# N904TW: 1983 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2013-08-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 16, 2013
- Status when cancelled: Sale reported, canceled
- Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 49156
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 16, 1983
- Last registry action: May 31, 2006
- Mode S code: AC7FC6
- Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City)
- Owner type: Individual
- Owner's area on the map: 39.1483° N, 94.6051° W: Placed by OpenAirDocs at the center of ZIP code 66115, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N904TW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=904TW
- Page: https://openairdocs.org/deregistered/N904TW-2013-08-16

From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md

## Service difficulty reports (87, newest 50)

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

- [SDR ZW0A0105401](https://openairdocs.org/sdr/ZW0A0105401), Jul 19, 2001: O-RING. 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. RE
- [SDR ZW0A0104003](https://openairdocs.org/sdr/ZW0A0104003), Jun 22, 2001: BATTERY PACK. 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), Jun 8, 2001: POWER SUPPLY. DISCHARGED. THE EGRESS LIGHTS CAME ON INTERMITTENTLY IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 5-18-2001.
- [SDR ZW0A0101801](https://openairdocs.org/sdr/ZW0A0101801), May 8, 2001: SEAT TRACK. CORRODED. 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), May 4, 2001: SEAT TRACK. CORRODED. 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, 5
- [SDR ZW0A0101205](https://openairdocs.org/sdr/ZW0A0101205), May 4, 2001: WEB. CORRODED. 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), May 3, 2001: WEB. CRACKED. 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 MEMB
- [SDR ZW0A0101112](https://openairdocs.org/sdr/ZW0A0101112), May 2, 2001: WEB. CORRODED. 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), May 2, 2001: SEAT TRACK. CORRODED. 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), May 2, 2001: FLOOR SUPPORT. CORRODED. 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. INSTA
- [SDR ZW0A0101109](https://openairdocs.org/sdr/ZW0A0101109), May 2, 2001: FLOOR SUPPORT. CORRODED. 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), May 1, 2001: WEB. CORRODED. 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, 
- [SDR ZW0A0101107](https://openairdocs.org/sdr/ZW0A0101107), May 1, 2001: SEAT TRACK. CORRODED. 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
- [SDR ZW0A0101306](https://openairdocs.org/sdr/ZW0A0101306), Apr 30, 2001: CARGO TRACK. CORRODED. 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), Apr 30, 2001: FAIRING. DAMAGED. 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 1
- [SDR ZW0A0101003](https://openairdocs.org/sdr/ZW0A0101003), Apr 30, 2001: SEAT TRACK. CORRODED. 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. SPL
- [SDR ZW0A0101002](https://openairdocs.org/sdr/ZW0A0101002), Apr 27, 2001: INTERCOSTAL. CORRODED. 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. REINSTALLE
- [SDR ZW0A0101001](https://openairdocs.org/sdr/ZW0A0101001), Apr 27, 2001: SEAT TRACK. CORRODED. 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), Apr 26, 2001: SEAT TRACK. CORRODED. 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 EXTRU
- [SDR ZW0A0100826](https://openairdocs.org/sdr/ZW0A0100826), Apr 25, 2001: FLOORBEAM. CORRODED. 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 W
- [SDR ZW0A0100825](https://openairdocs.org/sdr/ZW0A0100825), Apr 25, 2001: SEAT TRACK. CORRODED. 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 130
- [SDR ZW0A0100814](https://openairdocs.org/sdr/ZW0A0100814), Apr 25, 2001: ATTACH ANGLE. CRACKED. 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), Apr 25, 2001: CARGO TRACK. CORRODED. 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,
- [SDR ZW0A0100812](https://openairdocs.org/sdr/ZW0A0100812), Apr 25, 2001: FLOOR SUPPORT. CORRODED. 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 W
- [SDR ZW0A0100811](https://openairdocs.org/sdr/ZW0A0100811), Apr 25, 2001: FRAME. CORRODED. 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 2
- [SDR ZW0A0100810](https://openairdocs.org/sdr/ZW0A0100810), Apr 25, 2001: SEAT TRACK. CORRODED. 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
- [SDR ZW0A0100824](https://openairdocs.org/sdr/ZW0A0100824), Apr 24, 2001: ANGLE. CORRODED. 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), Apr 23, 2001: ANGLE. CORRODED. 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 6-7
- [SDR ZW0A0100827](https://openairdocs.org/sdr/ZW0A0100827), Apr 22, 2001: SKIN. DENTED. 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 
- [SDR ZW0A0100822](https://openairdocs.org/sdr/ZW0A0100822), Apr 22, 2001: SUPPORT. CRACKED. 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 A
- [SDR ZW0A0100833](https://openairdocs.org/sdr/ZW0A0100833), Apr 20, 2001: FLOOR SUPPORT. CORRODED. 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 SA
- [SDR ZW0A0100832](https://openairdocs.org/sdr/ZW0A0100832), Apr 20, 2001: CLIP. CRACKED. 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), Apr 20, 2001: SKIN. CRACKED. 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), Apr 20, 2001: CLIP. CRACKED. 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), Apr 20, 2001: RIB. CHIPPED. 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), Apr 20, 2001: RIB. CRACKED. 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), Apr 20, 2001: FLOOR SUPPORT. CORRODED. 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), Apr 19, 2001: SKIN. CORRODED. 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 COR
- [SDR ZW0A0100707](https://openairdocs.org/sdr/ZW0A0100707), Apr 19, 2001: WEB. CRACKED. 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, FI
- [SDR ZW0A0100706](https://openairdocs.org/sdr/ZW0A0100706), Apr 19, 2001: ATTACH ANGLE. CRACKED. 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
- [SDR ZW0A0100705](https://openairdocs.org/sdr/ZW0A0100705), Apr 19, 2001: FLOORBEAM. CORRODED. 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-LO
- [SDR ZW0A0100504](https://openairdocs.org/sdr/ZW0A0100504), Apr 18, 2001: FLOOR SUPPORT. CORRODED. 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
- [SDR TWAA0101001](https://openairdocs.org/sdr/TWAA0101001), Jan 16, 2001: O-RING. WORN. 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. 
- [SDR TWAA0016601](https://openairdocs.org/sdr/TWAA0016601), Oct 25, 2000: BATTERY. DISCHARGED. 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), Aug 22, 2000: CONTROL VALVE. FAILED. 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 RETRAC
- [SDR TWAA9904101](https://openairdocs.org/sdr/TWAA9904101), Mar 17, 1999: BULB. LOOSE. 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), Aug 27, 1998: BULB. LOOSE. 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 
- [SDR TWAA9808205](https://openairdocs.org/sdr/TWAA9808205), May 24, 1998: SENSOR. MALFUNCTIONED. 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 POSI
- [SDR TWAA9807404](https://openairdocs.org/sdr/TWAA9807404), May 10, 1998: COFFEEMAKER. SHORTED. 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. REPL
- [SDR TWAA9805002](https://openairdocs.org/sdr/TWAA9805002), Apr 1, 1998: RETRACT CYL. WORN. 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 GE

