizer Attach Fittings
  > DURING CHECK-C MAINT FOUND VERTICAL STABILIZER RT SIDE OF DORSAL FIN, AFT END OF VERTICAL STAB TO FUSELAGE ATTACH ANGLE, AFT OF PREVIOUS REPAIR HAD ANGLE WITH A 2 INCH CRACK. TRIMMED OFF BROKEN PART. MADE FILLER AND DOUBLER PER SRM 53-05, FIG 23A, AND INSTAL
- [SDR ZW0A0100705](https://openairdocs.org/sdr/ZW0A0100705.md): Floorbeam · corroded · Apr 19, 2001 · N904TW · Doug DC982 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINT FOUND CABIN FLOOR BEAM, LT SIDE OF TOP CAP, WAS CORRODED OUT AT STA 1250. REMOVED SUPPORT ANGLE AND FABRICATED NEW AND INSTALLED WITH HI-LOKS PER SPM 6-70-01.
- [SDR ZW0A0100504](https://openairdocs.org/sdr/ZW0A0100504.md): Floor Support · corroded · Apr 18, 2001 · N904TW · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT IN THE FWD CABIN FOUND FLOOR SUPPORT WITH CORROSION BETWEEN STA 160 AND 200, LBL 54 INCHES. REMOVED CORRODED FLOOR SUPPORT. MADE NEW OUT OF SAME MATERIAL PER SPM 6-78-01. RE-INSTALLED WITH SEALER PER SRM 51-30-2.
- [SDR TWAA0101001](https://openairdocs.org/sdr/TWAA0101001.md): O-Ring · worn · Jan 16, 2001 · N904TW · Doug DC982 · Landing Gear Brake System
  > IN DESCENT INTO SAT THE RT HYDRAULIC QUANTITY WENT TO ZERO. IT WAS NECESSARY TO MANUALLY EXTEND THE LANDING GEAR, AND TO BE TOWED OFF THE RUNWAY AFTER LANDING. REPLACED THE O-RING ON THE RT HYDRAULIC BRAKE PRESSURE MANIFOLD PLUG PORT DUE TO LEAKING HYDRAULIC
- [SDR TWAA0016601](https://openairdocs.org/sdr/TWAA0016601.md): Battery · discharged · Oct 25, 2000 · N904TW · Doug DC982 · Emergency Lighting
  > THE OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPLACED TWO BATTERIES. CHECK-C 3-20-00 STL.
- [SDR TWAA0013201](https://openairdocs.org/sdr/TWAA0013201.md): Control Valve · failed · Aug 22, 2000 · N904TW · Doug DC982 · Landing Gear Door Retract Section
  > THE NOSE LANDING GEAR DID NOT EXTEND WITH NORMAL GEAR EXTENSION. MANUAL EXTENSION WAS USED. FOUND NOSE LANDING GEAR WAS SLOW TO OPERATE. REPLACED THE NLG RETRACT CYL (P/N 3928137-5001), THE LANDING GEAR CONTROL VALVE (P/N 5916460-5509), AND THE RT HYD RESER
- [SDR TWAA9904101](https://openairdocs.org/sdr/TWAA9904101.md): Bulb · loose · Mar 17, 1999 · N904TW · Doug DC982 · Emergency Lighting
  > THE EMERGENCY LIGHT IN THE TAIL COMPT THAT SHINES ON HANDLE WAS INOPERATIVE. REPOSITIONED AND SECURED THE BULB. CHECK-C 2-26-99 MCI.
- [SDR TWAA9813902](https://openairdocs.org/sdr/TWAA9813902.md): Bulb · loose · Aug 27, 1998 · N904TW · Doug DC982 · Passenger Compartment Lighting
  > FLIGHT ATTENDANT RECEIVED AN ELECTRICAL SHOCK WHEN TOUCHING A FLOURSCENT LIGHT IN THE FORWARD GALLEY. THE LIGHT FIXTURE END CAP HAD OPENED AND THE BULB SLIPPED PARTIALLY OUT. REINSERTED BULB AND SECURED THE CAP. CHECK-C 4-1-98 STL.
- [SDR TWAA9808205](https://openairdocs.org/sdr/TWAA9808205.md): Sensor · malfunctioned · May 24, 1998 · N904TW · Doug DC982 · Landing Gear Position and Warning
  > STL - FLT 649 - AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR AND DOOR LIGHT REMAINED ON. CYCLED GEAR AND LIGHTS WENT OUT. ADJUSTED LEFT MAIN LANDING GEAR DOOR POSITION SENSOR TARGET MFG P/N 3939674-1. (M)
- [SDR TWAA9807404](https://openairdocs.org/sdr/TWAA9807404.md): Coffeemaker · shorted · May 10, 1998 · N904TW · Doug DC982 · Buffet/Galleys
  > STL - FLT 315 - NR 3 COFFEEMAKER CIRCUIT BREAKER POPPED. CREW RESET CB AND SPARKS WERE PRESENT AT THE COFFEEMAKER AND CB POPPED AGAIN. CREW LEFT CB POPPED. REPLACED COFFEEMAKER. CHECK-C 4-1-98 STL. (M)
- [SDR TWAA9805002](https://openairdocs.org/sdr/TWAA9805002.md): Retract Cyl · worn · Apr 1, 1998 · N904TW · Doug DC982 · Landing Gear Retraction/Extension System
  > STL - FLT 714 - AFTER CHECK-C MAINTENANCE FLT 714 RETURNED TO STL DUE TO NOSE GEAR DOOR UNSAFE LIGHT ON WITH GEAR RETRACTED. FOUND LOWER BUNGEE BOLT FOR NOSE GEAR TOO LONG MFG NAS1106-23D. HIT STRUCTURE AT DOUBLER. INSTALLED SHORTER BOLT. AIRCRAFT OPERATED

Next page: https://openairdocs.org/deregistered/N904TW-2013-08-16/reports.md?page=2

## 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 = 'N904TW' AND deregistration_id = 'N904TW-2013-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N904TW-2013-08-16/reports

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