# N9413T: 1995 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2013-09-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 27, 2013 - Exported to: Ukraine - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083) - 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: 53188 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 27, 1995 - Certificate issued: November 9, 1995 - Last registry action: October 26, 2012 - Mode S code: AD13B2 - Owner when cancelled: [Wilmington Trust Company Owner Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20OWNER%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N9413T - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9413T - Page: https://openairdocs.org/deregistered/N9413T-2013-09-27 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-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md ## Service difficulty reports (58, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA20130518003](https://openairdocs.org/sdr/AALA20130518003), May 17, 2013: BATTERY. INOPERATIVE. EMERGENCY LIGHTS ABOVE SEATS 28D THROUGH 32D INOPERATIVE. RESEATED THE BATTERIES IN THE POWER SUPPLY. OPS CHECK NORMAL - [SDR AALA20121018013](https://openairdocs.org/sdr/AALA20121018013), Oct 17, 2012: PORTABLE LIGHT. INOPERATIVE. LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NUMBER 1 DOOR PORTABLE LIGHT. OPS CHECK NORMAL. - [SDR AALA20121018012](https://openairdocs.org/sdr/AALA20121018012), Oct 17, 2012: BATTERY. NOT SEATED. CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 26 INOPERATIVE. RESEATED BATTERIES AT ROW 25. OPS CHECK NORMAL. - [SDR AALA20121018010](https://openairdocs.org/sdr/AALA20121018010), Oct 17, 2012: WIRE. DAMAGED. ESCAPE PATH LIGHT AT SEAT 22D INOPERATIVE. REPAIRED WIRING FOR ESCAPE PATH LIGHT AT SEAT 22D. OPS CHECK NORMAL. - [SDR AALA20120207TUL05](https://openairdocs.org/sdr/AALA20120207TUL05), Feb 7, 2012: SKIN. DAMAGED. DENT AND SCRATCHES IN FUSELAGE SKIN STATION 464 ABOVE LONGERON 21 RIGHT. DYE CHECKED AND NO CRACKS FOUND. FABRICATED AND INSTALLED CLASS III DOUBLER PER SRM 53- - [SDR AALA20120207TUL04](https://openairdocs.org/sdr/AALA20120207TUL04), Feb 7, 2012: SKIN. DAMAGED. DENT AND GOUGE IN FUSELAGE SKIN STATION 241 BETWEEN STRINGERS 21 AND 22 LEFT. DYE CHECKED AND NO CRACKS FOUND. INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 02. - [SDR AALA20120206TUL06](https://openairdocs.org/sdr/AALA20120206TUL06), Feb 6, 2012: CUSP WEB. CORRODED. LEFT CUSP FROM STATIONS 1171 TO 1176 CORRODED. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16. - [SDR AALA20120206TUL05](https://openairdocs.org/sdr/AALA20120206TUL05), Feb 6, 2012: CUSP WEB. DAMAGED. TOOLING MARK ON CUSP AT STATION 864 LEFT UNDER HORSECOLLAR. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16. - [SDR AALA20120206TUL04](https://openairdocs.org/sdr/AALA20120206TUL04), Feb 6, 2012: MEMBRANE. CORRODED. STATIONS 160 TO 200 CORRODED BELOW INBOARD LEG OF FORWARD SERVICE DOOR AREA FLOORBOARD SUPPORT. INSTALLED NEW SUBFLOOR AND OVERLAY DOUBLER PER AARD 53-20-00-16. - [SDR AALA20120131TUL10](https://openairdocs.org/sdr/AALA20120131TUL10), Jan 31, 2012: DOOR. DAMAGED. EXTERIOR SKIN ON MID CARGO DOOR HAS SEVERAL AREAS OF DAMAGE. REMOVED AND REPLACED OUTER SKIN ON MID CARGO DOOR PER ESO 80174. - [SDR AALA20120127TUL17](https://openairdocs.org/sdr/AALA20120127TUL17), Jan 27, 2012: CUSP WEB. CORRODED. AFT GALLEY SERVICE DOOR JAMB HAS CORROSION ON CUSP UNDER FORWARD AND AFT GIRT BAR SUPPORTS. INSTALLED DOUBLERS PER AARD 