PZL P.11c Specification  



PZL P.11c Specification

AvStop Online Magazine

 


Manufacturer: Panstwowe Zaklady Lotnicze (PZL) Warsaw, Poland
Crew:  One (pilot)
Powerplant: One PZL Bristol Mercury VS2 engine driving wooden 2-bladed Szomanski propeller, rated at 560 hp (441 kW) for take-off 

Dimensions

Wingspan:  10.72 m (35' 2") Length:  7.55 m (24' 9") Height:  2.85 m (9' 4") 

Weights

Empty:  1022 kg (2256 lb) Normal Take-off:  1650 kg (3642 lb) Max Take-off:  1800 kg (3974 lb) 

Armament

Fixed:  Two synchronized forward-firing 7.9 mm PWU wz.33 machine guns in the fuselage and (on some aircraft) additional two wing-mounted 7.9 mm machine guns
Disposable:  Four 12,5 kg bombs (two under each wing)

Performance

Maximum speed:  375 km/h (233 mph) at 5000 m (16405 ft), 276 km/h (172 mph) at sea level.
Cruise speed: 250 km/h (155 mph)
Stalling speed: 120 km/h (74.6 mph)
Climb: Initial 12.4 m/s (2441 ft/min), time to 2000 m (6561 ft) 2 min 29 s.
Service ceiling: 8040 m (26378 ft)
Range: 550 km (342 miles) 
 
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