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Contents

   



(Top)
 


1 Development  





2 Usage  





3 Operators  





4 Description  





5 Specifications (PWS-24bis)  





6 See also  





7 References  





8 External links  














PWS-24






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From Wikipedia, the free encyclopedia
 


PWS-24
Role Passenger aircraft
Manufacturer PWS
First flight August 1931
Introduction 1933
Primary user Polish civilian aviation (LOT Polish Airlines)
Produced 1933-1935
Number built 11

The PWS-24 was a Polish single-engine passenger aircraft for 4 passengers, built in PWS factory, used from 1933to1936byLOT Polish Airlines. In spite of its limited capacity, it was the only series-built airliner of domestic design ever used by the LOT.[1]

Development

[edit]

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 1931inBiała 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 hpLorraine Algol, instead of the 240 hpWright Whirlwind J-5. It was later tested with a 400 hpPratt & Whitney Wasp Junior engine. Maximum speed improved from 185 to 225 km/h, comparing with the basic variant.

In1934 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

[edit]

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,[2] 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.[2]

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.[3] It was broken up after an accident 8 September 1940.[3]

Operators

[edit]
 Poland
 Romania

Description

[edit]

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)

[edit]

Data from [citation needed]

General characteristics

Performance

See also

[edit]

Related development

Aircraft of comparable role, configuration, and era

References

[edit]
  1. ^ PZL.4, PZL.27, PZL.44 Wicher and PZL MD-12 were evaluated by LOT, being prototypes.
  • ^ a b Morgała 2003, p. 310
  • ^ a b Mazur 2016, p. 51-57
  • [edit]
    Retrieved from "https://en.wikipedia.org/w/index.php?title=PWS-24&oldid=1073233802"

    Categories: 
    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
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    This page was last edited on 21 February 2022, at 17:37 (UTC).

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