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||Four-seat touring and training monoplane
The Robin R.1180 Aiglon ia a French four-seat touring and training monoplane designed and built by Avions Robin.
The Aiglon is an all-metal low-wing monoplane with a fixed tricycle landing gear and powered by a nose-mounted 180hp (134kW) Lycoming O-360-A3AD engine. It was based on the early HR100 but had a lighter airframe and new fin and rudder. The prototype first flew on 25 March 1977 and the production version with detail improvements was certified on 19 September 1978.
- R.1180 Aiglon
- Prototype, one built
- R.1180T Aiglon
- Production variant with longer cabin side windows, 30 built.
- R.1180TD Aiglon II
- A R.1180T with a new instrument panel, improved cabin furnishing and an external baggage locker, 36 built.
- Crew: 1
- Capacity: 3
- Length: 7.26 m (23 ft 9¾ in)
- Wingspan: 9.08 m (29 ft 9½ in)
- Height: 2.38 m (7 ft 9¾ in)
- Wing area: 15.10 m² (162.54 ft²)
- Empty weight: 650 kg (1433 lb)
- Gross weight: 1150 kg (2535 lb)
- Powerplant: 1 × Lycoming O-360-A3AD flat-four piston engine, 134 kW (180 hp)
- Maximum speed: 151 km/h (156 mph)
- Range: 1625 km (1009 miles)
- Service ceiling: 5030 m (16,505 ft)
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Published - July 2009
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