# N926TW: 1985 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2007-05-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 10, 2007 - 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: 49356 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 8, 1997 - Certificate issued: September 23, 2004 - Last registry action: September 23, 2004 - Mode S code: ACD632 - Owner when cancelled: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC) - Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth) - Owner type: Corporation - Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N926TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=926TW - Page: https://openairdocs.org/deregistered/N926TW-2007-05-10 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 (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0202101](https://openairdocs.org/sdr/ZW0A0202101), Feb 19, 2002: BATTERY PACK. DURING ROUTINE MAINTENANCE (LS), PARTIAL EGRESS LIGHT FAILURE BETWEEN ROWS 14-19. REMOVED AND REPLACED BATTERY PACK PER MM 33-59-00. OPERATIONAL CHECK PERFORMED - [SDR ZW0A0109203](https://openairdocs.org/sdr/ZW0A0109203), Sep 24, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT THE FLOOR SEAT TRACK NUMBER 1 FROM STA 1136 TO 1218 HAD CORROSION. REPLACED SEAT TRACK SECTION FROM STA 1136 TO 1218 WITH NEW TRACK PER SRM - [SDR ZW0A0109202](https://openairdocs.org/sdr/ZW0A0109202), Sep 24, 2001: SILL. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON DOOR SILL MEMBRANE AT AFT SERVICE DOOR, STA 1138 TO 1179. REMOVED CORROSION PER SPM 6-80-01. INSTALLED SMALL DOUBLER REP - [SDR ZW0A0109201](https://openairdocs.org/sdr/ZW0A0109201), Sep 24, 2001: ATTACH FITTING. CORRODED. DURING CHECK-C MAINT THE AFT SERVICE DOOR SILL PLATE ATTACH FITTINGS, FWD AND AFT, WERE CORRODED. REMOVED CORRODED FITTINGS AND INSTALLED NEW FITTINGS PER SPM 6 - [SDR ZW0A0109105](https://openairdocs.org/sdr/ZW0A0109105), Sep 22, 2001: SKIN. CORRODED. DURING CHECK-C MAINT ON THE UPPER FUSELAGE, THE SKIN AT STA 226, LONGERON 5L, WAS OUT OF LIMITS AFTER REMOVAL OF CORROSION. INSTALLED EXTERNAL DOUBLER PER SRM 5 - [SDR ZW0A0109106](https://openairdocs.org/sdr/ZW0A0109106), Sep 21, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT THE NUMBER 1 SEAT TRACK AT LBL 44.5 INCHES HAD CORROSION FROM STA 1218 TO 1302. SPLICED IN NEW SECTION OF TRACK PER SRM 53-05, FIG 4F. - [SDR ZW0A0109104](https://openairdocs.org/sdr/ZW0A0109104), Sep 21, 2001: FLANGE. CRACKED. DURING CHECK-C MAINT THE AFT CARGO DOOR AFT MID FLANGE WAS CRACKED AT FASTENER HOLES. REPAIRED CARGO DOOR CRACK PER SRM 52-05, PAGE 110A. INSTALLED RIVETS PER S - [SDR ZW0A0109103](https://openairdocs.org/sdr/ZW0A0109103), Sep 19, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON THE NUMBER 2 SEAT TRACK, STA 1041 TO 1309, AT UPPER AND LOWER SURFACES OF FLOOR PANEL BOLT HOLES. REPLACED TRACK PER SRM - [SDR ZW0A0108901](https://openairdocs.org/sdr/ZW0A0108901), Sep 17, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND CORROSION AT UPPER SURFACE OF MEMBRANE LBL 54 INCHES, STA 1231. REMOVED CORROSION AND CUT OUT DAMAGED AREA. MADE DOUBLER AND INSTALLE - [SDR ZW0A0108810](https://openairdocs.org/sdr/ZW0A0108810), Sep 