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ROBIN AIGLON II
SEATING
Front: 2 Rear: 2
DIMENSIONS
Length: 7.26 m
Height 2.38 m
Wingspan 9.08 m
Wing area 15.10 m2
Cabin width, at elbow level 1.13m (44.5 in)
POWERPLANT
Manufacturer: Lycoming
Type O-360-A3A
4 cylinders
Power rating 180 BHP
Recommended TBO 2,000 hours
Propeller 2 blades, fixed pitch
FUEL
Usable fuel 50 Imp Gal (228 L)
LOADING
Empty weight 650 kg
Gross weight (take-off) 1,150 kg
Useful load 500 kg
Baggage load 60 kg
PERFORMANCE
Max Authorized Speed (Vne) 170 kts
Max level speed (at S/L) 144 kts
Max cruising (75% power, at optimum height) 134 kts
Econ. cruising speed (65% power) 128 kts
Max rate of climb (at S/L) 1100 kg 943 ft/mn
          1000 kg
1,100 ft/mn
Demonstrated crosswind component 22 kts
Service ceiling, 1000 kg 16,400 ft
Stalling speed (flaps down) 52 kts
Takeoff distance [ISA - 1,000 kg] 285 m (934 ft)
Clear 50' obstacle [ISA - 1,000 kg] 420 m (1,380 ft)
Landing distance [ISA - 1,000 kg] 305 m (1,000 ft)
Fuel consumption 75% power 8.4 gph
Fuel consumption 65% power 7.9 gph
Range (no reserve)  
    - @ 75% power
720 nm
    - @ 65% power
785 nm
Reference: Aiglon II Brochure, Avions Robin, France, ....
Given data is only for information. Please refer to the manufacturer for current data.

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