PZL.44 Wicher

· PZL Świdnik

Airplanes

Length

18.45 m

Flat Wing Span

23.8 m

Height

4.8 m

Flat Wing Area

75 m²

Max Seating

Cruise Speed

280 km/h

Max Speed

360 km/h

Max Ceiling

6850 m

Number of Engines

First Flight

1938-03-12

Number Built

Maximum Take-Off Weight

9.5 t (paragliders: kg)

Total Fuel Capacity

1800

Maximum Range

1840 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
PZL.44 Wicher	9.5	1800	1840

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Hall XPTBH		16.764	24.0792		Compare
Dornier Do 23		18.8	25.6		Compare
Amiot 143		18.24	24.53		Compare
Focke-Wulf Fw 42	BMW VI	17.7	25		Compare
Dornier Do 18		19.23	23.7		Compare
Rohrbach Ro V Rocco		19.3	25.9	12	Compare

All data (25 fields)

Name: PZL.44 Wicher
Manufacturer: PZL Świdnik
Description: The PZL.44 Wicher (gale) was a prototype of 14-seat, twin-engine Polish airliner, built in the Państwowe Zakłady Lotnicze (PZL) in 1938.
First Flight: 1938-03-12
Service End: 1939-01-01
Designer: PZL Świdnik
Type: Passenger plane
Length (m): 18.45
Height (m): 4.8
Cockpit Crew: 4
Max Seating: 14
Max Speed (km/h): 360
Cruise Speed (km/h): 280
Min Speed (km/h): 110
Max Ceiling (m): 6850
Rate of Climb (m/s): 6.9342
Capacity Description: 14 passengers
Number Built: 1
Powerplant Description: 2 × Wright GR-1820-G2 Cyclone 9-cylinder air-cooled radial piston engine, 746 kW (1000 hp) each
Primary Users: LOT Polish Airlines
Status: Prototype
Wikipedia Article (URL): en.wikipedia.org/wiki/PZL.44_Wicher
Flat Wing Span (m): 23.8
Flat Wing Area (m²): 75
Number of Engines: 2