Main Menu



A parallel development to the P.6, from which it differed essentially in having a higher-altitude engine and some steel elements in the otherwise all-duralumin fuselage structure, the P.7 was powered by a supercharged Bristol Jupiter VII.F radial affording 520hp at 3050m. The first of two prototypes, the P.7/I, was flown in October 1930, and featured a close-fitting, helmeted engine cowling, which gave place to a Townend ring on the P.7/II. Work on a pre-series batch of 10 of the P.7a fighters began in June 1931 for the Lotnictwo Wojskowe, a further 139 being subsequently ordered. The P.7a carried two 7.92mm Vickers "E" machine guns and differed from the prototypes in having a P.Z.L.-developed ring cowling, a revised cockpit, shorter ailerons and modified tail surfaces. The P.7a entered service in the winter of 1932-33, and three first line squadrons were still equipped with this type when the Wehrmacht assault on Poland was launched on 1 September 1939.

Max take-off weight: 1476 kg / 3254 lb
Empty weight: 1090 kg / 2403 lb
Wingspan: 10.57 m / 35 ft 8 in
Length: 6.98 m / 23 ft 11 in
Height: 2.69 m / 9 ft 10 in
Wing area: 17.90 sq.m / 192.67 sq ft
Max. speed: 327 km/h / 203 mph
Range: 600 km / 373 miles





Copyright © 2020 all-aero. All Rights Reserved.
Joomla! is Free Software released under the GNU General Public License.