The INTEGRAL R is a state-of-the-art, two-seat aerobatic training aircraft - unique design features make it unique in its class.
Ideal for basic training, UPRT or advanced aerobatics, the INTEGRAL R is the best choice in terms of performance and versatility. Thanks to its innovative design and state-of-the-art features, the aircraft offers excellent piloting performance.
Uncompromising maintenance and service requirements combined with a rugged and robust design make the INTEGRAL R a highly competitive design for both civilian and military pilot training.
Aura Integral R

maximum range: 980 km
cruising speed: max. 294 km/h
maximum flight ceiling: 3 810 m
payload: 260 kg
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Integral R
Versatile and efficient

Integral R
The INTEGRAL R is a classic training aircraft, but made with state-of-the-art technology. The lightweight and durable structure is the result of the use of wood and carbon fiber composite, combined for high rigidity with low empty weight.
The propulsion system allows you to use the full capabilities of the airframe - designed for aerobatics, the Lycoming AEIO-390 engine guarantees the reliability and low maintenance known from classic Lycoming engines, adding upgrades in the form of an electronic ignition system and fuel injection.
It is still a classic aerobatic aircraft with high performance - 210 horsepower provides excess power and the tailwheel landing gear system and flapless wing guarantee high aerodynamic efficiency, even in +7.5 / -7.5 G-load figures.

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MADE FOR ACROBATICS
The IINTEGRAL R is a new-generation aircraft, created from the ground up with a single purpose - to provide an effective platform for VFR, UPRT and higher aerobatic training at 21st century training centers. Low weight, modern use of materials and high structural strength provide unparalleled piloting performance in its class.
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NEW DIMENSION OF TRAINING
The layout of the cabin, in which the pilot and student sit side by side, provides excellent conditions for training and control of piloting technique. Aerodynamic parameters of the design ensure safe and predictable behavior of the aircraft not only in figures of higher aerobatics but also in standard phases of any flight.
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SAFETY FIRST
It is an aircraft designed with the slogan "Safety First" and meets the highest safety standards. The INTEGRAL R is equipped with a full-size rescue parachute, deflagration-protected fuel tanks and a digital flight performance analysis system, making it a leader in its class.
Expert section
Details
Dimensions
- Length: 7.26 m (23.82 ft)
- wingspan: 8.78 m (28.80 ft)
- Height: 2.48 m (8.13 ft)
Weights
- maximum takeoff weight: 2,216 lb (1,005 kg)
- payload: 573 lb (260 kg)
- empty aircraft weight (standard equipment): 1413 lb (641 kg)
- fuel volume and weight: 159 l (42 gal US)
Performance
- maximum cruising speed: 159 kts (294 km/h)
- maximum range: 530 nm (980 km)
- maximum flight ceiling: 12,500 ft (3,810 m)
- run-up (MTOW, sea level, standard atmosphere): 360 ft (110 m)
- 15m obstacle start: 1640 ft (500 m)
- run: 661 ft (200 m)
- landing from an obstacle 15 m: 1640 ft (500 m)
- fuel consumption: 42 l/h (3.8 gal/h)
- cabin type: unpressurized
Drive unit
- Engine: Lycoming AEIO-390/A3B6
- engine power: 210 hp
- propeller: MT Propeller MTV-15-B-C/C193-25
- number of blades: 2
- propeller diameter: 1.93 m (76 in)
- fuel: AVGAS
Avionics
- avionics type: Garmin G3X
- autopilot: none
- spare instruments: classic
Operating parameters
- type of operation: VFR-Day
- crew: 1
- number of passenger seats: 1
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The Integral R represents the latest generation of training aircraft tailored to train aerial aerobatics in a 'side by side' cabin layout.