# N902TW: 1983 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2008-02-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 4, 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: 49153
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 19, 1983
- Last registry action: March 24, 2006
- Mode S code: AC7858
- 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/N902TW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=902TW
- Page: https://openairdocs.org/deregistered/N902TW-2008-02-04

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 (49)

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

- [SDR ZW0A0201301](https://openairdocs.org/sdr/ZW0A0201301), Jan 28, 2002: ATTACH ANGLE. CRACKED. DURING CHECK-C FWD LT DORSAL FIN ATTACH ANGLE, .5 INCH CRACK WAS FOUND ON UPPER LEG VERIFIED WITH EDDY CURRENT. INSTALLED NEW ATTACH ANGLE PER SRM 51-30-02, 51-
- [SDR ZW0A0107902](https://openairdocs.org/sdr/ZW0A0107902), Sep 1, 2001: BATTERY PACK. DISCHARGED. THE EMERGENCY LIGHT IN THE TAIL CONE AND WALKWAY, AND THE CABIN EMERGENCY LIGHT IN THE CEILING AT THE AFT FLIGHT ATTENDANT SEAT AREA, WERE INOPERATIVE. REPLACED
- [SDR ZW0A0106901](https://openairdocs.org/sdr/ZW0A0106901), Aug 15, 2001: WIRE. BROKEN. ON ARRIVAL AT THE GATE THE LEADING EDGE SLATS WOULD NOT RETRACT. REPLACED BROKEN FLAP BUS WIRE, RUN 208B. REFERENCE IPC 27-30-00 FIGURE 2B ITEM 32. CHECK-C 2-5-
- [SDR ZW0A0102402](https://openairdocs.org/sdr/ZW0A0102402), May 29, 2001: POWER SUPPLY. DISCHARGED. THE EMERGENCY LIGHTS DID NOT COME ON IN HALF OF THE FIRST CLASS SECTION. REPLACED THE POWER SUPPLY. CHECK-C 2-5-01 STL.
- [SDR TWAA0018501](https://openairdocs.org/sdr/TWAA0018501), Nov 28, 2000: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHT AT THE TAIL CONE COMPARTMENT AND THE EMERGENCY LIGHTS AT ROWS 7 TO 10 WERE INOPERATIVE. REPLACED THE LAMP, P/N 1315, FOR THE TAIL COMPT, AND
- [SDR TWAA0011502](https://openairdocs.org/sdr/TWAA0011502), Jul 22, 2000: BATTERY. DISCHARGED. THE LT AND RT FWD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 10-25-00 MCI.
- [SDR TWAA0007502](https://openairdocs.org/sdr/TWAA0007502), May 13, 2000: SWITCH. STUCK. AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. CREW FOLLOWED GEAR HANDLE LOCKED PROCEDURE BUT GEAR HANDLE RELEASE BUTTON INEFFECTIVE. CREW LEFT GEAR DOWN AN
- [SDR TWAA0005802](https://openairdocs.org/sdr/TWAA0005802), Apr 3, 2000: SKIN. CRACKED. DURING C CHECK MAINT FOUND SKIN CRACKED AT FAIRING ATTACH HOLE, LOWER FUSELAGE STA 772, ABOVE LONGERON 29 RT, AND CORROSION AT STA 762 TO 772, LONGERON 28 RT TO
- [SDR TWAA0005304](https://openairdocs.org/sdr/TWAA0005304), Mar 30, 2000: DOUBLER. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON LOWER FWD SIDE OF PRESSURE BULKHEAD DOUBLER, RT OF CENTER LINE. REMOVED AND REMANUFACTURED DOUBLER PER SRM 53-14-3, FIG
- [SDR TWAA0005303](https://openairdocs.org/sdr/TWAA0005303), Mar 30, 2000: RIB. CRACKED. DURING CHECK-C MAINT, THE RT WING LEADING EDGE RIB WAS CRACKED INSIDE PANEL 1211R BEHIND NUMBER 5 SLAT. REMOVED AND REPLACED RIB PER SPM 6-70-02. INSTALLED FAST
- [SDR TWAA0004904](https://openairdocs.org/sdr/TWAA0004904), Mar 22, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, THE FLOOR SUPPORT AT STA 160 TO 200, RBL 45 HAD CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SPM 6-70-01.
