PWS-11
title: "PWS-11" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["1920s-polish-military-trainer-aircraft", "1930s-polish-sport-aircraft", "pws-aircraft", "single-engined-tractor-aircraft", "aircraft-first-flown-in-1929", "aircraft-with-fixed-conventional-landing-gear"] topic_path: "geography/poland" source: "https://en.wikipedia.org/wiki/PWS-11" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0
::data[format=table title="Infobox aircraft"]
| Field | Value |
|---|---|
| name | PWS-11 |
| image | PWS-11SM.jpg |
| caption | PWS-11SM |
| aircraft_type | Trainer aircraft |
| manufacturer | PWS |
| status | prototype |
| number_built | 2 |
| first_flight | 1929 |
| :: |
| name = PWS-11 | logo = | logo_size = | image = PWS-11SM.jpg | alt = | caption = PWS-11SM | long_caption = | other_names = | aircraft_type = Trainer aircraft | aim = | outcome = | related = | national_origin = | manufacturer = PWS | design_group = | designer = | builder = | issuer = | status = prototype | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = 2 | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = 1929 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded =
The PWS-11 was a Polish aerobatic and trainer aircraft, developed in 1928-1929 by PWS (Podlaska Wytwórnia Samolotów - Podlasie Aircraft Factory), which remained a prototype.
Design and development
::figure[src="https://upload.wikimedia.org/wikipedia/commons/e/e1/PWS-11bis.jpg" caption="PWS-11bis"] ::
In parallel with development of a fighter aircraft, the PWS-10, the design team of Aleksander Grzędzielewski and Augustyn Bobek-Zdaniewski from the PWS factory, started work on an intermediate aircraft for training fighter pilots. Like the PWS-10, the new plane was of a parasol wing configuration, but the shape of the fuselage, wings and empennage were similar to a liaison aircraft, the PWS-5 of the same designers and powered by the same engine. In 1929, the Aviation Department of the Polish War Ministry ordered the prototypes and an airframe for static tests. The plane was initially known as PWS-11SM, for szkolno-myśliwski (fighter/trainer).
The first prototype of the PWS-11 was flown in November 1929 at Biała Podlaska by Franciszek Rutkowski. Its handling characteristics were lacking and as a result, its empennage underwent several modifications. The second prototype of 1930, designated the PWS-11bis was much improved. The rectangular section fuselage was replaced by an oval one and an engine was fitted with a Townend ring. After further changes to the empennage and Townend ring, the aircraft was then highly maneuverable and was found satisfactory. The Air Force however was not interested and the plane was not built in series.
Operational history
The second prototype PWS-11bis received a registration number SP-ADS and was used for aerobatics, flown by Col. J. Kossowski, among others.
Construction
The PWS-11 was a single-seater parasol wing monoplane of wooden construction. The framed fuselage had a skin made of plywood (PWS-11) or aircraft fabric on wood strips (PWS-11bis), except for the engine compartment which was covered with duralumin sheeting. The rectangular wooden wings had two spars, which were covered with fabric and plywood and were supported by twin struts. The empennage was wooden, with the fixed surfaces plywood covered and fabric on the control surfaces. The pilot sat in an open cockpit, protected by a windshield. The undercarriage consisted of a fixed common axle conventional landing gear, with a rear skid. Fuel was carried in a 170 L tank mounted in the fuselage, forward of the pilot's cockpit.
The 9-cylinder Skoda-Wright Whirlwind J-5B air-cooled radial engine was built under licence in the Polish Skoda Works, giving a nominal power of 220 hp (164 kW) and take-off power of 240 hp (179 kW), driving a two-blade fixed pitch wooden propeller. A cruise fuel consumption was 48 L/h.
Specification (PWS-11bis)
|ref=Polskie konstrukcje lotnicze 1893–1939, Polish aircraft 1893-1939 |prime units?=met General characteristics
|crew=2 |length m=6.7 |length note= |span m=9 |span note= |height m=2.44 |height note= |wing area sqm=15 |wing area note= |aspect ratio= |airfoil=Bobek-Zdaniewski No.3 (Göttingen 647) |empty weight kg=666 |empty weight note= |gross weight kg=934 |gross weight note= |max takeoff weight kg= |max takeoff weight note= |fuel capacity= |more general= Powerplant
|eng1 number=1 |eng1 name=Skoda-Wright J-5B Whirlwind |eng1 type=9-cylinder air-cooled radial piston engine |eng1 kw= |eng1 hp=220 |eng1 note=
|prop blade number=2 |prop name=Szomański fixed pitch propeller |prop dia m= |prop dia note= Performance
|max speed kmh=210 |max speed note=at sea level ::::197 km/h at 2000 m |cruise speed kmh=180 |cruise speed note= |stall speed kmh=91 |stall speed note= |never exceed speed kmh= |never exceed speed note= |range km=630 |range note= |ferry range km= |ferry range note= |endurance= |ceiling m=4950 |ceiling note= |g limits= |roll rate= |climb rate ms= |climb rate note= |time to altitude=
:*1000 m in 2 minutes 44 seconds :*3000 m in 10 minutes 13 seconds |wing loading kg/m2=62.2 |wing loading note= |fuel consumption kg/km= |power/mass=0.0787 hp/lb |more performance=
References
References
- Glass, Andrzej. (1977). "Polskie konstrukcje lotnicze 1893–1939 [Polish aviation designs 1893–1939]". WKiŁ.
- (1971). "Polish aircraft 1893-1939". Putnam.
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