# N911TW: 1983 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2007-03-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 14, 2007
- Exported to: Thailand
- 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: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 49182
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: December 8, 1983
- Certificate issued: January 10, 2007
- Last registry action: January 10, 2007
- Mode S code: AC9C20
- 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/N911TW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=911TW
- Page: https://openairdocs.org/deregistered/N911TW-2007-03-14

From the FAA registry file of October 31, 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 (34)

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

- [SDR ZW0A0212603](https://openairdocs.org/sdr/ZW0A0212603), Dec 19, 2002: CABLE. THE FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE CABLE AND DRIED MOISTURE FROM THE TRACK. CHECK-C 8-15-02 STL. --CLOSED--
- [SDR ZW0A0108808](https://openairdocs.org/sdr/ZW0A0108808), Sep 18, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE RT TIE DOWN TRACK FROM STA 1212 TO 1322 WAS CORRODED. INSTALLED FABRICATED TRACK FROM STOCK. TRACK INSTALLED PER
- [SDR ZW0A0108807](https://openairdocs.org/sdr/ZW0A0108807), Sep 18, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND LT FLOOR TRACK CORRODED AT CLIP NUT HOLES AT STA 1222 THRU 1322, TIE DOWN TRACK. REMOVED CORRODED TRACK AND IN
- [SDR ZW0A0108806](https://openairdocs.org/sdr/ZW0A0108806), Sep 14, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND IN THE AFT CARGO COMPT, STA 1212 TO 1219, BETWEEN LONGERON 27R AND 28R, CORROSION ON BOTTOM SIDE OF UPPER WEB SKIN AND STRUCTURE AFT 
- [SDR ZW0A0108805](https://openairdocs.org/sdr/ZW0A0108805), Sep 14, 2001: DOOR FRAME. CRACKED. DURING CHECK-C MAINT FOUND APPROX 2 INCH CRACK IN FWD LEFT CABIN OUTER DOOR FRAME, LOWER FWD CORNER BELOW THE DOOR HINGE ASSEMBLY. REPLACED LOWER FWD CORNER OF 
- [SDR ZW0A0108802](https://openairdocs.org/sdr/ZW0A0108802), Sep 13, 2001: SILL. DAMAGED. DURING CHECK-C MAINT FOUND THE AFT CARGO COMPT DOOR SILL OTBD FLANGE HAD MATERIAL REMOVED BEYOND LIMITS, STA 1155 THRU 1212. REPAIRED TWO OUT OF LIMITS AREAS PE
- [SDR ZW0A0108706](https://openairdocs.org/sdr/ZW0A0108706), Sep 13, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CHAIR TRACK AT LBL 44 INCHES, STA 1088 TO 1309, WAS CORRODED BEYOND LIMITS. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK WITH TRACK
- [SDR ZW0A0108705](https://openairdocs.org/sdr/ZW0A0108705), Sep 13, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON LT CHAIR TRACK AT LBL 54, STA 1282 AND 1174. REMOVED CORROSION BY REPLACING CHAIR TRACK FROM STA 1174 TO 1309, LBL 54 IN
- [SDR ZW0A0108610](https://openairdocs.org/sdr/ZW0A0108610), Sep 12, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 3 CABIN FLOOR TRACK AT LBL 22 INCHES, STA 1096 TO 1309. REPLACED CHAIR TRACK PER SRM 53-05 AND DRAWING CO3580. IN
- [SDR ZW0A0108609](https://openairdocs.org/sdr/ZW0A0108609), Sep 12, 2001: PAN. CORRODED. DURING CHECK-C MAINT FOUND AREA UNDER FWD CABIN GALLEY DRAIN CORRODED ALL AROUND PAN AS VIEWED FROM THE E&E COMPARTMENT. INSTALLED REPAIR DOUBLER PER SRM 53-01,
- [SDR ZW0A0108608](https://openairdocs.org/sdr/ZW0A0108608), Sep 11, 2001: FRAME. CORRODED. DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON STA 1309 FORMER, FROM RT LONGERON TO LT LONGERON 25. ACCOMPLISHED SERVICE REWORK PER DRAWING SRO95300
- [SDR ZW0A0108316](https://openairdocs.org/sdr/ZW0A0108316), Sep 10, 2001: BEAM. CRACKED. DURING CHECK-C MAINT ON THE FWD LT PASSENGER DOOR, THE NR 6 DOOR BEAM WAS CRACKED 4 INCHES BELOW BAYONET FITTING. REPLACED THE NR 6 BEAM PER MM AND SRM 51-00, P
- [SDR ZW0A0108318](https://openairdocs.org/sdr/ZW0A0108318), Sep 8, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT RBL 44, STA 180 TO 200. INSTALLED NEW FLOOR SUPPORT PER SRM 51-30-7 AND SPM 6-70-01.
- [SDR ZW0A0108317](https://openairdocs.org/sdr/ZW0A0108317), Sep 7, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON RT FLOOR MEMBRANE AT STA 1297 TO 1309, BETWEEN RBL 44 IN AND RBL 54 IN TRACKS. INSTALLED REPAIRED WEB PER SRM 53-05, FIG
- [SDR ZW0A0108315](https://openairdocs.org/sdr/ZW0A0108315), Sep 6, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON AFT TOP OF FORMER LOCATED 9 INCHES LBL TO 21 IN LBL. REMOVED CORROSION FROM FORMER STA 1322, LBL 9 IN TO LBL 21 IN AND S
