# N912TW: 1983 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2007-03-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 13, 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: 49183 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: December 13, 1983 - Certificate issued: December 11, 2006 - Last registry action: December 11, 2006 - Mode S code: AC9FD7 - 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/N912TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=912TW - Page: https://openairdocs.org/deregistered/N912TW-2007-03-13 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 (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0305601](https://openairdocs.org/sdr/ZW0A0305601), Jul 4, 2003: PRESSURE SWITCH. FAULTY. DURING CLIMB FAILURE OF FILTER CLOG LIGHT OF RIGHT ENGINE ILLUMINATED. MADE UNSCHEDULED LANDING AT IAD AT IDLG AND DID NOT SHUT DOWN ENGINE. REMOVED OIL FILTER - [SDR ZW0A0302701](https://openairdocs.org/sdr/ZW0A0302701), Feb 21, 2003: LIGHT. INOPERATIVE. DURING OVERNITE PS CHECK AFT WALKWAY CTR CHUTE LITE INOP. REPLACED LAMP WITH BULB OPS CHECK PER 33-53-00. CHECK-C STL 11-27-02. --CLOSED-- - [SDR ZW0A0200502](https://openairdocs.org/sdr/ZW0A0200502), Jan 10, 2002: FRAME. CORRODED. DURING CHECK-C MAINT FOUND CORROSION AT STA 1271, AFT FACE OF FORMER LONGERON 29L TO 29R. REPAIRED FORMER PER SRM 53-03, FIG 2A. - [SDR ZW0A0200501](https://openairdocs.org/sdr/ZW0A0200501), Jan 9, 2002: SPLICE. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON STA 1309 FORMER REPAIR SPLICE, AFT SIDE BETWEEN LONGERON 29L AND 29R. REPLACED FORMER REPAIR SPLICE PER SRM 53-03, FIG 2 - [SDR ZW0A0200405](https://openairdocs.org/sdr/ZW0A0200405), Jan 5, 2002: SEAT TRACK. CORRODED. DURING CHECK-C MAINT IN THE FWD CABIN FOUND CHAIR TRACK CORRODED AT RBL 44, STA 201 TO 237. REPLACED CHAIR TRACK STA 201 TO 237 PER SPM 6-70-01, AND SRM 53-04 F - [SDR ZW0A0200404](https://openairdocs.org/sdr/ZW0A0200404), Jan 3, 2002: FRAME. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT, STA 1231, THE AFT FACE OF FORMER 29L TO 29R HAD CORROSION. REPLACED SECTION OF FORMER WITH NEW. CUT AND SPLICED AT - [SDR ZW0A0200403](https://openairdocs.org/sdr/ZW0A0200403), Jan 2, 2002: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT BETWEEN STA 693 AND 712, LONGERON 29L, THE BOTTOM FLANGE OF INTERCOSTAL WAS CORRODED. INSTALLED NEW INTERCOSTAL WITH NEW FASTENERS PER SRM - [SDR ZW0A0200402](https://openairdocs.org/sdr/ZW0A0200402), Dec 27, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE MID CARGO COMPT, STA 540 TO 560 LT TIE DOWN TRACK WAS CORRODED. REMOVED AND REPLACED TRACK PER SPM 6-70-01. - [SDR ZW0A0200401](https://openairdocs.org/sdr/ZW0A0200401), Dec 27, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE FWD CARGO COMPT THE LT HOLD DOWN TRACK HAD LIGHT TO HEAVY CORROSION, STA 365 TO 446. REMOVED AND REPLACED TRACK PER SRM 51-10-2. - [SDR ZW0A0200103](https://openairdocs.org/sdr/ZW0A0200103), Dec 26, 2001: STRUCTURE. CORRODED. DURING CHECK-C, CABIN FLOOR MEMBRANE HAD CORROSION ON FLOOR PANEL STA 148, RBL 30, MEMBRANE UNDER -A- GALLEY FLOOR DRAIN CORRODED FITTING, CORROSION MEMBRANE ST - [SDR ZW0A0200101](https://openairdocs.org/sdr/ZW0A0200101), Dec 21, 2001: ATTACH ANGLE. CORRODED. DURING CHECK-C MAINT THE FWD SERVICE DOOR AFT LOWER CORNER HAD CORROSION ON ATTACH ANGLE INSIDE 1.5 INCH BY 2.5 INCHES AT LIGHTENING HOLE. REMOVED CORROSION PER - [SDR ZW0A0200102](https://openairdocs.org/sdr/ZW0A0200102), Dec 20, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE MID CARGO COMPT THE LT TIE DOWN TRACK HAD SEVERAL CORRODED AREAS, STA 598 TO 788. REMOVED AND REPLACED TRACK PER SRM 51-10-3 AND 53- - [SDR ZW0A0112209](https://openairdocs.org/sdr/ZW0A0112209), Dec 18, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT IN THE MAIN CABIN THE LT INBOARD FLOOR TRACK WAS CORRODED AT STA 1135 TO 1308. REMOVED AND REPLACED TRACK PER SPM 6-70-01, SRM 51-10-3, 51- - [SDR ZW0A0112208](https://openairdocs.org/sdr/ZW0A0112208), Dec 18, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT THE MAIN CABIN FLOOR TRACK WAS CORRODED AT LBL 44, STA 1136 TO 1308. REMOVED AND REPLACED TRACK PER SPM 6-70-01, SRM 51-10-3, 51-30-2, 51-3 - [SDR ZW0A0112207](https://openairdocs.org/sdr/ZW0A0112207), Dec 18, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN AFT CARGO COMPT ON FORMER AT STA 1322, BETWEEN LONGERON 29L AND 29R. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 53-0 - [SDR ZW0A0112205](https://openairdocs.org/sdr/ZW0A0112205), Dec 18, 2001: ATTACH ANGLE. CRACKED. DURING CHECK-C MAINT THE RT FWD SERVICE DOOR INTERNAL HAD CRACKED ATTACH ANGLE, INSIDE UPPER 9 INCH BY 6 INCH LIGHTENING HOLE OF DOOR. FABRICATED AND INSTALLED - [SDR ZW0A0112211](https://openairdocs.org/sdr/ZW0A0112211), Dec 16, 2001: SKIN. DAMAGED. DURING CHECK-C MAINT FOUND EXTERNAL DOUBLER INSTALLED WITH BLIND FASTENERS AT STA 285, LONGERON 23L. INSTALLED SRM REPAIR PER 53-04, FIG 12B. - [SDR ZW0A0112206](https://openairdocs.org/sdr/ZW0A0112206), Dec 15, 2001: LONGERON. CORRODED. DURING CHECK-C MAINT FOUND CORROSION BETWEEN STA 1042 AND 1072, LONGERON 30, AROUND FASTENER HOLES IN LONGERON, SEVERAL LOCATIONS. REMOVED CORROSION AROUND FAST - [SDR ZW0A0112204](https://openairdocs.org/sdr/ZW0A0112204), Dec 14, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN MID CARGO COMPT THE FLOOR SUPPORT INTERCOSTAL WAS CORRODED AT STA 769 TO 788, BETWEEN LONGERON 28L TO 27L. REMOVED AND REPLACED CORRODED - [SDR ZW0A0112203](https://openairdocs.org/sdr/ZW0A0112203), Dec 14, 2001: FLOORBEAM. CORRODED. DURING CHECK-C MAINT ON CABIN FLOOR, FOUND CORROSION ON FLOORBEAM AT STA 1338, RBL 56. MADE CLIP PER SAMPLE AND DRAWING 9930612. - [SDR ZW0A0112202](https://openairdocs.org/sdr/ZW0A0112202), Dec 14, 2001: CLIP. CRACKED. DURING CHECK-C MAINT FOUND CRACK AT AFTER BODY BULKHEAD, RT SIDE, AT BASE OF MOUNT BRACKET FOR RUDDER TRIM ACTUATOR. REPLACED CLIP PER SPM 6-70-01. - [SDR ZW0A0112201](https://openairdocs.org/sdr/ZW0A0112201), Dec 14, 2001: FRAME. CORRODED. DURING CHECK-C MAINT IN THE MID CARGO COMPT, STA 540 LONGERON 28L TO 28R, THE AFT FACE OF THE FORMER HAD CORROSION. REMOVED CORROSION PER SRM 51-10-3 AND SPM 6- - [SDR ZW0A0112103](https://openairdocs.org/sdr/ZW0A0112103), Dec 13, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT THE FLOOR AT LBL 55 WAS CORRODED AT SEVERAL AREAS, STA 1106 TO 1190. REPLACED TRACK AT STA 1106 TO 1190 PER SRM 51-10-3, 51-30-1 AND 51-30- - [SDR ZW0A0112102](https://openairdocs.org/sdr/ZW0A0112102), Dec 13, 2001: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT THE AFT CARGO COMPT, AN INTERCOSTAL WAS CORRODED AT STA 1148 TO 1155, LONGERON 29R TO 30. REMOVED CORRODED PART. INSTALLED SERVICEABLE PART - [SDR ZW0A0112006](https://openairdocs.org/sdr/ZW0A0112006), Dec 11, 2001: SUPPORT. CRACKED. DURING CHECK-C MAINT, IN THE FWD CARGO COMPT FOUND A 1/2 INCH CRACK EMANATING FROM EACH SIDE OF RIVET HOLE WHERE AFT BULKHEAD VERTICAL SUPPORT MOUNTS TO CEILING - [SDR ZW0A0112005](https://openairdocs.org/sdr/ZW0A0112005), Dec 10, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT THE FWD CARGO COMPT FLOOR SUPPORT WAS CORRODED AT STA 427, LBL 15 TO RBL 12. REPLACED SUPPORT PER SRM 53-01. - [SDR ZW0A0112301](https://openairdocs.org/sdr/ZW0A0112301), Dec 7, 2001: GUSSET. CRACKED. DURING CHECK-C MAINT FOUND CRACK IN RT MAIN LANDING GEAR AFT INBOARD DOOR FRAME GUSSET. FABRICATED NEW GUSSET PER DRAWING 5936395. INSTALLED PER SRM 51-30. - [SDR ZW0A0112004](https://openairdocs.org/sdr/ZW0A0112004), Dec 7, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT THE TIE DOWN TRACK HAD CORROSION AT STA 1127 TO 1140, LBL 34 TO LBL 37. INSTALLED NEW TRACK. - [SDR ZW0A0112003](https://openairdocs.org/sdr/ZW0A0112003), Dec 7, 2001: FLOORBEAM. