OGAR

Type designation	SZD-45A SZD-45-2 "Ogar F"
Competition class	Two Seater
Number built	65
Crew	2
Length	7.95 m
Height	1.51 m
Wingspan	17.6 m
Wing area	19,10 m²
Aspect ratio	16.2
Empty mass	ca. 470 kg
Maximum mass	700 kg
Wing loading	ca. 36,6 kg/m²
Maximum speed	225 km/h
Speed in rough air	165 km/h (89 kts)
Stall speed	78 km/h 42 KTS)
Minimum sink rate	ca. 1.10 m/s with 85 km/h
Engine	Limbach SL-1700EC
Power	68 HP

PZL-Bielsko Ogar SZD-45A motor glider, built in 1976

The SZD-45 Ogar is a T-tailed cantilever high wing monoplane of wooden, aluminium and fibreglass construction designed in Poland. The prototype of this self-launching motorglider SP-0001 first flew on the 29th May 1973. soaring capability and staggered side-by-side two-place seating. There were 64 examples constructed excluding the prototype with 41 of these being exported.

It has a Hoffmann twin-bladed pusher propeller. The landing gear is semi-retractable. The U.S. import is powered with the dual ignition, turbocharged, Revmaster engine. The "Ogar" is certified for simple aerobatics

Ogar

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