PUMA advanced ultralight specifications, PUMA basic ultralight aircraft information, PUMA light sport aircraft specs and information.

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PUMA ultralight/lightsport aircraft performance and  specifications.

The following are the specifications and performance specs on the PUMA two place ultralight, advanced ultralight, experimental light sport aircraft when equipped with a  Rotax 80 HP engine.
PUMA Aircraft - Performance / Specifications with 80 HP Rotax aircraft engine.
Useful Load 496 lbs (225kg)
Empty Weight 662 lbs (300 kg)
Gross Weight 1158 lbs (525 kg)
Engine Rotax 912UL
Cruise Speed 75% (80 HP) 95 mph (160 km/h)
Stall Speed 40 mph (64 km/h)
Rate of Climb 1000 feet/min (5m/sec)
Glide Ratio 11:1
Wing Span 28 feet (8.5 m)
Length 20.8 feet (6.33 m)
Fuel Capacity 13.2 gallons (50L)
Cabin Width 44 inches (1118 mm)
For More information contact:
Otreb Technologies Inc.

2561 rue De la Symphonie
ST-Lazare J7T-3L1 QC
CANADA
514 581-5577
450 510-1700
www.puma-aircraft.com


PUMA ultralight, advanced ultralight, Lightsport Aircraft.

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