| Premier 65-02 | |
|---|---|
| Role | Utility aircraft |
| National origin | Brazil |
| Manufacturer | Indústria Aeronáutica Brasileira |
| Designer | Vicente Martin Llopis |
| First flight | 1965 |
| Number built | 1 |
The IABSA Aerobatic 65-02 was a Brazilian single-engine, multirole aircraft and touring braced high-wing designed and built by Indústria Aeronáutica Brasileira (IABSA), [1] powered by a 75 hp (56 kW) piston engine. Although well rated, it never went into production. [1]
Specifications
Data from Taylor 1965, p. 12
General characteristics
- Crew: 2
- Length: 4.67 m (15 ft 4 in)
- Wingspan: 5.30 m (17 ft 5 in)
- Powerplant: 1 × Continental A65 air-cooled four-cylinder horizontally-opposed, 56 kW (75 hp)
- Propellers: 2 fixed-pitch metal propeller-bladed
Performance
- Range: 600 km (370 mi, 320 nmi)
- Service ceiling: 4,000 m (13,000 ft)
References
Notes
Bibliography
- Taylor, John W. R. (1965). Jane's All The World's Aircraft 1965–66. London: Sampson Low, Marston & Company, Ltd.
- The Complete Illustrated Encyclopedia of the World's Aircraft. Secaucus, New Jersey: Chartwell Books. 1978. p. 196.
 | This article on an aircraft of the 1960s is a stub. You can help Wikipedia by expanding it. |
| Premier 65-02 | |
|---|---|
| Role | Utility aircraft |
| National origin | Brazil |
| Manufacturer | Indústria Aeronáutica Brasileira |
| Designer | Vicente Martin Llopis |
| First flight | 1965 |
| Number built | 1 |
The IABSA Aerobatic 65-02 was a Brazilian single-engine, multirole aircraft and touring braced high-wing designed and built by Indústria Aeronáutica Brasileira (IABSA), [1] powered by a 75 hp (56 kW) piston engine. Although well rated, it never went into production. [1]
Specifications
Data from Taylor 1965, p. 12
General characteristics
- Crew: 2
- Length: 4.67 m (15 ft 4 in)
- Wingspan: 5.30 m (17 ft 5 in)
- Powerplant: 1 × Continental A65 air-cooled four-cylinder horizontally-opposed, 56 kW (75 hp)
- Propellers: 2 fixed-pitch metal propeller-bladed
Performance
- Range: 600 km (370 mi, 320 nmi)
- Service ceiling: 4,000 m (13,000 ft)
References
Notes
Bibliography
- Taylor, John W. R. (1965). Jane's All The World's Aircraft 1965–66. London: Sampson Low, Marston & Company, Ltd.
- The Complete Illustrated Encyclopedia of the World's Aircraft. Secaucus, New Jersey: Chartwell Books. 1978. p. 196.
|
| This article on an aircraft of the 1960s is a stub. You can help Wikipedia by expanding it. |