IABSA Premier 64-01
Indústria Aeronáutica Brasileira · Brazil · first flew 1964 · light aircraft
The IABSA Premier 64-01 was a Brazilian two-seat training and touring braced high-wing monoplane.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 6.7 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Braced high-wing monoplane
- Two seats
- Single Continental A75 flat-four engine driving a two-bladed propeller
Look for a small Brazilian two-seat braced high-wing monoplane with a McCauley two-bladed metal propeller.
Specifications
- The IABSA Premier 64-01 has a length of 6.7 m (22 ft).
- It has a wingspan of 10.7 m (35 ft).
- Its maximum speed is 160 km/h (99 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
Designed by Vicente Martin Llopis and built by Industria Aeronáutica Brasileira (IABSA), it first flew in 1964. It was powered by a 75 hp Continental A75 air-cooled four-cylinder engine.
Variants
The Premier 64-01 was designed and built in small numbers, powered by a 75 hp piston engine.
Where you'll see it
It was designed for training and touring use, with a normal cruise of 130 km/h and a range of 600 km.
Related aircraft
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