# N908TW: 1983 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2013-04-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 29, 2013 - Status when cancelled: Sale reported, pending cancellation - 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: 49169 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 15, 1983 - Last registry action: May 31, 2006 - Mode S code: AC8EA2 - 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/N908TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=908TW - Page: https://openairdocs.org/deregistered/N908TW-2013-04-29 From the FAA registry file of November 5, 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 (70, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0206701](https://openairdocs.org/sdr/ZW0A0206701), Jun 21, 2002: LONGERON. DAMAGED. LONGERON 24L WAS DAMAGED AT STA 325. REPAIRED LONGERON 24L PER SRM 53-02, FIG 18. - [SDR ZW0A0201703](https://openairdocs.org/sdr/ZW0A0201703), Feb 6, 2002: LONGERON. CRACKED. DURING CHECK-C MAINTENANCE LONGERON 2R WAS FOUND CRACKED AT TAPERED END AFT OF STA 1418. A ONE INCH CRACK. REMOVED, FABRICATED, AND INSTALLED LONGERON PER SRM 5 - [SDR ZW0A0101303](https://openairdocs.org/sdr/ZW0A0101303), Apr 16, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE MID CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED AT STA 598 TO 680. INSTALLED NEW TRACK PER 53-05, FIG 4. - [SDR ZW0A0100109](https://openairdocs.org/sdr/ZW0A0100109), Apr 8, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON AFT RT CARGO TIE DOWN TRACK. INSTALLED NEW TRACK PER SPM 6-70-01, ITEM 4. INSTALLED NEW FASTENERS - [SDR TWAA0106310](https://openairdocs.org/sdr/TWAA0106310), Apr 5, 2001: FRAME. CORRODED. DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND FRAME AT STA 1309 WAS CORRODED FRONT AND BACK BETWEEN LONGERON 28R TO 28L. SPLICED FRAME REPAIR PER SRM 53-03, FIG - [SDR TWAA0106312](https://openairdocs.org/sdr/TWAA0106312), Apr 4, 2001: WEB. CORRODED. DURING OP 16 MAINT CHECK IN FWD CABIN FOUND CORROSION ON FLOOR MEMBRANE AT STA 200, RBL 45 TO 55. FABRICATED MEMBRANE STA 200, RBL 45 IN TO 55 IN PER SRM 53-14- - [SDR TWAA0106311](https://openairdocs.org/sdr/TWAA0106311), Apr 4, 2001: ATTACH ANGLE. CORRODED. DURING CHECK-C MAINT FOUND FRAME ATTACH ANGLE CORRODED AT FWD SIDE STA 1309, BETWEEN LONGERON 29L AND 29R. REPLACED FRAME ATTACH ANGLE PER SRM 53-03, FIG 3. - [SDR TWAA0106308](https://openairdocs.org/sdr/TWAA0106308), Apr 4, 2001: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT FOUND INTERCOSTAL CORRODED OTBD OF STA 1322, STRINGER 28L. FORMED NEW INTERCOSTAL PER SPM 6-70-01. INSTALLED PER SRM 51-30-5, 51-30-7, 51-1 - [SDR TWAA0106307](https://openairdocs.org/sdr/TWAA0106307), Apr 3, 2001: DOOR FRAME. CORRODED. DURING CHECK-C MAINT IN FWD CARGO COMPT FOUND CORROSION ON FWD CARGO DOOR LOWER JAMB. REMOVED LOWER FWD CARGO DOOR FLOOR PAN AND INSTALLED FLOOR PAN WITH HI-LOK - [SDR TWAA0106223](https://openairdocs.org/sdr/TWAA0106223), Apr 3, 2001: WEB. CORRODED. DURING CHECK-C MAINT ON THE FWD ENTRY DOOR, CORROSION WAS FOUND ON MEMBRANE AFT SIDE OF STA 160, LONGERON 18L. UT INSP INDICATES 40 PER CENT MATERIAL LOSS. REPA - [SDR TWAA0106205](https://openairdocs.org/sdr/TWAA0106205), Apr 2, 2001: SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND ON COCKPIT RT SIDE, BETWEEN STA 120 TO 148 AND 51 INCH RBL, FLOOR/WALL SUPPORT HAD CORROSION. MADE