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CAB Supercab
Light Utility · Early Jet (1946–1969)
The CAB GY-30 Supercab was a two-seat light aircraft built in France in 1954, as a further development of the CAB Minicab. The design was performed by Yves Gardan, a onetime employee of French aeronautical company SIPA. Changes incorporated in the Supercab included a more powerful engine, greater wingspan, manually retractable undercarriage, and slotted flaps that replaced the split flaps of the Minicab.
Specifications
- Category
- Fixed Wing
- Sub-Category
- Light Utility
- Domain
- Civil
- Era
- Early Jet (1946–1969)
- Engine
- 1× air-cooled four-cylinder horizontally opposed piston engine
- Thrust / Power
- 90 hp
- Length (ft)
- 18
- Wingspan (ft)
- 27
- Empty Weight (lb)
- 882
- MTOW (lb)
- 1351
- Service Ceiling (ft)
- 16404
- Max Speed (mph)
- 171