Indraéro Aéro 101
| Aéro 101 | |
|---|---|
|
|
| Type: | Sport plane |
| Design country: | |
| Manufacturer: | |
| First flight: |
May 1, 1950 (Aéro 110 prototype) |
| Number of pieces: |
13 |
The Aéro 101 was a double-decker training aircraft with double controls made by the French manufacturer Indraéro and made its first flight in 1953.
history
The aircraft had been built for the national Service de l'Aviation Légère et Sportive (SALS), which had the contract to equip aero clubs with aircraft and instructors. The aircraft had a boxer engine type Minié 4 DC-32 with 75 hp . The aircraft with a top speed of 170 km / h was developed by Chapeau & Blanchet .
The aircraft was a further development of the Aéro 110 prototype, which first flew on May 1, 1950. This predecessor had a 45 HP radial engine Salmson 9ADB and only a spur instead of a rear wheel and no wheel brakes. In addition, the rear fuselage of the 110 was a fabric-covered tubular steel construction, while the 101 was made of wood. The wings of the biplane both had the same wingspan and the wingspan remained the same for both types.
Technical specifications
| Parameter | Type 101 | Type 110 |
|---|---|---|
| crew | 2 | |
| length | 5.58 m | |
| span | 7.59 m | |
| Empty mass | 270 kg | |
| Max. Takeoff mass | 453 kg | |
| drive | a Minié 4 DC-32, 75 PS (55 kW) | a Salmson 9ADB, 45 PS (33 kW) |
| Top speed | 173 km / h | 130 km / h |
| Cruising speed | 150 km / h | 114 km / h |
| Starting rate of climb | 192 m / min | |
Web links
Individual evidence
- ^ William Green and Gerald Pollinger: The Aircraft of the World; MacDonald & Co (Publishers) Ltd. London 1955