PWS-24

From Wikipedia, the free encyclopedia

PWS-24
Type Passenger aircraft
Manufacturer PWS
Maiden flight August 1931
Primary user Polish civilian aviation
Produced 1933-1935
Number built 11

The PWS-24 was a Polish 6-seater passenger aircraft, used from 1933 to 1933 by the LOT Polish Airlines. It was the only aircraft of domestic design used by the LOT before the war.

Contents

[edit] Development

The aircraft was a development of an unsuccessful PWS-21, utilizing its wing of light construction. 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 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 the LOT airlines, built in 1933 (markings: SP-AJF, -AJG, -AJH, -AJJ, -AJK).

In 1932, a prototype was fitted with stronger engine Lorraine Algol (300 hp), instead of Wright Whirlwind J5 (240 hp). Then, it was tested with Pratt & Whitney Wasp Junior (400 hp) engine. Maximum speed raised from 185 to 225 km/h, comparing with 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. -AJH).

[edit] 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 engine 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-24 were broken up. The last SP-AJJ was broken up in 1938.

In 1935 PWS-24bis entered service in LOT. They were used there however only until 1936. PWS-24bis SP-AMR was sold to the Polish Air Force and used as staff machine. SP-ASY and -AMN were broken up in 1936-1937, SP-AMO was crashed at that time during tests.

The remaining two PWS-24bis (SP-AMP and-AMS) were converted to aerial photography in 1936 and used by the outbreak of World War II in September 1939. After the German invasion, SP-AMP was damaged, while SP-AMS was evacuated to Romania, where it was taken over by the Romanian aviation and used by them to aerial photography.

[edit] Description

Mixed construction passenger high-wing cantilever monoplane, with closed cab. A fuselage of a metal frame, covered with canvas on a wooden frame. Two-spar elliptical wings, of wooden construction, canvas and plywood covered. A passenger cabin in a fuselage, with a pair of doors. Crew of two, with double controls. Two-blade metal propeller. Conventional landing gear, with a rear skid. Fuel tanks 260 l in wings.

Engine:

General characteristics

  • Crew: 2, pilot and mechanic
  • Capacity: 4
  • Length: 9.65 m ()
  • Wingspan: 15 m ()
  • Height: 2.95 m ()
  • Wing area: 31.75 m² (ft²)
  • Empty weight: 1220 kg ()
  • Loaded weight: 2000 kg ()
  • Useful load: 780 kg ()
  • Powerplant:Pratt and Whitney Wasp Junior TB air-cooled 9-cylinder radial, 420 hp ()

Performance

Related development

PWS-21

Comparable aircraft

PWS-54 - Lublin R-XVI

Designation sequence

PWS-18 - PWS-19 - PWS-20 - PWS-21 - PWS-24 - PWS-26 - PWS-33 - PWS-35 - PWS-40


[edit] References

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