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Focke-wulf Fw 44 Stieglitz




The Focke-Wulf Fw 44 was a two-seater biplane known as the ''Stieglitz'' (Goldfinch) designed in Germany . It was produced by Focke-Wulf as a two-seat civilian Bi-plane for pilot training and sport flying.


DESIGN AND DEVELOPMENT

The first prototype flew in 1932. After many tests and modifications to increase the plane's durability and aerodynamics, the final Fw 44 proved to have excellent air worthiness.

A second version of the Fw 44 was the Fw 44B, which had an Argus AS 8 four-cylinder inverted inline air-cooled engine of 120 horsepower. This made the plane have a more slender, aerodynamic nose than the last engine the Fw 44 had. 20 Fw 44s purchased by China were modified for combat missions and participated in the early stage of Second Sino-Japanese War until all were lost in actions.

The last series version was Fw 44J, which was sold or built on license in several countries around the world.


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SPECIFICATIONS (FW 44)


  plane Or Copter plane
  jet Or Prop prop
  crew two, student and instructor
  length Main 730 m
  length Alt 23 ft 11 in
  span Main 90 m
  span Alt 29 ft 6 in
  height Main 280 m
  height Alt 9 ft 2 in
  area Main 20 m&2
  area Alt 2152 ft&2
  empty Weight Main 565 kg
  empty Weight Alt 1,243 lb
  loaded Weight Main 770 kg
  loaded Weight Alt 1,694 lb
  max Takeoff Weight Main 785 kg
  max Takeoff Weight Alt 1,727 lb
  engine (prop) Siemens Sh 14 A-4
  type Of Prop 7-cylinder radial engine
  number Of Props 1
  power Main 118 kW at 2,100 rpm
  power Alt 160 hp
  max Speed Main 185 km/h
  max Speed Alt 115 mi
  range Main 550 km
  range Alt 340 mi
  ceiling Main 3,900 m
  ceiling Alt 12,790 ft
  climb Rate Main 17 m/s
  climb Rate Alt 56 ft/s



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