53-20-00-16. - [SDR AALA20111114TUL05](https://openairdocs.org/sdr/AALA20111114TUL05), Nov 14, 2011: DUCT. FAILED. BNA - INFLIGHT PHL-DFW. CREW REPORTED TAIL TEMPERATURE OVERHEAT LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT DIVERTED BNA LANDED WITHOUT INCIDENT. AIRCRAFT REMO - [SDR AALA20101222TUL01](https://openairdocs.org/sdr/AALA20101222TUL01), Dec 21, 2010: ENGINE. OVERTEMP. BHM INFLIGHT DFW-ATL - CREW REPORTED RIGHT ENGINE OIL TEMP INDICATION CLIMBED IN EXCESS OF 190 DEGREES. RIGHT ENGINE WAS SHUTDOWN IN FLIGHT (SINGLE ENGINE TIME - [SDR AALA20100908DFW01](https://openairdocs.org/sdr/AALA20100908DFW01), Sep 7, 2010: BOOT. CRACKED. DFW - CREW REPORTED CABIN BEGAN TO DEPRESSURIZE DURING FLIGHT. INICIATED EMERGENCY DESCENT TO 8,000 FT. THE FLIGHT ATTENDANT REPORTED A LOUD AIR LEAK FROM THE A - [SDR AALA20100722TUL11](https://openairdocs.org/sdr/AALA20100722TUL11), Jul 22, 2010: FRAME. CRACKED. FRAME 1418 CRACKED AT LONGERON 2 RIGHT. INSTALLED DOUBLER IAW EA MD80-53-011690. - [SDR AALA2009052700973](https://openairdocs.org/sdr/AALA2009052700973), May 27, 2009: BATTERY PACK. DISCHARGED. SFO - BOTH AFT LEFT AND RIGHT OVERWING EXIT DOORS OVERHEAD EXIT LIGHT DIMS THEN BRIGHTENS. REPLACED BATTERY PACK AT B5-105 POSITION. - [SDR AALA2009021100059](https://openairdocs.org/sdr/AALA2009021100059), Jan 31, 2009: LONGERON. CRACKED. LONGERON 2 LEFT CRACKED AT STATION 1418. INSTALLED SPLICE PER AARD 53-30-00-2. - [SDR AALA2009021100058](https://openairdocs.org/sdr/AALA2009021100058), Jan 31, 2009: STRINGER. CRACKED. LONGERON 2 RIGHT CRACKED AT STATION 1418. INSTALLED SPLICE PER AARD 53-30-00-2. - [SDR AALA2009020900041](https://openairdocs.org/sdr/AALA2009020900041), Jan 30, 2009: BEAM. CRACKED. HORIZONTAL BEAM CRACKED UNDER INBOARD SUPPORT BOLT. THIRD BEAM UP AT FORWARD ENTRY DOOR. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH AARD 52-10-00-3. - [SDR AALA2009020900040](https://openairdocs.org/sdr/AALA2009020900040), Jan 30, 2009: SKIN. CRACKED. AFT SERVICE DOOR SKIN CRACKED AT HOLD OPEN HOOK CUTOUT. INSTALLED DOUBLER ON AFT SERVICE DOOR IN ACCORDANCE WITH SRM 52 05 00 FIGURE 54 SHEET 1. - [SDR AALA2009020900039](https://openairdocs.org/sdr/AALA2009020900039), Jan 30, 2009: FRAME. CRACKED. FRAME 1418 CRACKED AT STRINGER 2 RIGHT AT FORWARD SIDE AND AFT SIDE AT STIFFENER. - [SDR AALA200802439A](https://openairdocs.org/sdr/AALA200802439A), Oct 30, 2008: BATTERY PACK. DISCHARGED. SFO - AFT EMERGENCY LIGHTS ABOVE LEFT AND RIGHT AFT OVERWING ESCAPE HATCH INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS OVERHEAD RIGHT AND LEFT AF - [SDR AALA200801364](https://openairdocs.org/sdr/AALA200801364), May 22, 2008: BATTERY PACK. DISCHARGED. SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT 25D AFT TO TAIL CONE INOPERATIVE. CHARGED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 25D AFT TO TAIL CONE. SYSTEM - [SDR AALA200801363](https://openairdocs.org/sdr/AALA200801363), May 22, 2008: CONNECTOR. BROKEN. SFO - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) - [SDR AALA200800422](https://openairdocs.org/sdr/AALA200800422), Feb 27, 2008: BATTERY PACK. INOPERATIVE. LAX - OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5 125 FOR OVERWING EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERA - [SDR AALA20070196](https://openairdocs.org/sdr/AALA20070196), Jan 27, 2007: CONNECTOR. DISCONNECTED. SFO - FOUND EMERGENCY LIGHTS AT SEAT 28D INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20060845](https://openairdocs.org/sdr/AALA20060845), Oct 