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Avro 626 Prefect


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avro626prefect-2


1930

Moravko-Slezka Vazovka Tatra (Ringhoffer-Tatra) obtained licenses to build the Avro 626 as T.126, and the Bucker Bu 131 Jungmann as the T.131.

Avro 626 Prefect
Engine: Armstrong Siddeley Lynx IV C, 237 hp
Length: 26.509 ft / 8.08 m
Height: 9.58 ft / 2.92 m
Wingspan: 33.99 ft / 10.36 m
Wing area: 299.993 sq.ft. / 27.87 sq.m
Max take off weight: 2749.6 lb / 1247.0 kg
Weight empty: 1766.2 lb / 801.0 kg
Max. speed: 97 kt / 180 km/h
Cruising speed: 83 kt / 153 km/h
Service ceiling: 14797 ft / 4510 m
Wing load: 9.23 lb/sq.ft / 45.0 kg/sq.m
Range: 191 nm / 354 km
Crew: 3

Engine: Armstrong Siddeley Cheetah Va, 285 hp.
Max speed: 130 mph.

Avro 626 landplane
Engine: 1 x 240hp Armstrong Siddeley Lynx IVC
Take-off weight: 1249 kg / 2754 lb
Empty weight: 801 kg / 1766 lb
Wingspan: 10.36 m / 34 ft 0 in
Length: 8.08 m / 27 ft 6 in
Height: 2.92 m / 10 ft 7 in
Wing area: 27.87 sq.m / 299.99 sq ft
Max. speed: 180 km/h / 112 mph
Cruise speed: 153 km/h / 95 mph
Ceiling: 4511 m / 14800 ft
Range: 386 km / 240 miles

 

 


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