- [SDR TWAA0004814](https://openairdocs.org/sdr/TWAA0004814), Mar 21, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON CABIN FLOOR SUPPORT BEAM, STA 1250, LBL 24 TO 40. FLOORBEAM WAS CORRODED BEYOND LIMITS. FABRICATED NEW FLOORBEAM, INSTA
- [SDR TWAA0004707](https://openairdocs.org/sdr/TWAA0004707), Mar 21, 2000: SEAT TRACK. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON SEAT TRACK NUMBER 2, IN TRACK AND SCREW HOLES FOR FLOOR PANEL AT STA 1170 TO 1309. REMOVED CORROSION BY INSTALLING NEW 
- [SDR TWAA0004706](https://openairdocs.org/sdr/TWAA0004706), Mar 21, 2000: TRACK. CORRODED. DURING CHECK-C MAINT, THE MID CARGO BIN BETWEEN STA 769 AND 789 THE RT TRACK WAS CORRODED IN SEVERAL LOCATIONS. INSTALLED NEW TRACK PER SRM 6-70-01, PAGE 1.
- [SDR TWAA0004807](https://openairdocs.org/sdr/TWAA0004807), Mar 20, 2000: WINDOW POST. CUT. DURING CHECK-C MAINT, FOUND WINDOW BELT FRAMES WITH LIGHT CUTS AND SCRATCHES IN FOLLOWING LOCATIONS; LT 22, 46, 45, 44, 42, 43, 24, RT 23, RT AFT EXIT, RT FWD E
- [SDR TWAA0004705](https://openairdocs.org/sdr/TWAA0004705), Mar 20, 2000: CHANNEL. CORRODED. DURING CHECK-C MAINT, IN THE C3 CARGO COMPT FOUND CORROSION AT STA 1212 TO 1210, BETWEEN LONGERON 30 TO 29R ON U CHANNEL. REMOVED AND REPLACED U CHANNEL PER SPM
- [SDR TWAA0004604](https://openairdocs.org/sdr/TWAA0004604), Mar 20, 2000: SKIN. CRACKED. DURING CHECK-C MAINT, THE C3 CARGO DOOR FWD LOWER CORNER OF THE DOOR SKIN, 14 INCHES UP FROM THE BOTTOM EDGE, HAD 4 EACH BENDS. STRENGHTENED ONE AREA. THREE ARE
- [SDR TWAA0004812](https://openairdocs.org/sdr/TWAA0004812), Mar 17, 2000: FRAME. CORRODED. DURING CHECK-C MAINT, IN THE AFT CARGO COMPT FOUND CORROSION AFT SIDE OF FRAME, STA 1271 STRINGER 29L. REMOVED CORROSION BY FABRICATION OF NEW DOUBLER PER SRM 5
- [SDR TWAA0004811](https://openairdocs.org/sdr/TWAA0004811), Mar 17, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR SUPPORT, STA 180, RBL 8 TO 56. REMOVED AND REPLACED CORRODED PART PER SPM 6-70-01.