- [SDR ZW0A0108209](https://openairdocs.org/sdr/ZW0A0108209), Sep 6, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON AFT TOP OF FORMER, 9 INCHES LBL TO 21 IN LBL. REMOVED CORROSION FROM FORMER STA 1322, LBL 9 IN TO LBL 21 IN. SPLICED NEW
- [SDR ZW0A0108003](https://openairdocs.org/sdr/ZW0A0108003), Aug 29, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT FOUND CRACK IN LONGERON 4L AT ATTACH POINT OF LONGERON TO STA 160 FORMER, OTBD FASTENER. REPLACED LONGERON PER SPM 6-70-01.
- [SDR ZW0A0108002](https://openairdocs.org/sdr/ZW0A0108002), Aug 28, 2001: ATTACH ANGLE. CORRODED. DURING CHECK-C MAINT THE L1 DOOR SILL PLATE ATTACH ANGLE HAD CORROSION ON UPPER AND LOWER EDGE APPROXIMATELY STA 170 TO 190, LBL 57. FABRICATED NEW FLOOR SUPPOR
- [SDR TWAA0104702](https://openairdocs.org/sdr/TWAA0104702), Mar 11, 2001: SKIN. DENTED. A DENT 18 IN BY 12 IN BY 0.500 INCHES WAS FOUND ON PREFLIGHT, 8 FEET FWD OF THE FWD CARGO DOOR AND 30 IN AFT OF THE DRAIN MAST. FRAME BETWEEN LONGERON 24R AND 2
- [SDR TWAA0100501](https://openairdocs.org/sdr/TWAA0100501), Jan 5, 2001: ACM. CONTAMINATED. FUMES WERE REPORTED IN THE CABIN. OIL WAS FOUND IN THE LT ACM DUCTS. REPLACED THE ACM, CHANGED WATER SEPERATERS, AND ACCOMPLISHED PACK BURN OUT. CHECK-C 8-20-00
- [SDR TWAA0016602](https://openairdocs.org/sdr/TWAA0016602), Oct 23, 2000: BATTERY. DISCHARGED. BOTH COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 8-20-00 STL.
- [SDR TWAA0014401](https://openairdocs.org/sdr/TWAA0014401), Sep 14, 2000: POWER SUPPLY. INOPERATIVE. THE FIRST CLASS OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 8-9-00 STL.
- [SDR TWAA0009603](https://openairdocs.org/sdr/TWAA0009603), Jun 16, 2000: BATTERY. INOPERATIVE. THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 7 AND 10 WERE VERY DIM, AND A SMALL SECTION OF EGRESS LIGHTING WAS INOPERATIVE BETWEEN ROWS 24 AND 26. REPLACED THE BA
- [SDR TWAA0004601](https://openairdocs.org/sdr/TWAA0004601), Mar 19, 2000: A/C PACK. MALFUNCTIONED. ONE MINUTE PRIOR TO LANDING, AIR CONDITIONING TEMPERATURE INCREASED AND CABIN FILLED WITH SMOKE. TURNED OFF BOTH AIR CONDITIONING PACKS, DID NOT START THE APU. 
- [SDR TWAA9911206](https://openairdocs.org/sdr/TWAA9911206), Aug 9, 1999: BRACKET. CRACKED. DURING CHECK C MAINT, FOUND MOUNT BRACKET LEG AND WEB CRACKED AT RUDDER PITOT DRAIN MANIFOLD IN RT TAIL COMPT. REPAIRED BRACKET LEG AS NEC PER DC9 SRM 53-01, PA
- [SDR TWAA9818903](https://openairdocs.org/sdr/TWAA9818903), Nov 22, 1998: POWER SUPPLY. INOP. DURING PREFLIGHT INSPECTION, FOUND EGRESS LIGHTS INOP BETWEEN ROWS 2 TO 15. REPLACED POWER SUPPLY.
- [SDR TWAA9818802](https://openairdocs.org/sdr/TWAA9818802), Nov 22, 1998: BATTERY PACK. DISCHARGED. FOUND EGRESS TRACK LIGHTING INOPERATIVE BETWEEN CABIN ROW 2 AND 15. REPLACED BATTERY PACK AND REPAIRED FEEDER STRIP AT ROW 7. CHECK-C 9-17-98 STL.
- [SDR TWAA9803301](https://openairdocs.org/sdr/TWAA9803301), Mar 6, 1998: APU. MALFUNCTIONED. MCI - FLT 123 - THE APU QUIT IN-FLIGHT WITH THE LEFT ENGINE GENERATOR ALREADY DEFERRED INOPERATIVE PER MEL. MADE UNSCHEUDLED LANDING AT MCI. CORRECTED LT ENGINE
- [SDR TWAA9715201](https://openairdocs.org/sdr/TWAA9715201), Dec 26, 1997: WINDSHIELD. CRACKED. SFO - FLT 272 - IN CRUISE, THE FIRST OFFICER'S NR 1 WINDSHIELD CRACKED. REPLACED THE FIRST OFFICER'S NR 1 WINDSHIELD. MFG NR 5912290-506. OP-16 9-9-97 MCI. (X)
- [SDR TWAA9806010](https://openairdocs.org/sdr/TWAA9806010), Sep 19, 1997: SKIN. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE SKIN CRACKED BEYOND STOP DRILL ON A REPAIR, AT 3 PLACES FS 465 TO 470, STRINGER 30. REPAIRED PER ARA 11453 
- [SDR 96ZZZX4906](https://openairdocs.org/sdr/96ZZZX4906), Jul 6, 1996: STATOR. FAILED. OMA - FLT 114 - INVESTIGATION OF NR 2 ENGINE, S/N 3225, SHUTDOWN REVEALED AN 8TH STAGE COMPRESSOR STATOR, MFG P/N 789788, FRACTURED LIBERATING METAL PARTICLES I
- [SDR 96ZZZM1219](https://openairdocs.org/sdr/96ZZZM1219), Jul 6, 1996: TURBINE. FAILED. OMA - DURING CRUISE NR 2 ENGINE, S/N 3225, WAS SHUTDOWN DUE TO TURBINE FAILURE. ENGINE TOTAL TIME 34,212, CYCLES 17,878.
- [SDR 95ZZZM751](https://openairdocs.org/sdr/95ZZZM751), Nov 11, 1995: BUSHING. FAILED. ICT - DURING CRUISE, NR 1 ENGINE, S/N 3210, SPOOLED DOWN. SHUT DOWN ENGINE. FOUND INTERNAL MALFUNCTION IN N-2 ACCESSORY GEARBOX, MFG P/N 758300. CHANGED ENGINE 
- [SDR 95ZZZX1661](https://openairdocs.org/sdr/95ZZZX1661), Mar 21, 1995: SENSOR. FAILED. BOS - FLT 184 - DURING CRUISE ONE HOUR AFTER TAKEOFF, NLG RED UNSAFE LIGHT ILLUMINATED. DURING APPROACH, RED UNSAFE LIGHT REMAINED ON. CYCLED LANDING GEAR AND L

