# N906TW: 1983 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2008-07-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 7, 2008 - Status when cancelled: Valid registration - 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: 49160 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 9, 1983 - Certificate issued: March 24, 2006 - Last registry action: March 24, 2006 - Mode S code: AC8734 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N906TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=906TW - Page: https://openairdocs.org/deregistered/N906TW-2008-07-07 From the FAA registry file of October 29, 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 (102, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0101102](https://openairdocs.org/sdr/ZW0A0101102), Apr 26, 2001: ANGLE. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN CUSP ANGLE FWD OF SERVICE DOOR STATION 149 TO 164 AT LONGERON 18R, ON CUSP ANGLE AND VERTICAL ANGLE FWD EDGE OF RT SERVI - [SDR ZW0A0101010](https://openairdocs.org/sdr/ZW0A0101010), Apr 26, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AFT OF STA 200, BL 46R THRU BL 57R. INSTALLED NEW MEMBRANE FROM STA 200 TO 220, RBL 46 TO RBL 59, PER DRAWING 9 - [SDR ZW0A0101009](https://openairdocs.org/sdr/ZW0A0101009), Apr 26, 2001: WEB. CRACKED. DURING CHECK-C MAINT FOUND MEMBRANE AT STA 240, RBL 46 IN, WAS CRACKED. NEW MEMBRANE FABRICATED IN SHOP PER INTER SHOP WORK TICKET 837502 AND DRAWING 9930538. I - [SDR ZW0A0101008](https://openairdocs.org/sdr/ZW0A0101008), Apr 26, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT BL 52R THRU 58R, STA 168 THRU 200. CUT OUT DAMAGED SECTION OF MEMBRANE FROM STA 168 TO 200 AND REPAIRED PER - [SDR ZW0A0101007](https://openairdocs.org/sdr/ZW0A0101007), Apr 26, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 151 AND RBL 45R. CUT OUT DAMAGED SECTION OF MEMBRANE FROM STA 148 AND 160 RBL 40 IN TO RBL 59 IN. REPAIR - [SDR ZW0A0101006](https://openairdocs.org/sdr/ZW0A0101006), Apr 26, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND MEMBRANE CORRODED AT STA 160 TO 200, RBL 44 INCHES. CUT OUT CORRODED SECTION OF MEMBRANE FROM STA 160 TO 200, RBL 44 IN TO RBL 58 IN - [SDR ZW0A0101005](https://openairdocs.org/sdr/ZW0A0101005), Apr 26, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT BL 45R AND BETWEEN STA 160 THRU 200. FABRICATED NEW FLOOR SUPPORT PER DRAWING 9936534 AND SPM 6-70-01 P - [SDR ZW0A0100804](https://openairdocs.org/sdr/ZW0A0100804), Apr 24, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CABIN TRACK NUMBER 5 WAS CORRODED AT STA 200 TO 247, RBL 45 INCHES. INSTALLED NEW TRACK PER SPM 6-70-1. INSTALLED FASTENERS PER SRM 5 - [SDR ZW0A0100803](https://openairdocs.org/sdr/ZW0A0100803), Apr 23, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 200, FROM RBL 9 INCHES THRU RBL 46 INCHES. FABRICATED NEW FLOOR SUPPORT PER DRAWING 99 - [SDR ZW0A0100817](https://openairdocs.org/sdr/ZW0A0100817), Apr 23, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED FROM STA 1003 TO 1222. INSTALLED NEW TRACK PER SRM 53-05-4G, PER SRM 51-30-5, 51- - [SDR ZW0A0100809](https://openairdocs.org/sdr/ZW0A0100809), Apr 23, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO BIN AT STA 1220 TO 1332, THE LT TIE DOWN TRACK WAS CORRODED IN SEVERAL PLACES. REPLACED TIE DOWN TRACK STA 1002 TO 1320, L - [SDR ZW0A0100808](https://openairdocs.org/sdr/ZW0A0100808), Apr 23, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN AFT CARGO COMPT, THE LT TIE DOWN TRACK WAS CORRODED FROM STA 1212 TO STA 1231. REPLACED LT SIDE TIE DOWN TRACK FROM STA 1002 TO STA 1320 - [SDR ZW0A0100807](https://openairdocs.org/sdr/ZW0A0100807), Apr 21, 2001: MOUNT. CORRODED. DURING CHECK-C MAINT NUMBER 1 GALLEY TIE DOWN AT BL 10.5R, BL 45R AND BL 51R, HAD CORROSION. INSTALLED GALLEY TIE DOWNS PER SRM 51-30 AND 51-10-4. - [SDR ZW0A0100820](https://openairdocs.org/sdr/ZW0A0100820), Apr 21, 2001: SPLICE. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND LT TIE DOWN TRACK SPLICE CORRODED AT STA 1221. CORRODED SPLICE REMOVED FROM ACFT AND REPLACED WITH NEW. INSTAL - [SDR ZW0A0100806](https://openairdocs.org/sdr/ZW0A0100806), Apr 21, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND CORROSION UNDER NUMBER 1 GALLEY DRAIN PAN OTBD AFT CORNER. FABRICATED NEW MEMBRANE FROM 7075-T6 PER SRM 53-14-1, FIG 11. INSTALLED PE - [SDR ZW0A0100818](https://openairdocs.org/sdr/ZW0A0100818), Apr 20, 2001: SPLICE. CORRODED. DURING CHECK-C MAINT FOUND CORROSION AT AFT END OF LONGERON SPLICE BETWEEN FORMERS 1297 AND 1309 LONGERON 25L. REPLACED LONGERON 25L SPLICE WITH NEW BETWEEN STA - [SDR ZW0A0100819](https://openairdocs.org/sdr/ZW0A0100819), Apr 20, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT FROM STA 1211 TO 1323, RT TIE DOWN TRACK WAS CORRODED IN SEVERAL PLACES. REMOVED CORROSION BY INSTALLING NEW PART WITH SCREWS PER SRM 51-30 - [SDR ZW0A0100816](https://openairdocs.org/sdr/ZW0A0100816), Apr 20, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1320, FROM RBL 17 IN TO LBL 17 IN, THE FLOOR SUPPORT WAS CORRODED. REPLACED FLOOR SUPPORT WITH NEW. TREATED PER - [SDR ZW0A0100709](https://openairdocs.org/sdr/ZW0A0100709), Apr 18, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1320, LONGERON 27R TO 18L, AT STA 1320 FROM RBL 17 IN TO RBL 21 IN CORROSION ON BOTTOM OF FORMER FWD SIDE, - [SDR ZW0A0100507](https://openairdocs.org/sdr/ZW0A0100507), Apr 18, 2001: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO BILGE, FOUND CORROSION ON BOTH SIDE OF THE INTERCOSTAL BETWEEN STA 1309 AND 1323, LBL 17 INCHES. REMOVED AND REPLACED INTE - [SDR ZW0A0100506](https://openairdocs.org/sdr/ZW0A0100506), Apr 18, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT GALLEY AREA, FOUND CORROSION ON NUMBER 2 CHAIR TRACK OTBD FLANGE, FROM STA 1231 TO 1308. INSTALLED NEW CHAIR TRACK PER SPM 6-70- - [SDR ZW0A0100505](https://openairdocs.org/sdr/ZW0A0100505), Apr 18, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT IN CABIN FOUND TRACK CORRODED