N121CC - 1998 Cartercopters LLC Cartercopter Aircraft Registration
FEST1998 CARTERCOPTERS LLC CARTERCOPTER
Aircraft Description
N121CC is a 1998 Cartercopters LLC CARTERCOPTER, a single-engine reciprocating (piston) aircraft registered to Carter Aviation Technologies LLC in Wichita Falls, TX. This aircraft holds a experimental airworthiness certificate issued by the Federal Aviation Administration on January 18, 2005. The registration certificate was issued on June 8, 1998. The registration is set to expire on September 30, 2027. Powered by a Ama/expr UNKNOWN ENG engine, N121CC is. The aircraft's Mode S transponder code is A0579E (hex), used for ADS-B identification and flight tracking. The FAA registry record for N121CC was last updated on March 17, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Cartercopters LLC is an aircraft manufacturer with aircraft registered in the FAA database tracked by AviatorDB. AviatorDB tracks 1 Cartercopters LLC aircraft currently registered in the FAA database, including the CARTERCOPTER model.
AviatorDB has found no NTSB accident or incident reports involving N121CC. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (5)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Apr 8, 2003 | FTW03LA125 | Substantial | None | The pilot's failure to extend the landing gear. A factor was his diverted attention. |
| Apr 29, 2001 | FTW01LA108 | Substantial | None | the pilot's failure to maintain directional control during the takeoff initial climb. Contributory factors were the pilot's lack of experience with the aircraft and the soft terrain. |
| Mar 25, 2001 | FTW01LA086 | Substantial | None | the pilot's failure to maintain rotor rpm, which resuted in the main rotor contacting the tail during landing. |
| Dec 13, 2000 | FTW01LA040 | Substantial | None | The pilot's delay in lowering the collective during a run-on landing, which resulted in a runway overrun. A factor was the muddy terrain. |
| Dec 16, 1999 | FTW00LA045 | Substantial | None | The pilot's failure to maintain rotor rpm during takeoff, which resulted in a hard landing following the aborted takeoff. |
The pilot's failure to extend the landing gear. A factor was his diverted attention.
the pilot's failure to maintain directional control during the takeoff initial climb. Contributory factors were the pilot's lack of experience with the aircraft and the soft terrain.
the pilot's failure to maintain rotor rpm, which resuted in the main rotor contacting the tail during landing.
The pilot's delay in lowering the collective during a run-on landing, which resulted in a runway overrun. A factor was the muddy terrain.
The pilot's failure to maintain rotor rpm during takeoff, which resulted in a hard landing following the aborted takeoff.
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC