| Specifications |
|
|
Versions available: B or C model (C model has wider, longer fuselage). Empty Weight: 580 pounds - 650 pounds (dependent upon engine installation). Max Take Off Weight: 1200 pounds (545 kgs). Wing Span: 32.5 feet. Chord: 54 inch. Wing Area: 146 sq. feet. Length: 20 feet (including propeller and spinner). Height (flt attitude): 6ft 10in. Fuel Capacity: 12 imp. gallons (2 x wing tanks). Seating Capacity: 2 (side x side). Engine: Rotax 912 / Jabiru / Continental HP range: 65 -100 HP. VNE: 120 knots. Cruise: 70 - 85 knots. Stall: 26 - 30 knots. Take off roll (ground roll): 200 metres. Flaps: optional. Baggage: 20 kgs. Undercarraige: tailwheel (trigear optional). Brakes: Dual centre lever (optional heel brakes). Suspension: rebound spring. Construction: Fuselage - welded 4130 steel tube frame fabric covered. Wing - wood spar / marine ply ribs. fabric covered. Tail plane - welded 4130 steel tube frame fabric covered. FLIGHT CHARACTERISTICS. The following report is given by the builder of the blue J6-B Australian Karatoo that features on our photo page: "very mild stall - no wing drop - 3 points landings easier than wheelers - leisurely roll rate but can be whipped around with the addition of rudder, i.e., stall turn or agressive wing over". A J6-A Karatoo built in South Africa; "good glide ratio - smooth handling with perfect reaction - more rudder useage than ailerons - a real dream come true". Engine - 90 hp Continental with a 2 blade wooden prop. Take off roll - 500 metres, landing roll - 300 metres (airfield elevation 5,600 feet). Gross weight - 1120 pounds, empty weight 580 pounds. Top speed - 110 kts, Cruise - 80 kts, Stall - 40 kts. Rate of climb - 500 feet / minute. Fuel capacity - 52 ltres.
|
| < Prev | Next > |
|---|

