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Ken Brock Manufacturing Avion

 

brockavion


Offered as a completely finished, unassembled kit. A high-wing monoplane with conventional tail group and three-axis stick-and-rudder controls. Steerable nosewheel. Strut-braced, built-up rigid wings, Dacron cover-ing. Fuel tank built into pilot seat. POWERPLANT: Yamaha 15 hp, 2:1 reduction drive, 48-inch prop. LANDING GEAR: Spring tube.

Prototype
Wingspan 28’6”.
Wing area 114 sq ft.
Length 14’.
Height 78”
Empty weight 190 lbs.
Empty wt: 240 lbs.
Wing span: 29’.
Wing area: 145 sq.ft.
Height: 6’10”.
Length: 15’6”.
Fuel cap; 5 USG.
Construction: Aluminium, Dacron.
Engine: Rotax 277 (268 cc) 28 hp.
Max wt: 455 lbs.
Stall: 25 mph.
Max speed: 60 mph.
Vne: 80 mph.
Climb rate: 700 fpm @ 45 mph.
Design limit: +6, -4g.
Glide ratio: 7-1.
Wing loading: 3.14 lbs/sq.ft.
Power loading: 16.25 lbs/hp.

Production
Engine: Rotax 277.
Prop: 48 in.
Wingspan: 28 ft 6 in.
Wing area: 145 sq.ft.
Empty wt: 240 lbs.
Max wt: 500 lbs.
Cruise: 45-50 mph.
Stall: 24 mph.
Vmax: 63 mph.
T/O run: 100 ft.
Ldg roll: 20-50 ft.

 

 

 


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