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DEN05IA083](https://openairdocs.org/ntsb/DEN05IA083), May 28, 2005: McDonnell Douglas DC-9-82 (N911TW), Denver, CO, incident, minor damage. Probable cause: the reason for the occurrence was not determined.

## 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 20050528012049I](https://openairdocs.org/incident/20050528012049I), May 28, 2005: Doug DC982 (N911TW), Denver, CO, Minor damage. (-23) Note: American airlines has enrolled in the asap program; this crew has filed an asap report. Aircraft landed normally on rw 25R @den. Tire tracks showed…
- [Incident 19960706035639I](https://openairdocs.org/incident/19960706035639I), Jul 6, 1996: Doug DC982 (N911TW), Omaha, NE. Narrative: on July 6, 1996, a DC-9-82, N911TW, operating as twa flight 114 was enroute seattle, WA to st. louis, MO when the #2 (right) engine experienced high…
- [Incident 19880507020689I](https://openairdocs.org/incident/19880507020689I), May 7, 1988: Doug DC982 (N911TW), St Louis, MO. Stoiler deploy light came on on takeoff roll. Aborted safely. Adjusted wing inboard spoiler proximity switch.
- [Incident 19880323014229I](https://openairdocs.org/incident/19880323014229I), Mar 23, 1988: Doug DC982 (N911TW), St Louis, MO. Hydraulic system malfunctioned on climb. Returned. O-ring failed at engine driven pump. De-pressurization solenoid.
- [Incident 19870928062809I](https://openairdocs.org/incident/19870928062809I), Sep 28, 1987: Doug DC982 (N911TW), St Louis, MO. An aircraft landed short of a displaced threshold, damaging wiring. Inconclusive evidence this aircraft was the one
- [Incident 19860117004069I](https://openairdocs.org/incident/19860117004069I), Jan 17, 1986: Doug DC982 (N911TW), San Jose, CA, Minor damage. More than normal engine noise and vibration noted. Found FOD to both engines at destination.

## Other aircraft with N911TW

- [Registered now](https://openairdocs.org/aircraft/N911TW): Cirrus Design SR22, S/N 3172, built 2008

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