# N905TW: 1983 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2008-06-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 11, 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: 49157
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 19, 1983
- Certificate issued: March 2, 2006
- Last registry action: March 2, 2006
- Mode S code: AC837D
- 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/N905TW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=905TW
- Page: https://openairdocs.org/deregistered/N905TW-2008-06-11

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 (81, newest 50)

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

- [SDR AALA20060365](https://openairdocs.org/sdr/AALA20060365), Jun 6, 2006: ENGINE. MAKING METAL. IAD - CREW HEARD LOUD BANG AND REPORTED NUMBER TWO ENGINE COMPRESSOR STALL AT FLIGHT LEVEL 320. ENGINE AT IDLE WITH ALL PARAMETERS NORMAL. LANDED IAD WITHOUT IN
- [SDR AALA20050813](https://openairdocs.org/sdr/AALA20050813), Dec 11, 2005: COMPRESSOR. STALLED. STL - AT FL280 RIGHT ENGINE COMPRESSOR STALLED. OPERATED ENGINE AT IDLE AND LANDED STL WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMA
- [SDR AALA20050171](https://openairdocs.org/sdr/AALA20050171), Mar 6, 2005: CONTACT. DIRTY. SFO - ENTRY EMERGENCY LIGHTS AT NUMBER ONE DOOR INOPERATIVE. CLEANED CONTACTS FOR POWER AND GROUND FOR LEFT NUMBER 1 ENTRY DOOR EMERGENCY LIGHTS. SYSTEM GROUND 
- [SDR ZW0A0305002](https://openairdocs.org/sdr/ZW0A0305002), May 21, 2003: LIGHT. INOPERATIVE. THE EGRESS LIGHT AT ROW 7 AND THE EMERGENCY LIGHTS ABOVE THE L1 AND L2 DOORS WERE INOPERATIVE. REINSERTED THE LAMP INTO THE MODULE FOR THE EGRESS LIGHT, REPLACE
- [SDR ZW0A0305003](https://openairdocs.org/sdr/ZW0A0305003), May 21, 2003: BATTERY. INOPERATIVE. THE EMERGENCY LIGHTS AT BOTH AFT OVERWING EXITS, AND THE RT SIDEWALL EMERGENCY LIGHT IN THE TAILCONE, WERE INOPERATIVE. REPLACED THE BATTERY PN 408822101 IN THE
- [SDR ZW0A0303602](https://openairdocs.org/sdr/ZW0A0303602), Mar 27, 2003: POWER SUPPLY. INOPERATIVE. THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 25 THRU 31. REPLACED THE POWER SUPPLY. CHECK-C 12-3-02 STL.
- [SDR ZW0A0210701](https://openairdocs.org/sdr/ZW0A0210701), Oct 21, 2002: TRANSMITTER. MALFUNCTIONED. ON APPROACH WHEN FLAPS SELECTED TO 40 GOT SLAT DISAGREE LIGHT. SLOWED DESCEND RATE AND GOT STICK SHAKER. ACCOMPLISHED GO AROUND. SECOND APPROACH WAS NORMAL. REP
- [SDR ZW0A0205501](https://openairdocs.org/sdr/ZW0A0205501), May 28, 2002: WINDSHIELD. CAPTAIN'S WINDSHIELD CRACKED AND SHATTERED SHORTLY AFTER TAKEOFF.R/R CRACKED WINDSHIELD (P/N 217-0332), OPS CHECK WINDOW HEAT AND OPERATION NORMAL. --CLOSED-- L
- [SDR ZW0A0203001](https://openairdocs.org/sdr/ZW0A0203001), Mar 12, 2002: BLADE. FAILED. A LOUD BANG WAS HEARD FROM THE RIGHT ENGINE AND THE ENGINE SHUT ITSELF DOWN. THE FLIGHT RETURNED TO AIRPORT AND THE ENGINE WAS REPLACED. A FOURTH STAGE TURBINE 
