# N923TW: Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2012-01-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 5, 2012 - Status when cancelled: Registration pending - 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: 49379 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 14, 1997 - Last registry action: December 1, 2011 - Mode S code: ACCB0D - Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie) - Owner type: Individual - Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N923TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=923TW - Page: https://openairdocs.org/deregistered/N923TW-2012-01-05 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 (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0110301](https://openairdocs.org/sdr/ZW0A0110301), Oct 29, 2001: LIGHT. MALFUNCTIONED. THE EGRESS LIGHTING SYSTEM FLICKERED IN FLIGHT. UNABLE TO DUPLICATE THE PROBLEM. OPERATIONAL CHECKED NORMAL. - [SDR ZW0A0109602](https://openairdocs.org/sdr/ZW0A0109602), Oct 15, 2001: BATTERY. DISCHARGED. THE EMERGENCY LIGHTS IN THE TAIL COMPT FOR CHUTE AND CAT WALK WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER PACK. CHECK-C 8-10-01 MCI. - [SDR ZW0A0105707](https://openairdocs.org/sdr/ZW0A0105707), Jul 23, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT AT STA 1145 TO 1221, LBL 16 IN, THE LT TIE DOWN TRACK WAS CORRODED IN NUMEROUS LOCATIONS ALONG TRACK. INSTALLED TIE DOWN TRACK STA 1150 TO - [SDR ZW0A0105706](https://openairdocs.org/sdr/ZW0A0105706), Jul 23, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT IN THE AFT ACCY COMPT THE LONGERON END WAS CRACKED AT STA 1418, LONGERON 2L. REPLACED CRACKED LONGERON PER SRM 53-14-4, FIG 2. REPAIRED WIT - [SDR ZW0A0105705](https://openairdocs.org/sdr/ZW0A0105705), Jul 22, 2001: CARGO TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FROM STA 1041 TO 1145, AT LBL 16, THE LT TIE DOWN TRACK WAS CORRODED IN NUMEROUS LOCATIONS ALONG THE TRACK. - [SDR ZW0A0105704](https://openairdocs.org/sdr/ZW0A0105704), Jul 18, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN THE FWD CABIN FOUND FLOOR SUPPORT WITH CORROSION AT STA 168, RBL 10. INSTALLED NEW FLOOR SUPPORT WITH HLT 436 HI-LOKS, A SUBSTITUTION FO - [SDR ZW0A0105410](https://openairdocs.org/sdr/ZW0A0105410), Jul 18, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 147 TO 167, LBL 5 TO LBL 10. CUT OUT TWO AREAS OF CORROSION. REMOVED REMAINING CORROSION PER SPM 6-80-01 - [SDR ZW0A0105404](https://openairdocs.org/sdr/ZW0A0105404), Jul 17, 2001: SPAR CAP. CRACKED. DURING CHECK-C MAINT FOUND EYEBROW CRACK IN RT WING UPPER SPAR CAP AT OTBD FLAP HINGE INBD GUIDE PIN. INSTALLED DOUGLAS REPAIR DOUBLER PER DRAWING JO60272-501 A - [SDR ZW0A0105306](https://openairdocs.org/sdr/ZW0A0105306), Jul 16, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN FLOOR