# N928TW: 1991 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2013-03-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 26, 2013 - Status when cancelled: Sale reported, canceled - 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: 48012 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: November 24, 1999 - Last registry action: May 31, 2006 - Mode S code: ACDDA0 - Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City) - Owner type: Individual - Owner's area on the map: 39.1483° N, 94.6051° W: Placed by OpenAirDocs at the center of ZIP code 66115, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N928TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=928TW - Page: https://openairdocs.org/deregistered/N928TW-2013-03-26 From the FAA registry file of November 5, 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 (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0300301](https://openairdocs.org/sdr/ZW0A0300301), Jan 6, 2003: WARNING SYSTEM. ACTIVATED. WHEN THE LANDING GEAR WAS EXTENDED FOR APPROACH THE NOSE GEAR RED LIGHT STAYED ILLUMINATED. CREW DID A TOWER FLY BY THEN RECYCLED THE LANDING GEAR. THE INDICATI - [SDR TWAA0106209](https://openairdocs.org/sdr/TWAA0106209), Apr 2, 2001: BEAM. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT, THE LOWER CARGO DOOR BEAM HAD CORROSION. REMOVED AND REPLACED BEAM PER DOUGLAS PRINT 5930483, SRM 51-30-5, SRM 51-3 - [SDR TWAA0105911](https://openairdocs.org/sdr/TWAA0105911), Mar 23, 2001: BULKHEAD. CORRODED. DURING CHECK-C MAINT AT THE AFT LT LAVATORY, CORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD, STA 1338 FROM CUSP TO LONGERON 21L. REMOVED CORROSION. INSTALLED - [SDR TWAA0105508](https://openairdocs.org/sdr/TWAA0105508), Mar 23, 2001: FRAME. CORRODED. DURING CHECK-C MAINT AT LT AFT LAV FOUND CORROSION ON FORE AND AFT SIDES OF FORMER, STA 1338, FROM CUSP TO LONGERON 21L. REMOVED CORROSION AND INSTALLED REPAIR - [SDR TWAA0104914](https://openairdocs.org/sdr/TWAA0104914), Mar 15, 2001: BEAM. CORRODED. DURING OP 16 MAINT CHECK IN MID CARGO COMPT, THE LOWER DOOR BEAM HAD CORROSION REMOVAL GROUND BELOW 25 PERCENT AT STA 646. REPAIRED BEAM. - [SDR TWAA0104911](https://openairdocs.org/sdr/TWAA0104911), Mar 14, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 210, RBL 10. FABRICATED NEW FLOOR SUPPORT AND INSTALLED. - [SDR TWAA0104910](https://openairdocs.org/sdr/TWAA0104910), Mar 14, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CABIN NUMBER 2 CHAIR TRACK HAD CORROSION GROUND BEYOND LIMITS AT STA 1034 TO 1308. REPLACED SEAT TRACK FROM STA 1032 TO 1308. - [SDR TWAA0105003](https://openairdocs.org/sdr/TWAA0105003), Mar 13, 2001: LONGERON. CORRODED. DURING CHECK-C MAINT IN THE FWD CARGO COMPT, LONGERON 28L AT STA 294 WAS CORRODED. FABRICATED PARTS PER SRM 53-02. FINISHED REPAIR BY INSTALLING HI-LOKS PER SRM - [SDR TWAA0104803](https://openairdocs.org/sdr/TWAA0104803), Mar 13, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINTENANCE FOUND CABIN FLOOR TRACK AT LBL 45 INCHES HAD MATERIAL REMOVED BEYOND LIMITS ON CORROSION REMOVAL, STA 1088 TO 1127. REPLACED TRACK FR - [SDR TWAA0104802](https://openairdocs.org/sdr/TWAA0104802), Mar 13, 2001: WEB. CRACKED. DURING CHECK-C MAINTENANCE, THE CABIN FLOOR MEMBRANE HAD A HOLE WITH CRACK EMITTING FROM THE HOLE AT LBL 8.5 IN AND STA 180. ACCOMPLISHED EDDY CURRENT INSPECTIO - [SDR TWAA0104709](https://openairdocs.org/sdr/TWAA0104709), Mar 12, 2001: SKIN. TOOL DAMAGE. DURING CHECK-C MAINT FOUND HI-SPEED CUT IN FUSELAGE SKIN IN FWD CARGO BIN SIDE OF SKIN, STA 285, LONGERON 28L. WIDENED CUTOUT FROM 2.625 INCHES TO 4.25 INCHES. - [SDR TWAA0104708](https://openairdocs.org/sdr/TWAA0104708), Mar 12, 2001: SKIN. CORRODED. DURING CHECK-C MAINT FOUND IN THE FWD CARGO BIN FUSELAGE SKIN METAL WAS REMOVED BEYOND LIMITS ON CORROSION REMOVAL, LONGERON 28L, STA 285 THRU 298. SEALED FILLE - [SDR TWAA0104703](https://openairdocs.org/sdr/TWAA0104703), Mar 8, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT IN THE FWD CABIN, CORROSION WAS FOUND ON FLOOR SUPORT AT STA 218, BL ZERO, LBL 18 IN. FABRICATED NEW FLOOR SUPPORT, INSTALLED. - [SDR TWAA0104503](https://openairdocs.org/sdr/TWAA0104503), Mar 7, 2001: CASTING. CRACKED. DURING CHECK-C MAINT, CASTINGS WERE CRACKED APPROXIMATELY STA 69, 16 INCHES TO RT OF BL AND 16 INCHES TO LT OF BL, IN CEILING AREA OF NOSE GEAR WELL. REPLACED C - [SDR TWAA0104202](https://openairdocs.org/sdr/TWAA0104202), Mar 1, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FORMER FRAME AT STA 1212, LONGERON 18R. REMOVED CORROSION PER SPM 6-80-01. REPLACED FASTENERS PER SRM 51-01. - [SDR TWAA0104201](https://openairdocs.org/sdr/TWAA0104201), Mar 1, 2001: CLIP. CORRODED. DURING CHECK-C MAINT ON RT INTERCOSTAL CLIP AT LONGERON 15R, STA 1003, FOUND CORROSION. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PRIMED AREA PER SRM 51-10 - [SDR TWAA9914001](https://openairdocs.org/sdr/TWAA9914001), Oct 11, 1999: BATTERY. DISCHARGED. THE FIRST CLASS CABIN EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 2-2-99 MCI. - [SDR TWAA9913601](https://openairdocs.org/sdr/TWAA9913601), Oct 4, 1999: POWER SUPPLY. INOP. FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE, AND LAST ROW OF EGRESS LIGHTS WERE FLASHING WHEN SYSTEM WAS ARMED. REPLACED THE FORWARD CABIN POWER SUPPLY, AN - [SDR TWAA9801602](https://openairdocs.org/sdr/TWAA9801602), Jan 31, 1998: GYRO. FAILED. MCI - FLT 347 - ABORTED TAKEOFF, CAPTAIN'S ATTITUDE INDICATOR FAILED. REPLACED INDICATOR AND DIMMER CONTROL. ABORTED TAKEOFF SECOND TIME WITH CAPTAIN'S ATTITUDE ## 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 20020712037199I](https://openairdocs.org/incident/20020712037199I), Jul 12, 2002: Doug DC982 (N928TW), Washington, DC, Minor damage. (-23) AA3153 was a ferry flight originating at dca and dispatched to STC. It was parked at hardstand 2P on the south side of the airport. At 1550L it taxied… --- 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.