# N410EA: 1977 Mcdonnell Douglas DC-9-51, registration cancelled 2005-06-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 9, 2005 - Exported to: Swaziland - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-51](https://openairdocs.org/model/mcdonnell-douglas-dc-9-51) (registry code 3022051) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47731 - Year built: 1977 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 12, 1977 - Certificate issued: April 29, 2002 - Last registry action: September 16, 2003 - Mode S code: A4D485 - Owner when cancelled: [Boeing Capital Loan Corp](https://openairdocs.org/faa-owner/BOEING%20CAPITAL%20LOAN%20CORP) - Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas) - Owner type: Corporation - Owner's area on the map: 36.0845° N, 115.1461° W: Placed by OpenAirDocs at the center of ZIP code 89119, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N410EA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=410EA - Page: https://openairdocs.org/deregistered/N410EA-2005-06-09 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-9-51: https://openairdocs.org/model/mcdonnell-douglas-dc-9-51.md ## Service difficulty reports (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR WXOA00009](https://openairdocs.org/sdr/WXOA00009), Sep 21, 2000: POWER SUPPLY. INOPERATIVE. FAT - DURING SCHEDULED MAINTENANCE, CABIN EMERGENCY FLOOR PATHWAY LIGHTING SYSTEM FAILED TO ILLUMINATE AT SECOND POWER SUPPLY STATION. MAINTENANCE REPLACED EMER - [SDR WX0A00007](https://openairdocs.org/sdr/WX0A00007), Aug 17, 2000: POWER SUPPLY. FAILED. FAT - DURING SCHEDULED MAINTENANCE, TAILCONE EMERGENCY LIGHTING SYSTEM FAILED TO ILLUMINATE. MAINTENANCE REPLACED EMERGENCY LIGHT POWER SUPPLY. TAILCONE EMERGEN - [SDR WX0A00006](https://openairdocs.org/sdr/WX0A00006), Aug 16, 2000: BULB. FAILED. LGB - DURING FAA RAMP INSPECTION, TAILCONE EMERGENCY LIGHTING SYSTEM FAILED TO ILLUMINATE. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED BULBS. TAIL - [SDR WX0A00005B](https://openairdocs.org/sdr/WX0A00005B), Aug 14, 2000: BULB. FAILED. FAT - DURING SCHEDULED MAINTENANCE, TAILCONE EMERGENCY LIGHTING SYSTEM FAILED TO ILLUMINATE. MAINTENANCE REPLACED BULBS AND BATTERIES. TAILCONE EMERGENCY LIGHT - [SDR WX0A00005A](https://openairdocs.org/sdr/WX0A00005A), Aug 14, 2000: BATTERY. DISCHARGED. FAT - DURING SCHEDULED MAINTENANCE, TAILCONE EMERGENCY LIGHTING SYSTEM FAILED TO ILLUMINATE. MAINTENANCE REPLACED BULBS AND BATTERIES. TAILCONE EMERGENCY LIGHT - [SDR WX0A00001](https://openairdocs.org/sdr/WX0A00001), Jun 22, 2000: SPAR. CRACKED. FAT - DURING ACCOMPLISHMENT OF CARD 4027 .5 INCH CRACK DETECTED AT RIGHT WING REAR SPAR LOWER CAP AT THE NR 2 FLAP HINGE ATTACH BRACKET. AIRCRAFT FERRIED TO MHV - [SDR TWAA9903408](https://openairdocs.org/sdr/TWAA9903408), Feb 28, 1999: LONGERON. CRACKED. FOUND THE INBD FLANGE OF LONGERON 5R CRACKED .25 INCH WHERE IT ATTACHES TO FRAME AT STA 794. REPAIRED PER DC9 SRM 53-02, FIG 18 SHEET 1. CHECK-C 8-12-98 STL. - [SDR TWAA9903407](https://openairdocs.org/sdr/TWAA9903407), Feb 28, 1999: LONGERON. CRACKED. FOUND THE OTBD FLANGE OF LONGERON 4L CRACKED .25 INCH WHERE IT ATTACHES TO FRAME AT STA 794. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON PER SRM 53-02, FIG - [SDR TWAA9813404](https://openairdocs.org/sdr/TWAA9813404), Aug 12, 1998: FITTING. CORRODED. DURING CHECK-C MAINT, FOUND LONGERON 20R, LONGERON 21R, LONGERON 22R, HAD END FITTINGS CORRODED AT STA 1167 BULKHEAD. REPLACED END FITTINGS AT STA 1167 AND LONG - [SDR TWAA9813403](https://openairdocs.org/sdr/TWAA9813403), Aug 8, 1998: LONGERON. CRACKED. DURING CHECK-C MAINT, FOUND .25 INCH CRACK IN FLANGE OF LONGERON 23L AT STA 287. CUT OUT DAMAGED SECTION OF LONGERON, AND INSTALLED NEW