SUPPORT FASTENER HOLES, STA 160 TO 200, RBL 45. REPLACED FLOOR SUPPORT WITH P/N S2929169 EXTRUSION. - [SDR ZW0A0105011](https://openairdocs.org/sdr/ZW0A0105011), Jul 12, 2001: GUSSET. CORRODED. DURING CHECK-C MAINT FOUND GUSSET ON FORMER RING FACTORY SPLICE WAS CORRODED, STA 1193. REPLACED PART PER SRM 51-01 AND DRAWING 9936073. - [SDR ZW0A0105010](https://openairdocs.org/sdr/ZW0A0105010), Jul 12, 2001: GUSSET. CORRODED. DURING CHECK-C MAINT FOUND GUSSET ON TOP OF FORMER CORRODED, STA 1155 AND LBL 28. REPLACED CORRODED STRAP WITH NEW ONE PER DRAWING 9936067. - [SDR ZW0A0105008](https://openairdocs.org/sdr/ZW0A0105008), Jul 12, 2001: SKIN. PUNCTURED. DURING CHECK-C MAINT FOUND PUNCTURE HOLE IN LT WING L/E APPROX 8 INCHES FWD OF FRONT SPAR, 13 INCHES AFT AND OTBD OF NUMBER 1 SLAT ANTI-ICE TUBE ON LT WING L/E. - [SDR ZW0A0105007](https://openairdocs.org/sdr/ZW0A0105007), Jul 12, 2001: FRAME. CRACKED. DURING CHECK-C MAINT FOUND CANTED FORMER CRACKED, LOWER END OF STA 1485, OTBD OF STAIR CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 53-01 FIG 2. INSTALL - [SDR ZW0A0105204](https://openairdocs.org/sdr/ZW0A0105204), Jul 11, 2001: FITTING. CRACKED. DURING CHECK-C, A FORMER FOOT WAS FOUND CRACKED IN THE AFT ACCY COMPARTMENT AT STATION 1451 BETWEEN NR 1 AND NR 3 LEFT LONGERON. REPLACED FORMER FOOT WITH P/N 9 - [SDR ZW0A0105203](https://openairdocs.org/sdr/ZW0A0105203), Jul 11, 2001: WEB. DAMAGED. DURING CHECK C-FOUND MEMBRANE AT STATION 1231 ON LEFT SIDE OF CABIN DAMAGED BY ARCING POWER LEADS. REPAIRED PER SRM 53-01 PAGE 14 AND SRM 51-30-01. MCI - [SDR ZW0A0105009](https://openairdocs.org/sdr/ZW0A0105009), Jul 11, 2001: GUSSET. CORRODED. DURING CHECK-C MAINT FOUND FACTORY GUSSET ON TOP OF FORMER SPLICE CORRODED, STA 1174 AND LBL 30. REPLACED CORRODED STRAP WITH NEW ONE PER DRAWING 9936073. - [SDR ZW0A0105202](https://openairdocs.org/sdr/ZW0A0105202), Jul 10, 2001: ANGLE. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION ON THE ANGLE IN THE FWD LOWER CORNER OF THE DOOR JAM. REMOVED AND REPLACED CORNER ANGLE AND INSTALLE - [SDR ZW0A0105201](https://openairdocs.org/sdr/ZW0A0105201), Jul 10, 2001: THRESHOLD. CORRODED. DURING CHECK-C MAINT FOUND IN THE AFT CARGO COMPT THE BOTTOM OF THE DOOR THRESHOLD WAS CORRODED FROM STA 1162 TO 1205. REMOVED SPACER. FABRICATED NEW SPACER PER - [SDR ZW0A0105113](https://openairdocs.org/sdr/ZW0A0105113), Jul 10, 2001: ANGLE. CORRODED. DURING CHECK-C MAINT IN AFT CARGO COMPT FOUND CORROSION ON ANGLE IN AFT LOWER CORNER OF DOOR JAM. REMOVED AND REPLACED CORNER ANGLE AND INSTALLED HI-LOKS PER SR - [SDR ZW0A0105112](https://openairdocs.org/sdr/ZW0A0105112), Jul 10, 2001: FRAME. CRACKED. DURING CHECK-C MAINT FOUND AFT ACCY COMPT CANTED FORMER CRACKED AT LOWER END AT STA 1474, OTBD OF STAIR CUTOUT ON RT SIDE. REPAIRED PER SRM 53-01 PAGE 10. MATER - [SDR