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ROBIN 2160
CONFIGURATION
FAA certified aircraft
FAR 23, Acrobatic category (+6G/-3G)
SEATING 2 Seats
DIMENSIONS
Length: 7.10 m (23 ft 3 in)
Height 2.13 m (7 ft)
Wingspan 8.33 m (27 ft 4 in)
Wing area 13 m2 (140 sq ft)
POWERPLANT
Manufacturer: Textron-Lycoming
Type O-320-D2A
4 cylinders
Power rating 160 hp @ 2700 rpm
PROPELLER
Manufacturer Sensenich
Blades 2
Type fixed-pitch
FUEL CAPACITY
Standard 120 L
Optional 160 L
LOADING
Empty weight 550 kg (1,235 lb)
Maximum weight  
    - When operated in "A" category
800 kg (1,764 lb)
    - When operated in "U" category
900 kg (1,984 lb)
PERFORMANCE ("A" cat., at 800 kg max. weight)
Max. cruising speed, @ 75% power, 8500 ft 242 km/h (131 kt)
Max. range (std tank, no reserve)  
    - at 65% power / 127 kt / 11000 ft
952 km (514 nm)
    - at 75% power / 131 kt / 8500 ft
850 km (459 nm)
Max. rate of climb 5.2 m/s (1,023 ft/min)
Service ceiling 15,000 ft
Stalling speed (flaps down) 85 km/h (46 kt)
Take-off roll 230 m (754 ft)
Take-off run to 50 ft 410 m (1,345 ft)
Reference: Robin 2160 Brochure, Avions Robin, France, 1994
Given data is only for information. Please refer to the manufacturer for current data.

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