| RA-3 | |
|---|---|
![]()  | |
| Role | Aerobatic trainer | 
| National origin | United States | 
| Manufacturer | Rud Aero | 
| Introduction | 2013 | 
The Rud Aero RA-3 is an American composite aerobatic training aircraft, produced by Rud Aero.[1]
Design and development
The RA-3 is a single engine two-seat, side-by-side configuration, low wing, tricycle gear composite construction aircraft. The aircraft is built using carbon fiber construction throughout. The aircraft has a cambered training wing that can be exchanged for a constant chord symmetrical wing for advanced aerobatic training. The aircraft is designed to operate as an FAR Part 21.24 aircraft, with future modifications to meet American LSA standards.[2]
Variants
- RA-3
 - Base model
 - RA-3L
 - LSA variant
 
Specifications (RA-3)
Data from EAA, Manufacturer
General characteristics
- Crew: 1
 - Capacity: 1
 - Length: 22 ft (6.7 m)
 - Wingspan: 24 ft (7.3 m)
 - Empty weight: 1,100 lb (499 kg)
 - Gross weight: 1,800 lb (816 kg)
 - Fuel capacity: 44 U.S. gallons (170 L; 37 imp gal)
 - Powerplant: 1 × Lycoming IO-360 Horizontally opposed piston aircraft engine, 180 hp (130 kW)
 - Propellers: 3-bladed MT Propeller constant speed propeller
 
Performance
- Maximum speed: 130 kn (150 mph, 240 km/h)
 - Cruise speed: 117 kn (135 mph, 217 km/h)
 - Stall speed: 43 kn (50 mph, 80 km/h)
 - g limits: +-8g
 - Rate of climb: 1,961 ft/min (9.96 m/s)
 
Avionics
- Dynon Skyview
 
References
Wikimedia Commons has media related to Rud Aero RA-3.
- ↑ "RUD RA-3". Archived from the original on 25 August 2013. Retrieved 23 August 2013.
 - ↑ "Rud Aero Debuted Aerobatic trainer". Archived from the original on 1 February 2014. Retrieved 23 August 2013.
 
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