Civil Aviation Department Revathi
Civil Aviation Department · India · first flew 1967 · light aircraft
The Civil Aviation Department Revathi was a light utility aircraft designed in India principally for use by that country's flying clubs.
Recognition (WEFT)
| W — Wings | Low-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 7.58 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Conventional low-wing monoplane
- Fixed tailwheel undercarriage
- Two seats side by side with an optional third behind
A conventional low-wing monoplane with a welded steel-tube fuselage, an all-metal wing and a fixed tailwheel undercarriage.
Specifications
- The Civil Aviation Department Revathi has a length of 7.58 m (25 ft).
- It has a wingspan of 9.4 m (31 ft).
- Its maximum speed is 193 km/h (120 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
The Revathi first flew on 13 January 1967 and received Indian type certification in January 1969. It was powered by a 145 hp Rolls-Royce/Continental O-300C.
Variants
The prototype's wings and fuel system were later revised, and the resulting configuration was designated the Revathi Mk.II. It first flew on 20 May 1970 and received its type certificate on 31 October 1972.
Where you'll see it
It was intended principally for flying clubs.
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