All 87: https://openairdocs.org/deregistered/N904TW-2013-08-16/reports.md

## FAA accident and incident reports (5)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19970611022899I](https://openairdocs.org/incident/19970611022899I), Jun 11, 1997: Doug DC982 (N904TW), Portland, OR. On takeoff left csd oil light on. Aborted. Taxied to gate. No oil. Refilled departed. Reverser acc light came on.
- [Incident 19950206005609I](https://openairdocs.org/incident/19950206005609I), Feb 6, 1995: Doug DC982 (N904TW), Kansas City, MO. Narrative: during takeoff, rt. Engine, s/n 3257, failed at approximately 2600 ft. MSL. Aircraft returned to mci with rt. Engine shut down and landed without…
- [Incident 19880607038879I](https://openairdocs.org/incident/19880607038879I), Jun 7, 1988: Doug DC982 (N904TW), St Louis, MO, Minor damage. Upon landing the aft cone fell off. Maintenance replaced tail cone evac slide and container.
- [Incident 19880211009049I](https://openairdocs.org/incident/19880211009049I), Feb 11, 1988: Doug DC982 (N904TW), St Louis, MO. On takeoff with engine anti icing on. Ice protection temperature low came on. Changed aticipator and theromostat.
- [Incident 19870827056839I](https://openairdocs.org/incident/19870827056839I), Aug 27, 1987: Doug DC982 (N904TW), St Louis, MO. Unable to retract the nose gear after takeoff. Returned safely. Found nose strut flat. Replaced inflation valve.

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