L-39V

 

On request of the Czechoslovak Airforce, a single seat L-39V target towing modification was developed. The rear unpressurized cockpit of the eighth prototype, tested since 1972, was equipped with a winch device driven by a ram-air turbine, located in a pod under the fuselage. The KT-04 target was developed by Letov; and procedures for take off and target retrieval were also developed and tested
GDR