9, 2006: BATTERY. INOPERATIVE. LAS - EMERGENCY FLASHLIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED FLASHLIGHT BATTERIES FOR EMERGENCY FLASHLIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKE - [SDR AALA20050666](https://openairdocs.org/sdr/AALA20050666), Oct 12, 2005: BATTERY PACK. INOPERATIVE. IAH - COCKPIT AND GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT AND GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20041157](https://openairdocs.org/sdr/AALA20041157), Nov 22, 2004: CONNECTOR. DISCONNECTED. STL - EMERGENCY PATH LIGHTS AT SEAT 14DEF INOPERATIVE. FOUND CONNECTOR DISCONNECED AT SIDEWALL SEAT 14DEF. RECONNECTED CONNECTOR FOR EMERGENCY PATH LIGHTS AT SE - [SDR AALA20040687](https://openairdocs.org/sdr/AALA20040687), Jun 29, 2004: BATTERY PACK. INOPERATIVE. DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT IN AFT HALF OF CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR FORWARD AND AFT SEAT MOUNTED EMERGENCY ESCAPE PATH L - [SDR AALA20040334](https://openairdocs.org/sdr/AALA20040334), Mar 10, 2004: SOCKET. INOPERATIVE. STL - EMERGENCY EXIT LIGHT AT SEAT 24D INOPERATIVE. REPLACED SOCKET FOR EMERGENCY EXIT LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20040321](https://openairdocs.org/sdr/AALA20040321), Mar 5, 2004: CONNECTOR. LOOSE. DFW - EMERGENCY LIGHT AT SEAT ROW 19 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20040320](https://openairdocs.org/sdr/AALA20040320), Mar 5, 2004: BATTERY. INOPERATIVE. EMERGENCY LIGHT IN TAIL CONE AREA INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR EMERGENCY LIGHT IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20031330](https://openairdocs.org/sdr/AALA20031330), Nov 25, 2003: LIGHT. INOPERATIVE. DTW FRONT ENTRY EMERGENCY EXIT LIGHT UPPER LOCK BROKEN. REPLACED FRONT ENTRY EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR ZW0A0206402](https://openairdocs.org/sdr/ZW0A0206402), Jun 16, 2002: ACM. LEAKING. A BURNING ODOR WAS IN CABIN AND COCKPIT ON DESCENT. NO SMOKE. FOUND RT ACM OIL PUDDLING IN ACM OUTLET. THE NEXT STATION REPLACED THE RT ACM. - [SDR ZW0A0202201](https://openairdocs.org/sdr/ZW0A0202201), Feb 21, 2002: COMPUTER. THE CAPTAIN'S IAS INDICATOR FROZE AT 180 KNOTS ON CLIMB OUT. CREW MADE AN UNSCHEDULED LANDING AT MCI. REPLACED THE CAPTAIN'S AIR SPEED INDICATOR, PN 4057800-906 - [SDR ZW0A0105001](https://openairdocs.org/sdr/ZW0A0105001), Jul 12, 2001: ENGINE. MALFUNCTIONED. A LOUD NOISE WAS HEARD FROM THE LT ENGINE AND THE AIRCRAFT SHUTTERED. SMOKE APPEARED IN THE COCKPIT. ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED AT SZL. EMERGENCY - [SDR ZW0A0101603](https://openairdocs.org/sdr/ZW0A0101603), May 10, 2001: LIGHT. INOPERATIVE. THE EGRESS LIGHT AT SEAT 8D WAS INOPERATIVE DURING TEST. REPLACED THE LAMP. CHECK-C 12-3-00 JFK. - [SDR TWAA0019701](https://openairdocs.org/sdr/TWAA0019701), Dec 17, 2000: GCU. FAILED. IN CRUISE FLIGHT WITH RT GEN INOPERATIVE THE APU GEN TRIPPED OFF LINE. THE LT GEN BECAME ERRATIC AND FAILED TO PICK UP THE LOAD, FOLLOWED BY LT AC BUS REPEATEDL - [SDR TWAA0002903](https://openairdocs.org/sdr/TWAA0002903), Feb 21, 2000: COVER. MISSING. THE RED EGRESS LIGHT COVER WAS MISSING AT CABIN ROW 30. REPLACED THE RED COVER. CHECK-C 8-11-99 MCI. - [SDR TWAA9913608](https://openairdocs.org/sdr/TWAA9913608), Sep 23, 1999: BATTERY. DISCHARGED. THE EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 3, 5, 19, 21, AND 22. REPLACED THE LAMP, MFG PN 1315, FOR ROWS 3 AND 5, AND REPLACED THE BATTERY FOR REMAINING ROW - [SDR TWAA9910903](https://openairdocs.org/sdr/TWAA9910903), Jul 28, 1999: SKIN. DENTED. DURING CHECK-C MAINT, FOUND .5 INCH BY 0.080 DEEP AND .4375 INCH LONG BY 0.076 DEEP DENTS IN SKIN AT STA 1193, LONGERON 20L. TWO DENTS WITHIN .5 INCH OF EACH OT - [SDR TWAA9910902](https://openairdocs.org/sdr/TWAA9910902), Jul 27, 1999: LONGERON. MISREPAIRED. DURING CHECK-C MAINT, A 9 INCH BY 9 INCH CLASS 3 REPAIR, FOUND INSTALLED WITH BLIND FASTENERS AT STA 256, WL 209 AND LONGERON 17L, WAS DAMAGED. REPAIRED LONGERO - [SDR TWAA9910707](https://openairdocs.org/sdr/TWAA9910707), Jul 26, 1999: SKIN. GOUGED. DURING CHECK-C MAINT, FOUND FUSELAGE SKIN GOUGED AT STA 217, STRINGER 5L AND 6L. AN INTERIM REPAIR HAD BEEN INSTALLED PER ARA 15461. REPAIRED PER SRM 53-04, FIG - [SDR TWAA9910706](https://openairdocs.org/sdr/TWAA9910706), Jul 25, 1999: SKIN. MISREPAIRED. DURING CHECK-C MAINT, FOUND FUSELAGE SKIN REPAIR INSTALLED WITH BLIND FASTENERS AT STA 229 TO 245, STRINGER 18L. REPAIRED PER SRM 53-04, FIG 12B, WITH SOLID FAS - [SDR TWAA9907606](https://openairdocs.org/sdr/TWAA9907606), May 31, 1999: COVER. MISSING. DURING PREFLIGHT INSPECTION FOUND ESCAPE PATH LIGHTING COVER MISSING. REPLACED COVER. CC-01 9-1-98 STL. - [SDR TWAA9905702](https://openairdocs.org/sdr/TWAA9905702), Apr 17, 1999: COVER. MISSING. THE EGRESS LIGHTS AT AFT CABIN WAS MISSING THE COVER AND THE RED LENS. REPLACED THE COVER 0105601-003PA40, LAMP 7732, LEN 0105607-301, AND THE END PIECE 015609- - [SDR TWAA9904901](https://openairdocs.org/sdr/TWAA9904901), Apr 1, 1999: WIRE. LOOSE. THE EGRESS LIGHT AT CABIN ROW 2 HAD WIRE LOOSE FROM THE LIGHT AND THE COVER WAS MISSING. REPLACED THE WIRE SEGMENT AND INSTALLED COVER. CHECK-C 9-1-98 STL. - [SDR TWAA9903902](https://openairdocs.org/sdr/TWAA9903902), Mar 12, 1999: LAMP. LOOSE. FOUND EGRESS LIGHTS INOPERATIVE ON TEST AT ROW 21 TO 24, AND ROW 3. SECURED A LOOSE LIGHT SOCKET AT ROW 24, AND INSTALLED A LOOSE LAMP AT ROW 3. CHECK-C 9-1-98 - [SDR TWAA9819005](https://openairdocs.org/sdr/TWAA9819005), Nov 29, 1998: WIRE. WORN. FOUND EMERGENCY EGRESS LIGHT COVER STRIP MISSING AT CABIN ROW 17. REPLACED COVER (P/N 5778-1), AND LIGHT CABLE. CHECK -C 9-1-98 STL. All 58: https://openairdocs.org/deregistered/N9413T-2013-09-27/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CHI01IA211](https://openairdocs.org/ntsb/CHI01IA211), Jul 12, 2001: McDonnell Douglas MD-83 (N9413T), Whiteman AFB, MO, incident, minor damage. Probable cause: The separation of a fan blade due to fatigue failure which led to case separation and loss of engine power in the left engine. ## FAA accident and incident reports (2) 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 20010712016619I](https://openairdocs.org/incident/20010712016619I), Jul 12, 2001: Doug DC983 (N9413T), Knob Noster, MO, Minor damage. (-23) During cruise flight, the aircraft experienced a sudden vibration along with the #1 engine surging and smoke in the cockpit. The flight crew declared an… - [Incident 20001218025149I](https://openairdocs.org/incident/20001218025149I), Dec 18, 2000: Doug DC983 (N9413T), Billings, MT. (-23) A/c operating with right generator on MEL, using APU and left generators. Flight crew report: at cruise, FL330, the APU generator tripped off line and… ## Other aircraft with N9413T - [Cancelled 1988-12-01](https://openairdocs.org/deregistered/N9413T-1988-12-01): Cessna 210, S/N 57213. N-number assigned, not yet registered --- 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.