17, 2001: WEB. DAMAGED. DURING CHECK-C MAINT FOUND FLOOR MEMBRANE WAS TORN OUT AND ELONGATED HOLES FOR FASTENERS AT LBL 44 INCHES, STA 1175 TO 1191. INSTALLED MEMBRANE REPAIR PER SRM 5 - [SDR ZW0A0108809](https://openairdocs.org/sdr/ZW0A0108809), Sep 14, 2001: WEB. CRACKED. DURING CHECK-C MAINT THE AFT CABIN UPPER SURFACE OF MEMBRANE HAD CORROSION AT STA 1249 FROM LBL 47 INCHES TO LBL 56 IN, THE FLOOR MEMBRANE WAS CRACKED AT STA 12 - [SDR ZW0A0108804](https://openairdocs.org/sdr/ZW0A0108804), Sep 13, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 1155, LBL 23 INCHES TO LBL 44 INCHES. REPLACED WITH NEW PART PER SAMPLE AND SPM 6-70-1 AND DOUGLAS - [SDR ZW0A0108803](https://openairdocs.org/sdr/ZW0A0108803), Sep 13, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT BRACKET AT RBL 10 TO RBL 42, STA 180. REPLACED FLOOR SUPPORT PER SPM 6-70-01. - [SDR ZW0A0108607](https://openairdocs.org/sdr/ZW0A0108607), Sep 12, 2001: SKIN. DAMAGED. DURING CHECK-C MAINT FOUND A CLASS III REPAIR ON THE FUSELAGE AT STA 237, BETWEEN LONGERON 17L AND 18L. SKIN INSTALLED WITH CHERRY MAX RIVETS AT LONGERON 18 TO - [SDR ZW0A0108606](https://openairdocs.org/sdr/ZW0A0108606), Sep 12, 2001: ANGLE. CORRODED. DURING CHECK-C MAINT FOUND ANGLE WITH CORROSION AT STA 200, LBL 45. REPLACED CORRODED ANGLE PER SRM 51-30-02. - [SDR ZW0A0108605](https://openairdocs.org/sdr/ZW0A0108605), Sep 12, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CHAIR TRACK DAMAGED AT LBL 44 INCHES, STA 200 INSIDE TRACK. REMOVED CORROSION AND REPLACED CHAIR TRACK PER SPM 6-80-01 PAGE 2, AND SR - [SDR ZW0A0108604](https://openairdocs.org/sdr/ZW0A0108604), Sep 11, 2001: PULLEY BRACKET. CRACKED. DURING CHECK-C MAINT IN RT WHEEL WELL FOUND CRACK IN MOUNT BRACKET FOR FLAP BUS CABLE PULLEY MOUNT AT STA 994 TO 1003, BETWEEN LONGERON 20R AND 21R. ACCOMPLISHE - [SDR ZW0A0108403](https://openairdocs.org/sdr/ZW0A0108403), Sep 10, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FORMER FOOT AT LONGERON 29R TO LONGERON 29L, STA 1287. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PAINTED PER SRM 51 - [SDR ZW0A0108402](https://openairdocs.org/sdr/ZW0A0108402), Sep 10, 2001: FITTING. CRACKED. DURING CHECK-C MAINT FOUND IN LT WHEEL WELL POSSIBLE CRACK AT STA 946, KEEL BEAM AREA BETWEEN GEAR DOORS AT RBL 5 INCHES, 3 INCHES ABOVE FAIRING SUPPORTS. ACCOM - [SDR ZW0A0108401](https://openairdocs.org/sdr/ZW0A0108401), Sep 10, 2001: SUPPORT. CORRODED. DURING CHECK-C MAINT A FWD CABIN FLOOR ANGLE HAD CORROSION AT RBL 5 INCHES TO LBL 5, STA 200. FOUND CORRODED BEYOND LIMITS AND FABRICATED NEW SUPPORT. INSTALLED - [SDR ZW0A0108208](https://openairdocs.org/sdr/ZW0A0108208), Sep 6, 2001: WEB. CRACKED. DURING CHECK-C MAINT FOUND FLOOR MEMBRANE CRACKED OTBD OF RT OTBD CHAIR TRACK, STA 1271-1287. REPAIRED PER SRM 53-05, PAGE 345. - [SDR ZW0A0108207](https://openairdocs.org/sdr/ZW0A0108207), Sep 6, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT THE FLOOR SUPPORT HAD CORROSION AT STA 1212, LBL 14 TO RBL 6. REPLACED SUPPORT WITH NEW PART PER SPM 6-70-01 AND DOU - [SDR ZW0A0108206](https://openairdocs.org/sdr/ZW0A0108206), Sep 5, 2001: FITTING. CRACKED. DURING