Aura Aero Integral R
| Integral R | |
|---|---|
 | |
| General information | |
| Type | Two-seat aerobatic training monoplane |
| National origin | France |
| Manufacturer | AURA AERO |
| History | |
| First flight | June 2020 |
The AURO AERO Integral R is a French two-seat aerobatic low-wing training monoplane first flown in June 2020.[1][2] The aircraft is the first of a family of Integral aircraft to fly and achieved EASA Certification in the CS-23 Normal Aircraft category in December 2024.[3][1]
Design
[edit]The Integral R is a two-seat side by side cantilever low-wing monoplane with a fixed conventional landing gear with a tail-wheel. It has a wood structure reinforced with carbon and powered by a Lycoming AEIO-390-A3B6 piston aero-engine certified for aerobatic use with a tractor two-bladed propeller.[3]
Aircraft Specification
[edit]Data from [3]
General characteristics
- Crew: 2
- Length: 7.26 m (23 ft 10 in)
- Wingspan: 8.78 m (28 ft 10 in)
- Height: 2.48 m (8 ft 2 in)
- Wing area: 9.97 m2 (107.3 sq ft)
- Fuel capacity: 169 us gallons
- Powerplant: 1 × Lycoming AEIO-390-A3B6
- Propellers: 2-bladed MT-Propeller MTV-15-B-C / C-193-25, 1.93 m (6 ft 4 in) diameter
Performance
- Stall speed: 114 km/h (71 mph, 62 kn)
- Never exceed speed: 330 km/h (210 mph, 180 kn)
- Service ceiling: 3,810 m (12,500 ft)
- g limits: +6g/-4g
References
[edit]- ^ a b Ben Sampson (2024-12-20). "Auro-Aero Achieves Certification of Integral R aircraft". Retrieved 2024-12-28.
- ^ "AURA AERO Integral". Aura Aero SAS. Retrieved 2024-12-28.
- ^ a b c "Type Certificate Data Sheet EASA A.661" (PDF). EASA. 2024-12-18.