Type sheet: fw44

Focke Wulf FW 44 Stieglitz
Training and sports aircraft, Germany, 1934

[Technical Data] [Expo/Images] - [ Focke Wulf] [ General Aviation 1919-1938] [ Trainer 1919-1938]

Description:

The Stieglitz wasd developed by Kurt Tank. It was
designed as a biplane to get an aircraft that is
specially suited to aerobatics training.

Sizes and weights

Total Length :

23.950 ft

7.300 m

Greatest height :

8.858 ft

2.700 m

Wingspan :

29.528 ft

9.000 m

Wing area :

215.280 sqft

20.000 qm

Max take off weight :

1940.4 lbs

880.0 kg

Weight empty :

1245.8 lbs

565.0 kg

Max. weight carried :

694.6 lbs

315.0 kg

Performance data

Max. speed :

100 kts

185 km/h

Initial climb rate :

807.09 ft/min

4.10 m/s

Service ceiling :

12795 ft

3900 m

Wing load :

9.02 lbs/ft2

44.00 kg/qm

Range :

351 nm

650 km

Endurance :

4 h

4 h

Propulsion

Kind :

KSte

Type :

Siemens Sh-14 a Bramo

Power rating (max.) :

158 hp

160 ps

Count :

1

1

Total power rating (max.) :

158 hp

160 ps

Other

Crew :

0

0

2