Godbille JG.1B
| Godbille JG.1B | |
|---|---|
| Role | Two seat sport homebuilt aircraft |
| National origin | France |
| Designer | Jean Godbille |
| First flight | 1989 |
| Number built | 1 |
|
| |
The Godbille JG.1B is a French light, two seat amateur built aircraft, dating from 1989. Only one was constructed.
Design and development
The JG.1B is a small sports aircraft with two seats placed side-by side. It has a polyester fabric covered steel tube structure and is a cantilever, low wing monoplane. Its straight edged wings carry inboard flaps.[1]
Conventionally laid out, the JG.1B is powered by a 78 kW (105 hp) Potez 4E-20B1 air-cooled flat four engine which drives a two blade propeller. The two occupants sit over the wing leading edge under a PET canopy, which blends at the rear into a raised, rounded fuselage decking. As the decking drops away rearwards, a long dorsal fillet leads to a swept, straight edged fin with a narrow triangular rudder. The tailplane is wire braced to the fin. The JG.1B's tail wheel undercarriage is fixed.[1]
The JG.1B gained its Certificate of Airworthiness on 15 November 1989.[2] It remains on the French Civil Aircraft register in 2014.[3]
Specifications
Data from Gaillard (1991), p.246[1]
General characteristics
- Capacity: Two
- Length: 6.10 m (20 ft 0 in)
- Wingspan: 6.20 m (20 ft 4 in)
- Wing area: 9.4 m2 (101 sq ft)
- Empty weight: 418 kg (922 lb)
- Gross weight: 662 kg (1,459 lb)
- Powerplant: 1 × Potez 4E-20B1 air-cooled flat four, 78 kW (105 hp)
- Propellers: 2-bladed
Performance
- Cruising speed: 185 km/h (115 mph; 100 kn)
- Endurance: 4 hr
References
- 1 2 3 Gaillard, Pierre (1991). Les Avions Francais de 1965 à 1990. Paris: Éditions EPA. p. 246. ISBN 2 85120 392 4.
- ↑ Chillon, Jacques. Fox Papa - Registre des avions Français amateur (2009 ed.). Brive: Ver Luisant. p. 102. ISBN 978-2-3555-1-066-3.
- ↑ Partington, Dave. European registers handbook 2014. Air Britain (Historians) Ltd. ISBN 978-0-85130-465-6.