PWS-24

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1930s Polish passenger aircraft

title: "PWS-24" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["1930s-polish-airliners", "1930s-polish-civil-utility-aircraft", "1930s-polish-military-utility-aircraft", "pws-aircraft", "single-engined-tractor-aircraft", "high-wing-aircraft", "aircraft-first-flown-in-1931", "aircraft-with-fixed-conventional-landing-gear"] description: "1930s Polish passenger aircraft" topic_path: "geography/poland" source: "https://en.wikipedia.org/wiki/PWS-24" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary 1930s Polish passenger aircraft ::

::data[format=table title="Infobox aircraft"]

FieldValue
namePWS-24
imagePws-24.jpg
typePassenger aircraft
manufacturerPWS
first_flightAugust 1931
introduction1933
primary_userPolish civilian aviation (LOT Polish Airlines)
produced1933-1935
number_built11
::

|name =PWS-24 |image =Pws-24.jpg |caption = |type =Passenger aircraft |manufacturer =PWS |designer = |first_flight =August 1931 |introduction = 1933 |retired = |status = |primary_user =Polish civilian aviation (LOT Polish Airlines) |more_users = |produced =1933-1935 |number_built =11 |variants =

The PWS-24 was a Polish single-engine passenger aircraft for 4 passengers, built in PWS factory, used from 1933 to 1936 by LOT Polish Airlines. In spite of its limited capacity, it was the only series-built airliner of domestic design ever used by the LOT.

Development

The aircraft was a development of an unsuccessful PWS-21, utilizing its lightweight construction wing (weight 300 kg). A fuselage and stabilizers were new. The main designer was Stanisław Cywiński. The prototype (markings SP-AGR) first flew in August 1931 in Biała Podlaska. After trials and some modifications, it won a Ministry of Communication's contest for a successor of Junkers F-13 in LOT airlines, against Lublin R-XVI. In June 1932 it took the first place in a passenger aircraft race at the international air meeting in Warsaw.

Polish Ministry of Communication ordered a series of 5 aircraft for LOT airlines, built in 1933 (markings: SP-AJF, -AJG, -AJH, -AJJ, -AJK). In 1932, the prototype SP-AGR was fitted with a more powerful engine, the 300 hp Lorraine Algol, instead of the 240 hp Wright Whirlwind J-5. It was later tested with a 400 hp Pratt & Whitney Wasp Junior engine. Maximum speed improved from 185 to 225 km/h, comparing with the basic variant.

In 1934 a production of further 5 aircraft started, with Wasp Junior engines, designated PWS-24bis (markings: SP-AMN, -AMO, -AMP, -AMR, -AMS). Also one PWS-24 was converted to PWS-24bis (SP-ASY, ex. SP-AJH).

Usage

PWS-24 were put into use in LOT Polish Airlines from May 1, 1933 on domestic lines. Their flight characteristics and durability proved however worse, than of single-engined Fokker F.VIIa/1m, used by LOT, so their service was not long. In 1935 three PWS-24 (SP-AGR, -AJF, -AJJ) were converted to aerial photography variant, but in 1936 four PWS-24s were broken up. The last, SP-AJJ, was broken up in 1938.

PWS-24bis entered service in LOT in 1935. They were used there however only until 1936. PWS-24bis SP-AMR was sold in April 1935 to the Polish Air Force and used as a staff machine. It had a slight accident and compulsory landing on 27 April 1935, its further fate is not known. SP-ASY and -AMN were broken up in 1936-1937. SP-AMO was sold in 1936 to Maritime and Colonial League paramilitary organization and soon crashed in July 1936 during testing of a new variable-pitch propeller.

The remaining two PWS-24bis (SP-AMP and-AMS) were converted to aerial photography in 1936 and used until the outbreak of World War II in September 1939. After the German invasion, SP-AMP was damaged during bombing, while SP-AMS was evacuated to Romania, where it was seized by Romanian government in February 1940 and later used by the LARES line to aerial photography. It was broken up after an accident 8 September 1940.

Operators

;Poland

Description

High-wing cantilever monoplane of mixed construction, with closed cab and single engine. A fuselage of a steel frame, covered with canvas on a wooden frame. Straight one-piece wooden wing, with elliptical endings, two-spar, plywood covered. Tailfins of steel frame, canvas covered. Crew of two (pilot and mechanic), in a cab before the wing, with twin controls. Next and below in a fuselage, under the wing, there was a cabin for 4 passengers, with wide rectangular windows and a door on the left side. Radial engine in fuselage front, fitted with a Townend ring. Two-blade metal propeller of variable pitch. Conventional fixed landing gear, with a rear skid; struts with shock absorbers joined the main gear with wings. Fuel tanks 260 L in central wing section (cruise consumption 50-58 L/h in PWS-24, 95 L/h in PWS-24bis).

Engine:

Specifications (PWS-24bis)

::figure[src="https://upload.wikimedia.org/wikipedia/commons/3/30/PWS-24.svg"] ::

|ref= |prime units?=met General characteristics

|crew=2 |capacity=4 |length m=9.65 |length note= |span m=15 |span note= |height m=2.95 |height note= |wing area sqm=31.75 |wing area note= |aspect ratio= |airfoil= |empty weight kg=1220 |empty weight note= |gross weight kg=2000 |gross weight note= |max takeoff weight kg= |max takeoff weight note= |fuel capacity= |more general= Powerplant

|eng1 number=1 |eng1 name=Pratt and Whitney Wasp Junior TB |eng1 type=9-cylinder air-cooled radial piston engine |eng1 hp=420 |eng1 note=

|prop blade number=2 |prop name=variable-pitch propeller |prop dia m= |prop dia note= Performance

|max speed kmh=225 |max speed note= |cruise speed kmh=180 |cruise speed note= |stall speed kmh=90 |stall speed note=~ |never exceed speed kmh= |never exceed speed note= |range km=700 |range note= |ferry range km= |ferry range note= |endurance= |ceiling m=5000 |ceiling note= |climb rate ms=4.2 |climb rate note= |time to altitude= |wing loading kg/m2=63 |wing loading note= |fuel consumption kg/km= |power/mass= |thrust/weight= |more performance= Armament

References

  • Andrzej Glass: "Polskie konstrukcje lotnicze 1893-1939" (Polish aviation constructions 1893-1939), WKiŁ, Warsaw 1977 (Polish language, no ISBN)

References

  1. [[PZL.4]], [[PZL.27]], [[PZL.44 Wicher]] and [[PZL MD-12]] were evaluated by LOT, being prototypes.
  2. Morgała 2003, p. 310
  3. Mazur 2016, p. 51-57

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1930s-polish-airliners1930s-polish-civil-utility-aircraft1930s-polish-military-utility-aircraftpws-aircraftsingle-engined-tractor-aircrafthigh-wing-aircraftaircraft-first-flown-in-1931aircraft-with-fixed-conventional-landing-gear