- [SDR TWAA0004810](https://openairdocs.org/sdr/TWAA0004810), Mar 15, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT, THE RT WING T/E UPPER WING T/E PANEL LOWER SURFACE WAS DELAMINATED ABOVE THE O/B FLAP, O/B IDLER HINGE. REMOVED AND REPLACED WITH NEW PART
- [SDR TWAA0004809](https://openairdocs.org/sdr/TWAA0004809), Mar 15, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT, THE RT WING T/E LOWER SURFACE OF THE WING, UPPER T/E PANEL WAS DELAMINATED AT AILERON QUADRANT. REMOVED AND REPLACED WITH NEW (P/N 172779)
- [SDR TWAA0004808](https://openairdocs.org/sdr/TWAA0004808), Mar 15, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON LOWER SIDE OF THE FLOOR SUPPORT AROUND FASTENERS, STA 708 TO 712, RBL 8. REMOVED CORROSION, TREATED AND PRIMED METAL AN
- [SDR TWAA0004806](https://openairdocs.org/sdr/TWAA0004806), Mar 14, 2000: BRACE. CRACKED. DURING CHECK-C MAINT, THE AFT PRESSURE BULKHEAD, FWD RT SIDE DIAGONAL BRACE WAS CRACKED IN RADIUS UPPER END LONGERON 3R TO 4R, STA 1338. INSTALLED NEW BRACE PER
- [SDR TWAA0004815](https://openairdocs.org/sdr/TWAA0004815), Mar 11, 2000: SUPPORT BRACKET. CORRODED. DURING CHECK-C MAINT, THE FWD ENTRY DOOR SILL MOUNT SUPPORT WAS CORRODED, STA 160 TO 200, LBL 55. REMOVED CORRODED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED
- [SDR TWAA0004214](https://openairdocs.org/sdr/TWAA0004214), Mar 5, 2000: BOLT. CORRODED. DURING CHECK-C MAINT, FOUND RUSTED HUCK BOLT ON TOP OF WINDOW FRAME BETWEEN STA 636 AND 655. CLEANED RUST FROM FASTENER AND TREATED PER SPM 6-80-01, PAGE 1.
- [SDR TWAA0004213](https://openairdocs.org/sdr/TWAA0004213), Mar 5, 2000: BOLT. CORRODED. DURING CHECK-C MAINT, FOUND RUSTED HUCK BOLTS AT STA 826, LONGERON 17L. REMOVED RUST FROM HUCK BOLT PER SPM 6-80-01.
- [SDR TWAA0004212](https://openairdocs.org/sdr/TWAA0004212), Mar 5, 2000: BOLT. CORRODED. DURING CHECK-C MAINT, FOUND THREE RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 294 AND 313. REPLACED FASTENERS PER MM 56-20-00.
- [SDR TWAA0004211](https://openairdocs.org/sdr/TWAA0004211), Mar 5, 2000: BOLT. CORRODED. DURING CHECK-C MAINT, FOUND RUSTED BOLT ON WINDOW FRAME BETWEEN STA 788 AND 807. REPLACED RUSTED BOLT PER SRM 51-30-0.
- [SDR TWAA0004206](https://openairdocs.org/sdr/TWAA0004206), Mar 5, 2000: FASTENER. CORRODED. DURING CHECK-C MAINT, FOUND RUSTED FASTENER AT STA 712, LONGERON 15L. CLEANED RUST FROM FASTENER AND REPLACED NUT AND WASHER.
- [SDR TWAA0004205](https://openairdocs.org/sdr/TWAA0004205), Mar 5, 2000: NUT. CORRODED. DURING CHECK-C MAINT, FOUND RUSTED NUT ON LONGERON 10L AT STA 332. CHANGED NUT AND WASHER PER SPM 6-30-07.
- [SDR TWAA0004204](https://openairdocs.org/sdr/TWAA0004204), Mar 5, 2000: FASTENER. CORRODED. DURING CHECK-C MAINT, FOUND RUSTED FASTENER AT STA 712, LONGERON 15L. CLEANED RUST FROM FASTENER AND REPLACED NUT AND WASHER PER SPM 6-30-07.
- [SDR TWAA0004203](https://openairdocs.org/sdr/TWAA0004203), Mar 5, 2000: BOLT. CORRODED. DURING CHECK-C MAINT, FOUND THREE RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 693 AND 712. REMOVED 3 RUSTED BOLTS AND INSTALLED 3 NEW BOLTS AND WASHERS PER SPM 6-3
- [SDR TWAA0004202](https://openairdocs.org/sdr/TWAA0004202), Mar 5, 2000: BOLT. CORRODED. DURING CHECK-C MAINT, FOUND THREE RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 769 AND 788. REPLACED RUSTED BOLTS PER SRM 51-30-0.
