Developed in 1947. For directional control, the cabin could be manually displaced to change the center of gravity [Ref 316].
Design authority: Seibel Helicopter Company
Primary manufacturer: Seibel Helicopter Company
Parent type: No type defined
Aircraft status: No longer flying
VTOL type: Helicopter
Lift devices: 1 Single main rotor
Dedicated control device: 1 Tail rotor
Crew required: 1 in Single seater arrangement
Landing gear: Wheels (non-retractable)