AT LBL 48 INCHES, STA 1183 TO 1308. REPLACED CHAIR TRACK PER SPM 6-70-01. PRIMED AND PAINTED PER SRM 51-10-3. - [SDR ZW0A0100503](https://openairdocs.org/sdr/ZW0A0100503), Apr 17, 2001: RIB. CRACKED. DURING CHECK-C MAINT ON RT MLG DOOR, THE OTBD CORNER AT Y-948 HAD A CRACK IN THE RIB. ACCOMP NDT STOP DRILL PER 51-00-03, PART 6. STOP DRILLED CRACK PER SRM 51- - [SDR ZW0A0100501](https://openairdocs.org/sdr/ZW0A0100501), Apr 17, 2001: CLIP. CORRODED. DURING CHECK-C MAINT IN THE ELECTRONIC COMPT FOUND CORROSION ON CLIPS AT STA 130 AND 160, BOTH OTBD OF LONGERON 28R. CORRODED CLIPS REMOVED. NEW CLIPS FABRICATE - [SDR ZW0A0100403](https://openairdocs.org/sdr/ZW0A0100403), Apr 16, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN FWD CABIN, FOUND CORROSION ON FLOOR SUPPORT AT STA 160 THRU STA 200, LBL 7 INCHES. MADE NEW FLOOR SUPPORT PER SAMPLE PER SPM 6-70-01, RE - [SDR ZW0A0100402](https://openairdocs.org/sdr/ZW0A0100402), Apr 16, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT TIE DOWN TRACK WAS CORRODED AT STA 1117 TO 1155. REMOVED AND REPLACED TIE DOWN TRACK AS REQUIRED PER SPM 6-70 - [SDR ZW0A0100317](https://openairdocs.org/sdr/ZW0A0100317), Apr 13, 2001: LONGERON. CORRODED. DURING CHECK-C MAINT FOUND DEEP CORROSION ON LONGERON 23R, WITH PITS IN BOTTOM END TIE, STA 1320 TO 1338. REPLACED LONGERON 23R WITH NEW. SEALED PART DURING INS - [SDR ZW0A0100316](https://openairdocs.org/sdr/ZW0A0100316), Apr 12, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION ON FLOOR SUPPORT AT STA 200, FROM BL 0 THRU BL 5L. FABRICATED NEW PART PER SRM 53-14-1, FIG 11. INSTALLED RIVE - [SDR ZW0A0100315](https://openairdocs.org/sdr/ZW0A0100315), Apr 12, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN FWD CABIN, FOUND CORROSION ON FLOOR SUPPORT AT STA 218 AND BL 0. MADE FLOOR SUPPORT PER DRAWING 9936535-31 USING MATERIAL 2929169, 7075- - [SDR ZW0A0100314](https://openairdocs.org/sdr/ZW0A0100314), Apr 12, 2001: LONGERON. CORRODED. DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON LONGERON 30 BETWEEN STA 1003 AND 1022. CORROSION REMOVED BY SPOT FACE AND BLEND PER ARA 17738, SRM 51 - [SDR ZW0A0100313](https://openairdocs.org/sdr/ZW0A0100313), Apr 12, 2001: SEAT TRACK. WORN. DURING CHECK-C MAINT FOUND CAPTAINS SEAT TRACK WORN, FWD OTBD. REPAIRED SEAT TRACK PER SRM 53-05, FIG 92, AND DRAWING CO4216. - [SDR ZW0A0100305](https://openairdocs.org/sdr/ZW0A0100305), Apr 11, 2001: WEB. CORRODED. DURING CHECK-C MAINT IN AFT CABIN, FOUND CORROSION AT FLOOR PAN, STA 1297, BETWEEN 5 AND 6 TRACK. REMOVED OLD MEMBRANE AND REPLACED WITH NEW PER SERVICE BULLETI - [SDR ZW0A0100304](https://openairdocs.org/sdr/ZW0A0100304), Apr 11, 2001: WEB. CORRODED. DURING CHECK-C MAINT IN AFT CARGO COMPT, BETWEEN STA 1287 AND 1306, LONGERON 28R WEB MEMBRANE WAS CORRODED IN TWO PLACES. REMOVED OLD MEMBRANE AND REPLACED WITH - [SDR ZW0A0100303](https://openairdocs.org/sdr/ZW0A0100303), Apr 11, 2001: FRAME. CORRODED. DURING CHECK-C MAINT THE FWD E AND E COMPT FORMER WAS