- [SDR ZW0A0109901](https://openairdocs.org/sdr/ZW0A0109901), Oct 20, 2001: BATTERY PACK. DISCHARGED. THE CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE ROWS 12 TO 21 AND 28 TO 29, AND THE EGRESS LIGHTS WERE INOPERATIVE ROW 1 TO 14. REPLACED THE BATTERIES P/N 4
- [SDR ZW0A0109501](https://openairdocs.org/sdr/ZW0A0109501), Oct 8, 2001: BRACKET. CRACKED. DURING CHECK-C MAINT FOUND BRACKET CRACKED AT STA 1485, 18 INCHES RBL, JUST FWD OF RUDDER TRIM CABLE SPOOL BRACKET. FABRICATED AND INSTALLED REPLACEMENT BRACKET
- [SDR ZW0A0108602](https://openairdocs.org/sdr/ZW0A0108602), Sep 14, 2001: LIGHT. INOPERATIVE. THE AFT TAIL CONE AREA EMERGENCY CAT WALK LIGHT, AND THE AFT TAIL CONE AREA EMERGENCY LIGHT, WERE INOPERATIVE. REPLACED THE LIGHT ASSEMBLY P/N 0200335-001 FOR T
- [SDR ZW0A0108601](https://openairdocs.org/sdr/ZW0A0108601), Sep 14, 2001: LIGHT. INOPERATIVE. THE EMERGENCY EXIT SIGN AT THE LT OVERWING EXIT, AND THE EMERGENCY CEILING LIGHT BETWEEN NUMBER 4 GALLEY AND THE AFT AIRSTAIR DOOR, WERE INOPERATIVE. REPLACED T
- [SDR ZW0A0103301](https://openairdocs.org/sdr/ZW0A0103301), Jun 11, 2001: WIRE. CHAFED. CREW REPORTED THE PA SYSTEM WAS INOPERATIVE FROM THE AFT FLIGHT ATTENDANT POSITION. FOUND SEVERAL WIRES HAD SHORTED AND BURNED FROM RUBBING ON A LIGHTENING HOLE
- [SDR TWAA0106212](https://openairdocs.org/sdr/TWAA0106212), Mar 30, 2001: LONGERON. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON LONGERON 26R, BETWEEN STA 1338 AND 1322. INSTALLED NEW LONGERON AND SPLICE PER SRM 53-02, PAGE 49 AND ARA 17645, STA 129
- [SDR TWAA0106211](https://openairdocs.org/sdr/TWAA0106211), Mar 30, 2001: FITTING. CORRODED. DURING CHECK-C MAINT FOUND STRINGER TIE FITTING HAD CORROSION AT STA 1338, STRINGER 21R. REPLACED STRINGER 21R TIE FITTING PER SRM 51-30-05.
- [SDR TWAA0105912](https://openairdocs.org/sdr/TWAA0105912), Mar 29, 2001: SKIN. DENTED. DURING CHECK-C MAINT FOUND DENT IN FUSLEAGE AT STA 237, BETWEEN LONGERON 24L AND 25L. DENT WAS 1 INCH BY 2 IN BY 0.050 DEEP. REPAIRED DENT PER 53-04, PAGE 37 FI
- [SDR TWAA0105910](https://openairdocs.org/sdr/TWAA0105910), Mar 29, 2001: SKIN. DENTED. DURING CHECK-C MAINT FOUND DENT IN FUSELAGE FROM STA 229 TO 234, BETWEEN LONGERON 24L AND 25L. DENT WAS 5 INCHES BY 1.750 BY 0.020 DEEP. REPAIRED DENT IN FUSELA
- [SDR TWAA0105804](https://openairdocs.org/sdr/TWAA0105804), Mar 27, 2001: BULKHEAD. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON PRESSURE BULKHEAD AT STA 1338, BETWEEN STRINGER 25R AND 26R. REMOVED AND REPLACED TIE FITTING. INSTALLED FASTENERS PER D
- [SDR TWAA0105703](https://openairdocs.org/sdr/TWAA0105703), Mar 26, 2001: SKIN. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON STA 1338 AFT PRESSURE BULKHEAD LOWER TEE. REPLACED FUSELAGE SKIN STA 1311 TO 1338, LONGERON 21R TO 26R, PER ARA 17647 AN
