PWS-19

The PWS-19 was a Polish reconnaissance and bomber aircraft prototype of the 1930s. 

Only one prototype was built.

Specifications

Crew

2 

Length

9.17 m (30 ft 1 in)

Wingspan

14.5 m (47 ft 7 in)

Height

3.16 m (10 ft 4 in)

Wing area

29 m2 (310 sq ft)

Empty weight

1,340 kg (2,954 lb)

Gross weight

1,950 kg (4,299 lb)

Max take-off weight

2,185 kg (4,817 lb)

Powerplant

1 × Pratt & Whitney Hornet T2 9-cylinder air-cooled radial piston engine, 391 kW (525 hp) (nominal)

Propellers

2-bladed fixed-pitch propeller

Performance

Maximum speed

234 km/h (145 mph, 126 kn)

Cruise speed

190 km/h (120 mph, 100 kn)

Stall speed

99 km/h (62 mph, 53 kn) ~

Range

700 km (430 mi, 380 nmi)

Service ceiling

7,200 m (23,600 ft)

Rate of climb

7.5 m/s (1,480 ft/min)

Wing loading

67 kg/m2 (14 lb/sq ft)

Armament

Guns

2 x 7.7 mm Vickers machine guns

(1 forward-firing, 1 movable),

Bombs

250 kg (550 lb) bombs.