CORRODED BELOW DOOR SILL AND BEHIND EQUIPMENT RACK, STA 168, STRINGER 18R TO 21R. FORMER CORRODED BEOND LI - [SDR ZW0A0100210](https://openairdocs.org/sdr/ZW0A0100210), Apr 10, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN THE FWD CABIN, FOUND CORROSION ON FLOOR SUPPORT AT BL 56 INCHES, AND FROM STA 160 TO 200. REMOVED VISIBLE CORROSION PER SPM 6-80-01. NEW - [SDR ZW0A0100209](https://openairdocs.org/sdr/ZW0A0100209), Apr 10, 2001: ATTACH ANGLE. CRACKED. DURING CHECK-C MAINT FOUND COCKPIT FLOOR PANEL ATTACH ANGLE CRACKED AT STA 121, LBL 2 INCHES. INSTALLED NEW ANGLE PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 5 - [SDR ZW0A0100208](https://openairdocs.org/sdr/ZW0A0100208), Apr 10, 2001: SKIN. DAMAGED. DURING CHECK-C MAINT ON FWD LT FUSELAGE, FOUND CHERRY RIVETED REPAIR AT STA 275, LT SIDE. REPAIRED AREA PER SRM 53-04, FIG 12C. - [SDR ZW0A0100207](https://openairdocs.org/sdr/ZW0A0100207), Apr 10, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND CORROSION AROUND FLIGHT ATTENDANT CHAIR MOUNT ON MEMBRANE AT STA 164 AND BL 15L. CUT OUT DAMAGED AND CORRODED AREA. INSTALLED FILLER - [SDR ZW0A0100107](https://openairdocs.org/sdr/ZW0A0100107), Apr 9, 2001: SKIN. GOUGED. DURING CHECK-C MAINT FOUND GOUGE IN FUSELAGE SKIN BELOW LAV SERVICE PANEL, CURRENTLY HAVING SURFACE PATCH INSTALLED. CUT OUT SKIN AND INSTALLED DOUBLER PER SRM - [SDR ZW0A0100106](https://openairdocs.org/sdr/ZW0A0100106), Apr 9, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CORRODED AT STA 200, RBL 47 IN TO 58 IN. FLOOR SUPPORT CORRODED BEYOND LIMITS. FABRICATED NEW FLOOR SUPPORT PER S - [SDR ZW0A0100105](https://openairdocs.org/sdr/ZW0A0100105), Apr 9, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CABIN TRACK CORRODED AT LBL 55 INCHES, STA 995 TO 1136. REMOVED CORROSION PER SPM 6-80-01 PAGE 3. INSTALLED AND REPLACED SEAT TRACK P - [SDR ZW0A0100502](https://openairdocs.org/sdr/ZW0A0100502), Apr 7, 2001: FRAME. CRACKED. DURING CHECK-C MAINT AT RT MLG WHEEL WELL DOOR, FOUND A ONE INCH CRACK IN RADIUS OF UPPER END OF FORMER, SECOND AFT OF THE DOOR. ACCOMP NDT STOP DRILL PER 51-00 - [SDR ZW0A0100104](https://openairdocs.org/sdr/ZW0A0100104), Apr 6, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT FOUND CRACK ON LONGERON 4L AT STA 160. REMOVED AND INSTALLED NEW LONGERON PER SPM 6-70-01 PAGE 3 PARA 4. INSTALLED RIVETS PER SRM 51-30-02. - [SDR ZW0A0100206](https://openairdocs.org/sdr/ZW0A0100206), Apr 5, 2001: FRAME. CORRODED. DURING CHECK-C MAINT IN AFT CARGO COMPT, FOUND CORROSION ON UPPER EDGE OF FORMER AT STA 1271 BETWEEN RBL 6 AND LBL 6. REMOVED CORROSION PER SPM 6-80-01. - [SDR ZW0A0100205](https://openairdocs.org/sdr/ZW0A0100205), Apr 5, 2001: STRUCTURE. CORRODED. DURING CHECK-C MAINT FOUND IN CABIN, CORROSION AROUND RIVETS AT BL 0, FROM STA 160 THRU 200. REMOVED CORROSION PER SPM 6-80-01. REPLACED FASTENERS PER SRM 51-30 - [SDR ZW0A0100204](https://openairdocs.org/sdr/ZW0A0100204), Apr 5, 2001: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT FOUND IN CABIN, CORROSION ON INTERCOSTAL AND CLIP AT LONGERON 16R, STA 160 TO 165. REMOVED CORROSION PER SPM 6-80-01. - [SDR TWAA0106306](https://openairdocs.org/sdr/TWAA0106306), Apr 4, 2001: STOP FITTING. CRACKED. DURING CHECK-C MAINT IN THE AFT CABIN, THE AFT CABIN ENTRY DOOR STOP CASTING WAS CRACKED ON RT SIDE, 36 INCHES ABOVE FLOOR RBL 17 INCHES. REPLACED BRACKET PER S - [SDR TWAA0106305](https://openairdocs.org/sdr/TWAA0106305), Apr 4, 2001: STOP FITTING. CRACKED. DURING CHECK-C MAINT IN THE AFT CABIN, THE AFT ENTRY DOOR STOP CASTING WAS CRACKED ON RT SIDE, 18 INCHES ABOVE FLOOR RBL 17 INCHES. REPLACED BRACKET WITH NEW PE - [SDR TWAA0106304](https://openairdocs.org/sdr/TWAA0106304), Apr 4, 2001: FRAME. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FOUND CORROSION ON FORMER AT STA 1155 BETWEEN LONGERON 25L THRU 27L. REMOVED PART FROM AIRCRAFT. REMOVED CORROSION - [SDR TWAA0106230](https://openairdocs.org/sdr/TWAA0106230), Apr 4, 2001: SUPPORT BRACKET. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON SUPPORT BRACKET AT STA 1148, ABOVE LONGERON 20R. FABRICATED NEW SUPPORT ANGLE PER PART REMOVED US All 102: https://openairdocs.org/deregistered/N906TW-2008-07-07/reports.md ## FAA accident and incident reports (6) 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 19990820032289I](https://openairdocs.org/incident/19990820032289I), Aug 20, 1999: Doug DC982 (N906TW), Salt Lake City, UT. (-23) On takeoff the left engine had two compressor stalls. The throttle was retarded slowly and then advanced producing another stall. The power was set at… - [Incident 19971228042599I](https://openairdocs.org/incident/19971228042599I), Dec 28, 1997: Doug DC982 (N906TW), Indianapolis, IN. Narrative: flight 46B enroute stl-lga diverted to ind due to fuel imbalance. An emergency was declared due to the rt. Main fuel quantity was decreasing but not… - [Incident 19950725026909I](https://openairdocs.org/incident/19950725026909I), Jul 25, 1995: Doug DC982 (N906TW), Baltimore, MD, Minor damage. NR2 engine turbine failed on climbout. Returned. Failure was contained. - [Incident 19860927059809I](https://openairdocs.org/incident/19860927059809I), Sep 27, 1986: Doug DC982 (N906TW), St Louis, MO, Minor damage. Wing tip struck a fence while positioning aircraft in a penalty box. - [Incident 19850918050689I](https://openairdocs.org/incident/19850918050689I), Sep 18, 1985: Doug DC982 (N906TW), St Louis, MO. Aborted takeoff due to number 1 gen trip and csd low oil pressure light. Oil leak at csd oil out line retorqued. - [Incident 19850226009079I](https://openairdocs.org/incident/19850226009079I), Feb 26, 1985: Doug DC982 (N906TW), Portland, OR, Minor damage. Mild compressor stalls on power back, taxi and with takeoff power application. FOD to nr 1 and nr 2 engines. ## Other aircraft with N906TW - [Registered now](https://openairdocs.org/aircraft/N906TW): Textron B300, S/N FL-1138, built 2018 --- 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.