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 AURA 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

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

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

1. Ben Sampson (2024-12-20). "Auro-Aero Achieves Certification of Integral R aircraft" . Retrieved 2024-12-28.
2. "AURA AERO Integral". Aura Aero SAS. Retrieved 2024-12-28.
3. "Type Certificate Data Sheet EASA A.661" (PDF). EASA. 2024-12-18.