NEW ANGLE USING 0.040 7075T6. TRIM - [SDR TWAA0106204](https://openairdocs.org/sdr/TWAA0106204), Apr 2, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT LBL 4, STA 180 TO 200. REPLACED FLOOR SUPPORT PER SRM 51-10-4, SRM 51-30-1, AND SPM 6-70-1. - [SDR ZW0A0100108](https://openairdocs.org/sdr/ZW0A0100108), Mar 30, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND IN LT CABIN BETWEEN STA 160 AND 200, 6 INCHES INBD OF FWD PASSENGER ENTRY, FLOOR MEMBRANE HAD CORROSION. REPLACED DAMAGED CORRODED PA - [SDR TWAA0106309](https://openairdocs.org/sdr/TWAA0106309), Mar 30, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND IN CABIN AT STA 160, 42 IN LBL, FLOOR SUPPORT HAD CORROSION. REPLACED FLOOR SUPPORT PER SRM 51-70-0. - [SDR TWAA0106203](https://openairdocs.org/sdr/TWAA0106203), Mar 30, 2001: WEB. CRACKED. DURING CHECK-C MAINT FOUND IN CABIN AT FWD PASSENGER ENTRY AT STA 200, 8 IN INBD, MEMBRANE HAD A 1 INCH CRACK. REPLACED WITH NEW MEMBRANE WHERE AREA WAS CRACKED - [SDR TWAA0106222](https://openairdocs.org/sdr/TWAA0106222), Mar 30, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT BETWEEN STA 160 AND 200, 6 INCHES INBD OF PASSENGER FWD ENTRY, HAD CORROSION ON FLANGE TOP AND BOTTOM. FABRICATED - [SDR TWAA0106221](https://openairdocs.org/sdr/TWAA0106221), Mar 30, 2001: WEB. CORRODED. DURING CHECK-C MAINT IN THE FWD CABIN FOUND CORROSION BELOW GALLEY DRAIN STA 148 TO 160, RBL 44 TO RBL 54. REMOVED CORRODED MEMBRANE. FABRICATED NEW MEMBRANE PE - [SDR TWAA0106220](https://openairdocs.org/sdr/TWAA0106220), Mar 30, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND RT COCKPIT FLOOR AREA BETWEEN STA 133 TO 160, AND 26 IN RBL, MEMBRANE HAD CORROSION. REMOVED CORROSION THEN FABRICATED NEW WEB PER IP - [SDR TWAA0106106](https://openairdocs.org/sdr/TWAA0106106), Mar 30, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND CABIN MEMBRANE 7 INCHES INBD OF FWD PASSENGER ENTRY AND 11 INCHES FWD OF STA 200, HAD CORROSION. REPLACED CORROSION AREA PER SRM 51-7 - [SDR TWAA0105809](https://openairdocs.org/sdr/TWAA0105809), Mar 30, 2001: FLOOR SUPPORT. BROKEN. DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE FLOOR SUPPORT WAS BROKEN AND CORRODED BETWEEN STA 1155 AND 1147, BETWEEN LONGERON 29R AND 30R. REMOVED OLD PART - [SDR TWAA0105808](https://openairdocs.org/sdr/TWAA0105808), Mar 30, 2001: FITTING. CORRODED. DURING CHECK-C MAINT IN THE FWD CABIN THE RT GALLEY HOLD DOWN WAS CORRODED AT STA 160, RBL 45. REPLACED CASTING PER SRM 51-10-4 AND SPM 06-70-01. - [SDR TWAA0105807](https://openairdocs.org/sdr/TWAA0105807), Mar 30, 2001: FITTING. CORRODED. DURING CHECK-C MAINT IN THE FWD CABIN, THE RT GALLEY HOLD DOWN WAS CORRODED AT STA 160, RBL 51. REPLACED CASTING PER SRM 51-10-4 AND SPM 06-70-01. - [SDR TWAA0105806](https://openairdocs.org/sdr/TWAA0105806), Mar 29, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CABIN CORROSION WAS FOUND ON NUMBER 2 FLOOR TRACK, FROM STA 1136 TO 1307. CLEANED CORROSION PER SPM 6-80-01 AND SRM 53-05. TREAT - [SDR TWAA0105606](https://openairdocs.org/sdr/TWAA0105606), Mar 27, 2001: WEB. CORRODED. DURING CHECK-C MAINT IN THE AFT CABIN FOUND CORROSION AND CRACKS IN MEMBRANE AT STA 1174 TO 1250, LBL 45 INCHES. REMOVED CORROSION AND DAMAGED AREA. MADE DOUBLE - [SDR TWAA0105512](https://openairdocs.org/sdr/TWAA0105512), Mar 26, 2001: BRACE. CORRODED. DURING CHECK-C MAINT IN MID CARGO