- [SDR TWAA0106213](https://openairdocs.org/sdr/TWAA0106213), Mar 2, 2001: ANGLE. CORRODED. DURING CHECK-C MAINT THE LOWER Y CHORD SECTION AT STA 1338, STRINGER 24R TO 24L, HAD CORROSION. INSTALLED Y-CHORD PER SRM 53-03 FIG 37A, AND ARA 17647A, STRINGE
- [SDR TWAA0103607](https://openairdocs.org/sdr/TWAA0103607), Feb 21, 2001: FORMER. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1308 AT LONGERON 28L TO 28R. CUT OUT CORROSION. INSTALLED NEW FORMER SECTION LONGERON 28L TO 28R AND REPAI
- [SDR TWAA0103404](https://openairdocs.org/sdr/TWAA0103404), Feb 20, 2001: FORMER. DAMAGED. DURING CHECK-C MAINT FOUND AIR SUPPLY VALVE HAD WORN HOLE INTO FORMER RING AT STA 1380, BELOW LONGERON 5L AND 6L. INSTALLED DOUBLER PER SRM 53-01 FIG 4. REINSTA
- [SDR TWAA0103324](https://openairdocs.org/sdr/TWAA0103324), Feb 19, 2001: LONGERON. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON LONGERON 29L, STA 1287 TO 1308. REMOVED CORROSION BY REPLACING PART. INSTALLED NEW LONGERON PER SRM 53-14-3, PAGE 21. IN
- [SDR TWAA0103325](https://openairdocs.org/sdr/TWAA0103325), Feb 16, 2001: LONGERON. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON BOTTOM OF LONGERON 20R AT INTERSECTION WITH STA 1338 AND TIE CLIP AT END OF LONGERON. REMOVED CORRODED EXTRUSION SECTION
- [SDR TWAA0103323](https://openairdocs.org/sdr/TWAA0103323), Feb 16, 2001: FORMER. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FORMER 1338, 4 INCHES ABOVE LONGERON 18L, AFT OF LAV TANK HOLD DOWN CLIP, BETWEEN CLIP AND FORMER. REPAIRED PER SRM 53-0
- [SDR TWAA0103322](https://openairdocs.org/sdr/TWAA0103322), Feb 15, 2001: FORMER. CORRODED. DURING CHECK-C MAINT FOUND FORMER WITH CORROSION AT STA 1338, 5 INCHES ABOVE LONGERON 18R AT ATTACH POINT FOR LAV TANK HOLD DOWN CABLE. REPAIRED FORMER PER SRM 
- [SDR TWAA0103320](https://openairdocs.org/sdr/TWAA0103320), Feb 15, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND TOP OF FLOOR SUPPORT CORRODED IN SEVERAL PLACES AT STA 1155, BETWEEN LBL 15 AND RBL 07. INSTALLED NEW SUPPORT REF IPC 25-52-00 FIG 3L
- [SDR TWAA0103319](https://openairdocs.org/sdr/TWAA0103319), Feb 15, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT SEVERAL PLACES STA 1136 TO 1212, RBL 8 INCHES. INSTALLED NEW SUPPORT PER DRAWING 5936660. INSTALLED BOLTS, 
- [SDR TWAA0103318](https://openairdocs.org/sdr/TWAA0103318), Feb 15, 2001: SPLICE. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON LONGERON SPLICE AT STA 1193, LONGERON 29L. REMOVED CORROSION BY REPLACEMENT OF PART. INSTALLED FABRICATED PART MANUFACTU
- [SDR TWAA0103104](https://openairdocs.org/sdr/TWAA0103104), Feb 13, 2001: BRACKET. CORRODED. DURING CHECK-C MAINT FOUND BRACKETS CORRODED AT FWD CARGO DOOR STA 1155 LOWER AFT CORNER OF ENTRY SILL AREA, AND STA 1212 LOWER FWD CORNER OF ENTRY SILL AREA. I
- [SDR TWAA0103009](https://openairdocs.org/sdr/TWAA0103009), Feb 13, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND FORMER CORRODED AT STA 1212, LONGERON 26 TO 27L. REMOVED CORROSION BY REPLACEMENT OF PART. INSTALLED NEW FRAME PER PRINT 9936073.
