Microjet 200
Microjet SA · France · first flew 1980 · light aircraft
The Microjet 200 was a French jet trainer designed and built by Microjet SA.
Recognition (WEFT)
| W — Wings | Low-mounted, straight |
|---|---|
| E — Engines | 2 × turbojet, fuselage-mounted |
| F — Fuselage | 6.67 m fuselage |
| T — Tail | V-tail |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Lightweight two-seat jet trainer
- Twin Microturbo TRS 18-1 turbojets
- Low-wing layout with a V-tail
Look for a small low-wing twin-jet trainer with a V-tail.
Specifications
- The Microjet 200 has a length of 6.67 m (22 ft).
- It has a wingspan of 7.56 m (25 ft).
- Its maximum speed is 463 km/h (288 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
The all-wood prototype first flew on 24 June 1980, and the first of three mixed-construction pre-production 200Bs flew on 19 May 1983.
Variants
Four Microjet 200 aircraft were built.
Where you'll see it
It was a lightweight jet trainer powered by two Microturbo TRS 18-1 turbojets.
Related aircraft
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