- [SDR TWAA0004210](https://openairdocs.org/sdr/TWAA0004210), Mar 4, 2000: BOLT. CORRODED. DURING CHECK-C MAINT, FOUND THREE RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 541 AND 560. REMOVED 3 BOLTS AND INSTALLED 3 NEW BOLTS AND WASHERS PER SPM 6-30-07.
- [SDR TWAA0004209](https://openairdocs.org/sdr/TWAA0004209), Mar 4, 2000: BOLT. CORRODED. DURING CHECK-C MAINT, FOUND FOUR RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 579 AND 598. REMOVED 4 RUSTED BOLTS AND INSTALLED 4 NEW BOLT AND WASHERS PER SPM 6-30-
- [SDR TWAA0004208](https://openairdocs.org/sdr/TWAA0004208), Mar 4, 2000: BOLT. CORRODED. DURING CHECK-C MAINT FOUND RUSTED BOLT ON WINDOW FRAME BETWEEN STA 503 AND 522. REMOVED 1 RUSTED BOLT AND INSTALLED 1 NEW BOLT AND WASHER PER SPM 6-30-07.
- [SDR TWAA0004207](https://openairdocs.org/sdr/TWAA0004207), Mar 4, 2000: BOLT. CORRODED. DURING CHECK-C MAINT, FOUND RUSTED BOLT ON WINDOW FRAME BETWEEN STA 446 AND 465. REMOVED 2 RUSTED BOLTS AND INSTALLED 2 NEW BOLTS AND WASHERS PER SPM 6-30-07.
- [SDR TWAA0003930](https://openairdocs.org/sdr/TWAA0003930), Mar 3, 2000: STRINGER. CORRODED. DURING CHECK-C MAINT, FOUND IN THE CABIN, STRINGER 15R ANGLE WAS CORRODED ON AFT SIDE AT STA 1005. FABRICATED NEW PART PER SPM 6-70-01, PAGE 2 AND 3, PARAGRAPH 
- [SDR TWAA9908002](https://openairdocs.org/sdr/TWAA9908002), Jun 4, 1999: SWITCH. OUT OF POSITION. THE EGRESS LIGHTING CAME ON WITH EMERGENCY LIGHT SWITCH IN THE OFF POSITION. CHECKS WERE MADE TO VERIFY THE PERFORMANCE OF THE SYSTEM. UNABLE TO DUPLICATE THE R
- [SDR TWAA9811801](https://openairdocs.org/sdr/TWAA9811801), Jul 21, 1998: LIGHT. INOPERATIVE. THE AFT EGRESS LIGHT STRIP, AFT OF LAST PAX SEAT, WAS INOP AND COVER BROKEN. REPAIRED LIGHT STRIP AND REPLACED LIGHT COVER, CHECK-C 2-1-98 STL. (M)
- [SDR TWAA9811502](https://openairdocs.org/sdr/TWAA9811502), Jul 14, 1998: SKIN. BENT. DURING OVERNIGHT MAINTENANCE, FOUND THE L-1 CABIN DOOR LOWER FORWARD CORNER OF DOOR SKIN BENT INWARD 9 INCHES. AREA CUT OUT, FILLER AND DOUBLER INSTALLED PER SR
- [SDR TWAA9810101](https://openairdocs.org/sdr/TWAA9810101), Jun 22, 1998: OIL PUMP. LEAKING. IN FULL COLD POSN LT AIR COND PACK REPORTED TO CAUSE OILY BURNING SMELL AND MADE CABIN APPEAR FOGGY. CREW WENT TO MANUAL AND SMELL AND FOG WENT AWAY. THE LT AND
- [SDR TWAA9804303](https://openairdocs.org/sdr/TWAA9804303), Mar 24, 1998: COMPRESSOR. STALLED. RNO - FLT 224 - ABORTED TAKEOFF AT 100 KTS DUE TO COMPRESSOR STALLS ON RT ENGINE. FOUND COMPRESSOR BLADES DAMAGED FROM APPARENT ICE INGESTION. (M)
- [SDR TWAA9802202](https://openairdocs.org/sdr/TWAA9802202), Feb 11, 1998: BATTERY PACK. DISCHARGED. STL - FLT 30 - THE EGRESS LIGHTING CAME ON IN-FLIGHT BETWEEN ROWS 15 AND 21. REPLACED BATTERY PACK. CHECK-C ON 1-25-98 STL. (X)
