Single-engine pistonPolish touring and sports aircraft
PZL.5
The PZL-5 was a Polish two-seat touring and sports aircraft of 1930 constructed and produced by the PZL.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- PZL
- Category
- Single-engine piston
- Country of origin
- Second Polish Republic
- First flight
- 1930-05-01
Specifications
- Cruise speed
- 70 kt
- Max speed
- 89 kt
- Range
- 290 nm
- Service ceiling
- 12,188 ft
- Rate of climb
- 670 ft/min
- Max takeoff weight
- 1,642 lb
- Empty weight
- 950 lb
- Fuel capacity
- 25.3 US gal
- Powerplant
- de Havilland Gipsy I
- Engines
- 1
- Seats
- 2
- Length
- 22 ft
- Wingspan
- 27 ft
- Height
- 8 ft
- Number built
- 15
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.