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON TOP OF FLOOR BEAM CAP AT STA 1250 FROM LBL 24 TO LBL 43. REMOVED PART AND REMOVED CORROSION PER SPM 6-80-01. INSTALLED P - [SDR ZW0A0111902](https://openairdocs.org/sdr/ZW0A0111902), Dec 6, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT THE FLOOR SUPPORT WAS CORRODED AT STA 1155, LBL 22 TO LBL 44. REMOVED AND REPLACED CORRODED PART PER SPM 6-70-01, PAGE 1. - [SDR ZW0A0111801](https://openairdocs.org/sdr/ZW0A0111801), Nov 29, 2001: WEDGE. DAMAGED. DURING CHECK-C MAINT THE RT WING T/E FLAP, OTBD END OF THE OTBD AFT FLAP HAD DAMAGE TO THE T/E WEDGE. REPAIRED T/E WEDGE PER SRM 57-09, FIG 45. - [SDR TWAA0000503](https://openairdocs.org/sdr/TWAA0000503), Dec 3, 1999: SILL. CORRODED. DURING CHECK-C MAINT, THE LOWER FRAME AT THE AFT CARGO DOOR SILL HAD CORROSION GROUND BEYOND LIMITS. REPLACED THE FRAME PER SPM 6-70-01, PAGE 1. - [SDR TWAA9810503](https://openairdocs.org/sdr/TWAA9810503), Jul 1, 1998: LIGHT. SMOKING. STL - FLT 603 - DURING TAKEOFF, CABIN ATTENDANT NOTICED SMOKE AT OVERHEAD GALLEY LIGHT. REPLACED LAMP. SUSPECTED OVEN RESIDUE. (M) - [SDR TWAA9805503](https://openairdocs.org/sdr/TWAA9805503), Nov 17, 1997: SKIN. DENTED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN FUSELAGE SKIN FS 219 STR 17L. DENT IS OVER PREVIOUS DAMAGE REPAIR. REPAIRED AREA AS REQUIRED PER DC9 MD80 SS - [SDR TWAA9615901](https://openairdocs.org/sdr/TWAA9615901), Dec 21, 1996: PROX SENSOR. FAILED. STL - FLT 29 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR. FOUND LEFT MAIN LANDING GEAR - [SDR 96ZZZM787](https://openairdocs.org/sdr/96ZZZM787), Mar 24, 1996: PROX COMPUTER. FAILED. AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLE LANDING GEAR, FOUND INTERNAL MALFUNCTIO - [SDR 96ZZZX1236](https://openairdocs.org/sdr/96ZZZX1236), Feb 3, 1996: FUEL CONTROL. FAILED. STL - FLT 296 - DURING APPROACH, NR 2 ENGINE, SN 3232, SPUN DOWN. COMPLETED SHUTDOWN CHECKLIST. FOUND INTERNAL MALFUNCTION IN FUEL CONTROL, MFG PN 769606-16. RE ## FAA accident and incident reports (5) 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 19881222069089I](https://openairdocs.org/incident/19881222069089I), Dec 22, 1988: Doug DC982 (N912TW), Wichita, KS. Odor of fuel in cabin. Diverted to Wichita, landed without incident. Cause of odor not given. - [Incident 19880504019679I](https://openairdocs.org/incident/19880504019679I), May 4, 1988: Doug DC982 (N912TW), St Louis, MO. Right engine failed with a loud noise on climbout. Returned. Turbine had failed causing exhaust cone to tear away. - [Incident 19860414022999I](https://openairdocs.org/incident/19860414022999I), Apr 14, 1986: Doug DC982 (N912TW), St Louis, MO. Loss of right hydraulic system fluid en route. Safe landing. Ruptured o ring in brake accumulator. - [Incident 19851127065049I](https://openairdocs.org/incident/19851127065049I), Nov 27, 1985: Doug DC982 (N912TW), St Louis, MO. Tail compartment overheat warning light came on. Returned. Left augmentation clamp in compartment loose. - [Incident 19850822045199I](https://openairdocs.org/incident/19850822045199I), Aug 22, 1985: Doug DC982 (N912TW), Kansas City Int, MO. Smoke and fumes in cockpit and cabin. Diverted where maintenance replaced oven in galley. Timer was defective. ## Other aircraft with N912TW - [Registered now](https://openairdocs.org/aircraft/N912TW): Kubicek Factory S R O BB26AZ, S/N 2223, built 2023 --- 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.