- [SDR TWAA9802001](https://openairdocs.org/sdr/TWAA9802001), Feb 2, 1998: LONGERON. DAMAGED. STL - DURING OP-9 MAINTENANCE CHECK, THE LOWER LONGERON LEG WAS FOUND DAMAGED AT L23 STATION 1366 AT APU AREA. REPAIRED L23 PER ARA 12000. (M)
- [SDR TWAA9712701](https://openairdocs.org/sdr/TWAA9712701), Oct 23, 1997: SLIDE. DEPLOYED. STL - WHILE PARKED AT THE GATE THE TAILCONE EMERGENCY ESCAPE SLIDE WAS INADVERTENTLY DEPLOYED BY SECURITY PERSONNEL. THE SLIDE FUNCTIONED PROPERLY. REMOVED AND 
- [SDR TWAA9613301](https://openairdocs.org/sdr/TWAA9613301), Oct 31, 1996: CONNECTOR. CORRODED. STL - ABORTED TAKEOFF AT 50 KNOTS DUE TO A WHEEL NOT TURNING LIGHT ILLUMINATION. CLEANED CORROSION FROM THE ANTI-SKID VALVE CONNECTOR. OPERATIONAL CHECK NORMAL.
- [SDR 96ZZZM1074](https://openairdocs.org/sdr/96ZZZM1074), Jun 9, 1996: COMPRESSOR. STALLED. SLC - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO COMPRESSOR STALLS. FOUND METAL PARTICLES IN ENGINE BLEED AIR DUCT AND CAPS. CHANGED ENGINE. ENGINE OPERATION TH
- [SDR 96ZZZX1202](https://openairdocs.org/sdr/96ZZZX1202), Feb 20, 1996: JAMB. CORRODED. MCI - DURING OP-15, FOUND CORROSION ON AFT CARGO DOOR JAMB LOWER BEAM. REPLACED BEAM PER SRM 51-01, PAGE 1, ITEM C. AIRCRAFT TT: 39,822 HRS; 20,932 CYCLES.

## FAA accident and incident reports (4)

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 20000605033639I](https://openairdocs.org/incident/20000605033639I), Jun 5, 2000: Doug DC982 (N902TW), Cedar Rapids, IA, Minor damage. (-23)Pilot requested a missed approach. On second attempt aircraft departed runway surface at about 3,700 feet from approach end of runway nine at Cedar…
- [Incident 19950630024329I](https://openairdocs.org/incident/19950630024329I), Jun 30, 1995: Doug DC982 (N902TW), Baltimore, MD, Minor damage. Near right main tire blew. Aborted takeoff. Engine injested casing stopping engine. Emergency evacuated.
- [Incident 19920630028899I](https://openairdocs.org/incident/19920630028899I), Jun 30, 1992: Doug DC982 (N902TW), Wichita, KS. Passenger became ill with seizures en route. Diverted to Wichita. Passenger deplaned and received medical attention
- [Incident 19851213066379I](https://openairdocs.org/incident/19851213066379I), Dec 13, 1985: Doug DC982 (N902TW), St Louis, MO. Engine failed on takeoff roll. Nose accessory case with bullet attached ingested by engine.

## Other aircraft with N902TW

- [Registered now](https://openairdocs.org/aircraft/N902TW): Costruzioni Aeronautiche Tecna P2008, S/N 136, built 2017

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