CHECK-C MAINT THE T FITTING BELOW KEEL BEAM, STA 875, WAS CRACKED. REMOVED FITTING. FABRICATED NEW FITTING AND INSTALLED PER SRM 51-10-4. - [SDR ZW0A0107303](https://openairdocs.org/sdr/ZW0A0107303), Aug 22, 2001: STUD. BACKED OUT. EXPERIENCED AN OIL LOSS ON THE NUMBER 1 ENGINE. SHUT DOWN THE ENGINE AND LANDED AT IND. FOUND OIL FILTER HOUSING STUDS HAD PULLED OUT. WAS NECESSARY TO REPLACE - [SDR ZW0A0105301](https://openairdocs.org/sdr/ZW0A0105301), Jul 17, 2001: BATTERY PACK. DURING PREFLIGHT THE FIRST CLASS EGRESS LIGHTS WERE FOUND INOP. REMOVED MOISTURE FROM EGRESS LIGHT TRACK AND REPLACED BATTERY PACK P/N 5822-2. LAST CHECK C 08/2 - [SDR ZW0A0102501](https://openairdocs.org/sdr/ZW0A0102501), May 30, 2001: BATTERY. DISCHARGED. THE EGRESS LIGHTS DID NOT COME ON FROM ROW 1 TO 7. REPLACED THE DISCHARGED BATTERY PACK P/N 5822-1, REPLACED ONE BURNED OUT LAMP P/N 36262-4, AND CLEANED MOISTU - [SDR TWAA0014002](https://openairdocs.org/sdr/TWAA0014002), Sep 8, 2000: POWER SUPPLY. INOPERATIVE. THE EGRESS LIGHTS WERE ON ALL THE TIME AT ROW 16 TO 20. REPLACED THE POWER SUPPLY. CHECK-C 8-20-00 STL. - [SDR TWAA0010702](https://openairdocs.org/sdr/TWAA0010702), Jul 9, 2000: BATTERY PACK. DISCHARGED. THE FWD HALF OF THE CABIN HAD THE EGRESS LIGHTS FAIL. REPLACED BATTERY PACK. CHECK-C 8-28-99 JFK. - [SDR TWAA0003605](https://openairdocs.org/sdr/TWAA0003605), Mar 6, 2000: LIGHT. CONTAMINATED. FIRST CLASS EGRESS FLOOR TRACK CONTAMINATED WITH FLUID. REMOVED FC FLOOR HARNESS ASSY, CLEANED CONTAMINATION. REINSTALLED FC FLOOR HARNESS ASSY. AC02 01-12-00 D - [SDR TWAA9908706](https://openairdocs.org/sdr/TWAA9908706), Jun 22, 1999: LIGHT. MALFUNCTIONED. THE CABIN EGRESS LIGHTS AT ROWS 6 TO 16 WERE ILLUMINATED REGARDLESS OF SWITCH POSITION. RECYLED THE EGRESS LIGHT SYSTEM. CHECK-C 10-18-98 STL. - [SDR TWAA9908701](https://openairdocs.org/sdr/TWAA9908701), Jun 22, 1999: BATTERY PACK. DISCHARGED. THE CABIN EGRESS LIGHTS FROM ROWS 6 TO 16 CAME ON IN FLIGHT. DURING TROUBLESHOOTING FOUND THE FORWARD CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE NUMBER - [SDR TWAA9817503](https://openairdocs.org/sdr/TWAA9817503), Oct 29, 1998: BATTERY PACK. DISCHARGED. THE FLOOR EGRESS LIGHTS AT ROW 29 FORWARD KEPT CYCLING ON AND OFF WITH SWITCH IN THE ARMED POSITION. REPLACED BATTERY PACK AT ROW 24. CHECK-C 10-10-98 STL. ---- - [SDR TWAA9817502](https://openairdocs.org/sdr/TWAA9817502), Oct 29, 1998: CONNECTOR. LOOSE. THE EGRESS LIGHTS AT CABIN ROW 29 FORWARD KEPT COMING ON AND OFF. TIGHTENED CONNECTOR AT THE POWER SUPPLY. CHECK-C 10-10-98 STL. ---CLOSED--- - [SDR TWAA9714903](https://openairdocs.org/sdr/TWAA9714903), Dec 17, 1997: RECEIVER. FAILED. STL - FLT 284 - DURING CRUISE, NR 1 VOR FAILED. REPLACED FOR RECEIVER MFG PN 42-607-1. NEW AIRCRAFT. (X) ## 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 20010822021019I](https://openairdocs.org/incident/20010822021019I), Aug 22, 2001: Doug DC982 (N926TW), Indianapolis, IN. (-23) On 08/22/01, twa flight 731 while enroute bdl to stl, the #1 engine oil quantity decreased to zero, followed by low oil pressure light and loss of… --- 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.