- [SDR TWAA0102806](https://openairdocs.org/sdr/TWAA0102806), Feb 12, 2001: SHEAR TIE. CRACKED. DURING CHECK-C MAINT FOUND FORMER FOOT CRACKED AT STA 1309, BETWEEN LONGERON 13 AND 14. REPLACED CRACKED FORMER FOOT. SPLICED PER SRM 53-03 FIG 3. INSTALLED PER
- [SDR TWAA0103321](https://openairdocs.org/sdr/TWAA0103321), Feb 10, 2001: FLOORBEAM. CORRODED. DURING CHECK-C MAINT IN FWD CARGO COMPT FOUND CORROSION ON BOTTOM OF FLOOR SUPPORT AT STA 138, AT INTERSECTION WITH LONGERON 18R, CORROSION ON REAR OF BULKHEAD 
- [SDR TWAA0102805](https://openairdocs.org/sdr/TWAA0102805), Feb 10, 2001: SKIN. DENTED. DURING CHECK-C MAINT FOUND DENT 2.7 BY 3.6 BY 0.093 DEEP IN SKIN OF AFT CARGO DOOR. CUT OUT 2 .6875 ROUND PLUG FROM SKIN 0.050. INSTALLED 2024-T3 PLUG WITH A BA
- [SDR TWAA0102804](https://openairdocs.org/sdr/TWAA0102804), Feb 10, 2001: FLOORBEAM. CORRODED. DURING CHECK-C MAINT FOUND 4 INCH J-ANGLE FLOOR SUPPORT CORRODED AT STA 1155, RBL 13 INCHES. REPLACED ANGLE WITH NEW. INSTALLED HI-LOKS PER SRM 51-30-5.
- [SDR TWAA0102803](https://openairdocs.org/sdr/TWAA0102803), Feb 9, 2001: FRAME. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS FOUND ON FORMER AT STA 1271, LONGERON 28R TO 28L. REMOVED CORROSION. INSTALLED NEW J-ANGLE. PAINTED R
- [SDR TWAA0102802](https://openairdocs.org/sdr/TWAA0102802), Feb 7, 2001: SHEAR TIE. CRACKED. DURING CHECK-C MAINT FOUND CRACK AT FORMER FOOT (SHEAR TIE) STA 1429, BETWEEN LONGERON 1 AND 2R. REPLACED FORMER FOOR PER DRAWING 9911840-112. INSTALLED PER 51-
- [SDR TWAA0102713](https://openairdocs.org/sdr/TWAA0102713), Feb 7, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND FLOOR MEMBRANE CORRODED AT STA 163, LBL 16 INCHES. REMOVED CORROSION PER SPM 6-80-01. TREATED AREA PER SRM 51-10-3. FABRICATED DOUBLE
- [SDR TWAA0102712](https://openairdocs.org/sdr/TWAA0102712), Feb 7, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND HEAVY CORROSION ON MEMBRANE AT LBL 54 INCHES, BETWEEN STA 160 AND 190. REMOVED CORRODED AREA. FABRICATED DOUBLER AND INSTALLED PER SR
- [SDR TWAA0102507](https://openairdocs.org/sdr/TWAA0102507), Feb 4, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT AT LBL 54, STA 1309, FOUND CORROSION ON CABIN CHAIR TRACK FLANGE. REMOVED CORROSION PER SPM 6-80-01. REMOVED DAMAGED TRACK PER DRAWING 5930
- [SDR TWAA0102506](https://openairdocs.org/sdr/TWAA0102506), Feb 4, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CABIN FLOOR TRACK AT LBL 54, THE NUMBER 1 TRACK WAS GROUND BEYOND LIMITS AT STA 1237 AND 1303. REMOVED DAMAGED TRACK STA 1174 TO 1303
- [SDR TWAA0102505](https://openairdocs.org/sdr/TWAA0102505), Feb 4, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN CABIN ON SEAT TRACK, AT LBL 54 INCHES, STA 1252 AND STA 1283 TO 1280. REMOVED DAMAGED TRACK AT BOTH LOCATIONS. INSTALLED