COMPT, FOUND CORROSION ON CORNER BRACE AT STA 693, RBL 7 IN. REPLACED BRACE PER SRM 51-30-5. - [SDR TWAA0105511](https://openairdocs.org/sdr/TWAA0105511), Mar 26, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 200, LBL 4 TO RBL 4. REPLACED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 53-14-1. - [SDR TWAA0105412](https://openairdocs.org/sdr/TWAA0105412), Mar 23, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT NUMBER 5 CABIN FLOOR TRACK WAS CORRODED AT STA 237. REPLACED TRACK FROM STA 200 TO 247, PER SRM 53-05 FIG 4. - [SDR TWAA0105411](https://openairdocs.org/sdr/TWAA0105411), Mar 23, 2001: WEB. CRACKED. DURING CHECK-C MAINT FOUND CABIN MEMBRANE CRACKED AT STA 253 TO 275, RBL 54 INCHES. REPAIRED CRACKED MEMBRANE PER SRM 53-01, FIG 4 SHEET 3. INSTALLED RIVETS PER - [SDR TWAA0105410](https://openairdocs.org/sdr/TWAA0105410), Mar 22, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT RBL 8 TO RBL 45, STA 200. FABRICATED AND INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 53-14-1, 51-30 - [SDR TWAA0105409](https://openairdocs.org/sdr/TWAA0105409), Mar 22, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN THE AFT LAV AREA, THE CABIN FLOOR SUPPORT WAS CORRODED, STA 1307, LBL 18 INCHES. INSTALLED NEW FLOOR SUPPORT PER SRM 51-30-1. - [SDR TWAA0105408](https://openairdocs.org/sdr/TWAA0105408), Mar 22, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CABIN SEAT TRACK NUMBER 6 HAD CORROSION BETWEEN STA 389 AND 769. REPLACED TRACK SECTIONS. SPLICED PER SRM 53-05, FIG 4D. - [SDR TWAA0105407](https://openairdocs.org/sdr/TWAA0105407), Mar 21, 2001: DOOR. CRACKED. DURING CHECK-C MAINT FOUND RT MAIN WHEEL WELL DOOR, FWD INBD CORNER OF THE DOOR CRACKED. INSTALLED DOUBLER PER SRM 52-05, FIG 28. - [SDR TWAA0105406](https://openairdocs.org/sdr/TWAA0105406), Mar 21, 2001: WEB. CRACKED. DURING CHECK-C MAINT FOUND CABIN FLOOR MEMBRANE CRACKED AT STA 332 TO 351, RBL 54 INCHES. INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4. INSTALLED FORMER RING FI - [SDR TWAA0105405](https://openairdocs.org/sdr/TWAA0105405), Mar 21, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT RBL 8, STA 180 TO 200. REMOVED FLOOR SUPPORT AND FABRICATED NEW PER SRM 53-14-01, FIG 11 SHEET 1. TREAT - [SDR TWAA0105204](https://openairdocs.org/sdr/TWAA0105204), Mar 20, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT IN AFT CABIN FOUND CORROSION ON CHAIR TRACK AT SEVERAL PLACES, STA 1003 TO 1146. INSTALLED NEW TRACK PER INSTALLATION PRINT 5930566. TREATE - [SDR TWAA0105203](https://openairdocs.org/sdr/TWAA0105203), Mar 20, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CABIN FLOOR TRACK NUMBER 4, BETWEEN STA 200 AND 256, HAD CORROSION ON TOP AND BOTTOM OF FLANGE SURFACE. REMOVED OLD TRACK AND INSTALL - [SDR TWAA0105103](https://openairdocs.org/sdr/TWAA0105103), Mar 19, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AND BROKEN AT STA 180, RBL 9 IN TO RBL 44 INCHES. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30. - [SDR TWAA0105102](https://openairdocs.org/sdr/TWAA0105102), Mar 16, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 160 TO 200, RBL 44. REPLACED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2. - [SDR TWAA0104916](https://openairdocs.org/sdr/TWAA0104916), Mar 15, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINTENANCE FOUND CABIN FLOOR TRACK NUMBER 2, RBL 22, WAS CORRODED TOP AND BOTTOM AT STA 1136 TO 1307. REMOVED 16 FT LENGTH OF TRACK AND REPLACED - [SDR TWAA0104915](https://openairdocs.org/sdr/TWAA0104915), Mar 15, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINTENANCE FOUND CORROSION ON CHAIR TRACK 2 1/2 L AT STA 1117 TO 1136. REPLACED PART WITH NEW AND INSTALLED. - [SDR ZW0A0101106](https://openairdocs.org/sdr/ZW0A0101106), Mar 14, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN THE AFT CABIN THE FLOOR SUPPORT STRUCTURE WAS CORRODED AT STA 1250, LBL 23 TO RBL 43. REMOVED CORRODED SUPPORT AND REPLACED WITH NEW AND - [SDR TWAA0104909](https://openairdocs.org/sdr/TWAA0104909), Mar 14, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN AFT CABIN FOUND FLOOR SUPPORT STRUCTURE CORRODED AT STA 1250, LBL 23 AND RBL 43. REMOVED CORRODED SUPPORT AND REPLACED WITH NEW PART. IN - [SDR TWAA0105004](https://openairdocs.org/sdr/TWAA0105004), Mar 12, 2001: FITTING. CRACKED. DURING CHECK-C MAINT FOUND FAIRING SUPPORT STRUCTURE BRACKET WAS CRACKED AT CENTER OF KEEL BEAM, STA 875. REPLACED CRACKED TEE FITTING WITH NEW PER SPM 6-70-01, - [SDR TWAA0105005](https://openairdocs.org/sdr/TWAA0105005), Mar 9, 2001: SKIN. DAMAGED. DURING CHECK-C MAINT FOUND STATIC BURNS AT STA 61, 20 INCHES BELOW LONGERON 18R. CUT OUT AND INSTALLED DOUBLER REPAIR PER SRM 53-04, PAGE 18. - [SDR TWAA0103303](https://openairdocs.org/sdr/TWAA0103303), Feb 20, 2001: BATTERY PACK. DISCHARGED. THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 1 THRU 5, THE FWD GALLEY EXIT SIGN, AND ROW 19 AND 20 EGRESS LIGHTS. REMOVED MOISTURE FROM CONNECTORS FOR FWD CABIN - [SDR TWAA0012903](https://openairdocs.org/sdr/TWAA0012903), Aug 18, 2000: LANYARD. DISCONNECTED. ON THE LEFT SIDE MOST FORWARD CABIN DOOR, THE ESCAPE SLIDE LANYARD DISCONNECTED FROM THE SLIDE. RECONNECTED THE LANYARD. CHECK-C 2-12-00 STL. - [SDR TWAA0012702](https://openairdocs.org/sdr/TWAA0012702), Aug 15, 2000: LIGHT. INOPERATIVE. THE FIRST CLASS EMERGENCY EGRESS LIGHTS WERE INOPERATIVE. REPLACED ONE LUMINSCENT STRIP LIGHT AND REMOVED WATER FROM THE EGRESS TRACK SECTION. CHECK-C 2-12-00 S - [SDR TWAA0010003](https://openairdocs.org/sdr/TWAA0010003), Jun 25, 2000: LIGHT. INOPERATIVE. THE EGRESS LIGHTS WERE INOPERATIVE AT THE FWD GALLEY AND ALL OF THE FIRST CLASS SEATS. FOUND LIGHTS WET. REMOVED AND DRIED THE LAMPS AND ALL CONNECTIONS. CHECK- - [SDR TWAA0003601](https://openairdocs.org/sdr/TWAA0003601), Mar 5, 2000: COALESCER BAG. CONTAMINATED. WHITE SMOKE IN COCKPIT ON CLIMB-OUT. REPLACE LEFT PAC COALESCER BAG CONTAMINATED WITH OIL. PLACCARDED APU INOP. AC05 12-21-99 DFW. - [SDR TWAA9914701](https://openairdocs.org/sdr/TWAA9914701), Oct 30, 1999: COALESCER BAG. DIRTY. PRIOR TO DEPARTURE FLT CREW REPORTED SMOKEY SMELL IN CABIN. CHANGED WATER SEPARATOR BAGS AND PERFORMED PACK BURN OUT. All 70: https://openairdocs.org/deregistered/N908TW-2013-04-29/reports.md ## FAA accident and incident reports (1) 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 19880815047289I](https://openairdocs.org/incident/19880815047289I), Aug 15, 1988: Doug DC982 (N908TW), St Louis, MO. Departed with b fire sensor placarded inoperative. A fire warning came on after takeoff. Returned. Landed ok. ## Other aircraft with N908TW - [Registered now](https://openairdocs.org/aircraft/N908TW): Head Balloons AX7-77, S/N 501, built 2022 --- 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.