ZW0A0104905](https://openairdocs.org/sdr/ZW0A0104905), Jul 9, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CHAIR TRACK CORROSION AT STA 1030 TO 1211 LBL 22 INCHES, STA 1079 TO 1136 LBL 22 INCHES, STA 1136 AND LBL 22 INCHES, AND HOLES DRILLE - [SDR ZW0A0102002](https://openairdocs.org/sdr/ZW0A0102002), May 20, 2001: BATTERY PACK. DISCHARGED. THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 1 TO 10, AND ROW 18 TO 22. REPLACED THE BATTERY PACK FOR ROW 1 TO 10, AND REPAIRED A BROKEN WIRE FOR ROW 18 TO 22. C - [SDR TWAA0017604](https://openairdocs.org/sdr/TWAA0017604), Nov 9, 2000: LIGHT. INOPERATIVE. THE RT AFT AIRSTAIRS EMERGENCY SIDEWALL LIGHT, EMERGENCY EXIT MARKER FWD OF THE FWD CARGO DOOR, EMERGENCY OVERHEAD LIGHT ROWS 12 TO 18, AND THE FIRST CLASS EGRE - [SDR TWAA0016003](https://openairdocs.org/sdr/TWAA0016003), Oct 13, 2000: BATTERY. WORN. THE EGRESS LIGHTS WERE INOPERATIVE IN THE TAIL COMPARTMENT. REPLACED THE BATTERIES IN THE BATTERY PACK B5-27 AND B5-28. CHECK-C 6-9-00 JFK. - [SDR TWAA0006201](https://openairdocs.org/sdr/TWAA0006201), Apr 21, 2000: LIGHT. INOPERATIVE. THE FWD CABIN EGRESS LIGHTS WERE INOPERATIVE. CLEANED MOISTURE FROM EGRESS LIGHT TRACK. CHECK-C 8-3-99 STL. - [SDR TWAA9912601](https://openairdocs.org/sdr/TWAA9912601), Sep 8, 1999: BATTERY. DISCHARGED. THE TAIL CONE SLIDE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY. CHECK-C 8-3-99 STL. - [SDR TWAA9911201](https://openairdocs.org/sdr/TWAA9911201), Aug 15, 1999: BATTERY PACK. DISCHARGED. GREEN EMERGENCY ESCAPE LIGHT STRIP, MID CABIN, STAYS ILLUMINATED WITHOUT ACTIVATION RIGHT SIDE. REPLACED BATTERY PACK AT OVERWING POSITION. CHECK C 07-26-99 STL - [SDR TWAA9907402](https://openairdocs.org/sdr/TWAA9907402), May 24, 1999: FAN. FAILED. DURING PRE-FLIGHT, A STRONG ODOR WAS NOTED THROUGHOUT THE AIRCRAFT. THE PASSENGERS WERE REMOVED FROM THE AIRCRAFT SAFELY. THE RADIO STANDBY COOLING FAN WAS THE - [SDR TWAA9711401](https://openairdocs.org/sdr/TWAA9711401), Sep 17, 1997: OVEN. DIRTY. RNO - FLT 235 - DURING CRUISE, THE NR 1 GALLEY EMITTED SMOKE. CLEANED DEBRIS FROM THE INSIDE OF OVEN. OPERATIONAL CHECK NORMAL. OP16 - 6-18-97. (X) - [SDR TWAA9715001](https://openairdocs.org/sdr/TWAA9715001), Mar 31, 1997: GEN CONTROL. FAILED. STL - FLT 1058 - ON TAKEOFF ROLL, LOST RIGHT AC AND RIGHT DC BUSSES. ALSO, HAD A CROSS TIE LOCKOUT. REPLACED RT GENERATOR CONTROL MFG PN 976J254-4. (M) ## FAA accident and incident reports (1) 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 20020324009419I](https://openairdocs.org/incident/20020324009419I), Mar 24, 2002: Doug DC982 (N923TW), Omaha, NE. (-23) Aircraft landed on runway 32L, reported braking action poor. Aircraft turned off at taxiway 'w' and slid nose wheel into grass. Aircraft continued to… --- 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.