- [SDR TWAA0102407](https://openairdocs.org/sdr/TWAA0102407), Feb 1, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORRODED FLOOR PANEL SUPPORT AT STA 200, RBL 4 INCHES TO LBL 4 INCHES. REMOVED CORRODED SUPPORT. FABRICATED NEW SUPPORT FROM STOCK AN
- [SDR TWAA0102406](https://openairdocs.org/sdr/TWAA0102406), Feb 1, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORRODED FLOOR SUPPORT AT RBL 44 INCHES, STA 160 TO 200. REMOVED CORRODED SUPPORT AND FABRICATED NEW SUPPORT. INSTALLED PER SRM 51-30
- [SDR TWAA0102202](https://openairdocs.org/sdr/TWAA0102202), Jan 31, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT, FOUND LONGERON 12L CRACKED AT ATTACH POINT TO 1287 FORMER RING. REMOVED CRACKED LONGERON FOR REPAIR PER SRM 53-02 FIG 18.
- [SDR TWAA0102201](https://openairdocs.org/sdr/TWAA0102201), Jan 31, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION AT LBL 36 INCHES, STA 1138 TO 1110. REPLACED TRACK. FABRICATED NEW TRACK FROM STOCK AND INSTALLED PER SRM 51-30-01. PRIMED
- [SDR TWAA0103407](https://openairdocs.org/sdr/TWAA0103407), Jan 29, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CHAIR TRACK WITH HEAVY CORROSION AT STA 1130 TO 1322, LBL 22 INCHES. REMOVED AND REPLACED TRACK PER SPM 6-70-01. INSTALLED FASTENERS 
- [SDR TWAA0101912](https://openairdocs.org/sdr/TWAA0101912), Jan 29, 2001: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND INTERCOSTAL CORRODED, ATOP FLOORBEAM AT STA 1250, LBL 23 TO 46. REPLACED CORRODED FLOORBEAM SUPPORT AND INSTALLED FASTENERS PER SRM 
- [SDR TWAA0101911](https://openairdocs.org/sdr/TWAA0101911), Jan 29, 2001: WEB. CRACKED. DURING CHECK-C MAINT, FOUND MEMBRANE WITH 3 INCH CRACK AT LBL 50, STA 1022, BETWEEN NUMBER 1 AND 2 FLOOR TRACKS. REPAIRED CRACK AT LBL 50 INCHES, STA 1022 MEMBR

All 81: https://openairdocs.org/deregistered/N905TW-2008-06-11/reports.md

## FAA accident and incident reports (3)

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 19920721035689I](https://openairdocs.org/incident/19920721035689I), Jul 21, 1992: Doug DC982 (N905TW), West Palm Beach, FL. Unsafe left main gear indication. Made fly-by. Landed safely. Found MLG position indicator light inoperative.
- [Incident 19910806037139I](https://openairdocs.org/incident/19910806037139I), Aug 6, 1991: Doug DC982 (N905TW), Wichita, KS. Passenger had an apparent heart attack en route. Unscheduled landing at Wichita. Passenger taken to hospital.
- [Incident 19851012055929I](https://openairdocs.org/incident/19851012055929I), Oct 12, 1985: Doug DC982 (N905TW), St Louis, MO. Smoke and flames from brakes extinguished by mechanic at gate. Thrust reversers had been deferred.

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