SECTION AND SPLICE PER S - [SDR TWAA9813402](https://openairdocs.org/sdr/TWAA9813402), Aug 8, 1998: LONGERON. CRACKED. DURING CHECK-C MAINT, FOUND .25 INCH CRACK IN FLANGE OF LONGERON 24L AT STA 294. CUT OUT DAMAGED SECTION OF LONGERON AND INSTALLED NEW SECTION AND SPLICE PER SR - [SDR TWAA9813401](https://openairdocs.org/sdr/TWAA9813401), Aug 6, 1998: BEAM. CRACKED. DURING CHECK-C MAINT, THE FWD RT SERVICE DOOR BEAM HAD A 2 IN CRACK AT FWD END. REPLACED BEAM IN SHOP ON TICKET 836667 PER SRM 52-05, FIG 25 AND 51-10. - [SDR TWAA9719004](https://openairdocs.org/sdr/TWAA9719004), Feb 8, 1997: CSD. FAILED. CMH - DURING TAKEOFF NR 2 ENGINE, S/N 1718, FIREWARNING LIGHT ILLUMINATED DUE TO A FAILED CSD. REMOVED AND REPLACED CONSTANT SPEED DRIVE, MFG P/N 696233B. OPERA - [SDR TWAA9613305](https://openairdocs.org/sdr/TWAA9613305), Oct 30, 1996: FITTING. CRACKED. STL - DURING SPECIAL CHECK, FOND A TWO INCH CRACK IN LONGERON 29R FITTING, STATION 732.5 FORWARD SIDE. REMOVED AND REPLACED FITTING PER SRM 51-30-5 AND TWA STAN - [SDR 96ZZZX3855](https://openairdocs.org/sdr/96ZZZX3855), May 28, 1996: ENGINE. FAILED. STL - FLT 564 - DURING APPROACH, SHUT DOWN NR 2 ENGINE, S/N 1722, DUE TO INCREASING EGT. ACCOMPLISHED NORMAL LANDING. FOUND TURBINE DAMAGE AND METAL PARTICLES I - [SDR 96ZZZM1042](https://openairdocs.org/sdr/96ZZZM1042), May 28, 1996: TURBINE. DAMAGED. STL - DURING APPROACH SHUT DOWN NR 2 ENGINE, S/N 1722, DUE TO INCREASING EGT. ACCOMPLISHED NORMAL LANDING. FOUND TURBINE DAMAGE AND METAL PARTICLES IN TAILPIPE. - [SDR 96ZZZX1240](https://openairdocs.org/sdr/96ZZZX1240), Jan 26, 1996: ACTUATOR. FAILED. STL - FLT 503 - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED. REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNAL FAILURE, MFG PN 2589445-933. OP - [SDR 96ZZZM208](https://openairdocs.org/sdr/96ZZZM208), Jan 26, 1996: ACTUATOR. FAILED. STL - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED. REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNAL FAILURE, MFG P/N 2589445-933. OPERATIONAL - [SDR 96ZZZX231](https://openairdocs.org/sdr/96ZZZX231), Dec 15, 1995: CSD. FAILED. STL - FLT 126 - AFTER TAKEOFF, NR 2 CSD LOW PRESSURE LIGHT CAME ON. NR 2 CSD DISCONNECTED. REMOVED AND REPLACED CSD, MFG PN 696233B, OPERATIONAL AND LEAK CHECK - [SDR 96ZZZM54](https://openairdocs.org/sdr/96ZZZM54), Dec 2, 1995: BULB. FAILED. STL - FLT 124 - DURING LAYOVER, MAINTENANCE FOUND RIGHT AFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB. OPERATIONAL CHECK NORMAL. - [SDR 95ZZZZ251](https://openairdocs.org/sdr/95ZZZZ251), May 23, 1995: COALESCER. DIRTY. STL - FLT 518 - DURING CLIMB A SMOKE ODOR APPEARED IN CABIN. TURNED RIGHT AIR CONDITIONING PACK TO FULL COLD, ODOR AND HAZE DISSIPATED, RETURNED TEMPERATURE CON - [SDR 95ZZZZ250](https://openairdocs.org/sdr/95ZZZZ250), May 23, 1995: AMPLIFIER. MALFUNCTIONED. STL - FLT 518 - DURING CLIMB A SMOKE ODOR APPEARED IN CABIN. TURNED RIGHT AIR CONDITIONING PACK TO FULL COLD, ODOR AND HAZE DISSIPATED, RETURNED TEMPERATURE CON - [SDR 95ZZZX1231](https://openairdocs.org/sdr/95ZZZX1231), Jan 4, 1995: BELT RING. CRACKED. STL - DURING CHECK-C, FOUND .25 INCH CRACK IN BELT RING, IN TAIL COMPARTMENT, STA 1212.809, LONGERON 6L, 6R, 5R, 5L, 4R, AND 4L. REPLACED BELT RING PER SRM 51-1 ## 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 19891008054069I](https://openairdocs.org/incident/19891008054069I), Oct 8, 1989: Doug DC951 (N410EA), Atlanta, GA, Minor damage. Aircraft lost NR4 main wheel assembly during landing. Cause of failure not stated. ## Other aircraft with N410EA - [Registered now](https://openairdocs.org/aircraft/N410EA): Pipistrel D O O ALPHA TRAINER, S/N AT162A0016, built 2025 --- 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.