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General Aircraft Monospar ST 25

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Top speed
  
229 km/h

Length
  
8.03 m

Manufacturer
  
General Aircraft Limited

Wingspan
  
12 m

First flight
  
June 19, 1935

General Aircraft Monospar ST-25 httpsuploadwikimediaorgwikipediacommonsthu

The General Aircraft Monospar ST-25 was a British 1930s light twin-engined utility aircraft.

Contents

Design and development

The Monospar ST-25 was a low-wing cantilever monoplane with a fabric-covered metal structure. The monospar name came from the use of a single spar in the wing structure, that had been developed by H J Stieger. The cabin was enclosed with five seats. It was based on the GAL Monospar ST-10, with the addition of a folding seat for a fifth passenger, extra side windows, and the addition of a radio receiver. On 19 June 1935, the prototype (G-ADIV) made its first flight at Hanworth Air Park. It was designated Monospar ST-25 Jubilee, to honour the 25th anniversary of the reign of King George V.

Operational history

  • The last flying Monospar ST-25 (ZK-AFF), of Piet Van Asch, the owner of New Zealand Aerial Mapping Ltd, was lost in 1986 in a hangar fire.
  • The last surviving Monospar ST-25 (OY-DAZ), an ST-25 Ambulance, was fully restored during 1989-1999, and is now displayed in Egeskov Veteranmuseum at Egeskov Castle, Denmark.
  • Variants

    Monospar ST-25 Jubilee
    (1935-1936) Single fin and rudder. 30 built.
    Monospar ST-25 De Luxe
    One Monospar ST-25 Jubilee with a large single fin and two Niagara II engines, later converted to the prototype Monospar ST-25 Universal, with twin fins.
    Monospar ST-25 Ambulance
    Variants of both Monospar ST-25 Jubilee and ST-25 Universal, with a large door on the starboard side to allow a stretcher to be loaded.
    Monospar ST-25 Universal
    (1936-1939) Twin fin and twin rudder. 29 built, including the conversion of the De Luxe.
    Monospar ST-25 Freighter
    A variant of the Monospar ST-25 Universal, with a large freight door but without the passenger seating.
    GAL.26
    One modified Monospar ST-25 Jubilee, fitted with two Cirrus Minor I engines in 1936.
    GAL.41
    One experimental aircraft based on the Monospar ST-25 Universal. A new fuselage was built containing a pressurized section with two seats. Its purpose was to test possible pressurization systems for a proposed airliner, the GAL.40. The GAL.41 flew for the first time 11 May 1939, and was grounded in 1941.

    Operators

     Australia
  • Adelaide Airways
  •  Canada
  • Eastern Canada Air Lines (five ST-25 Freighters, delivered in 1936)
  •  Denmark
     France
  • Armée de l'Air (2 ST-25 in Indochine (Vietnam) in November 1945)
  •  Netherlands
  • Van Melle's Confectionery Works, Breskens (one Jubilee, PH-IPM "Dubbele Arend', delivered in 1935)
  •  New Zealand
  • New Zealand Aerial Mapping
  • Royal New Zealand Air Force
  •  Romania
  • Royal Romanian Air Force
  •  Spain
  • Spanish Republican Air Force
  •  Spain
  • Spanish Air Force
  •  Turkey
  • General Command of Mapping (Turkey)
  • Turkish Government (two ST-25 Freighters for parachute training delivered in 1937)
  •  United Kingdom
  • Crilly Airways
  • Royal Aircraft Establishment (two Jubilees used for radio development)
  • Royal Air Force (impressed civil aircraft used during the second world war)
  • Specifications (Monospar ST-25 Jubilee)

    Data from Jackson, 1973

    General characteristics

  • Crew: one
  • Length: 26 ft 4 in (8.03 m)
  • Wingspan: 40 ft 2 in (12.24 m)
  • Height: 7 ft 10 in (2.39 m)
  • Wing area: 217 sq ft (20.2 m2)
  • Empty weight: 1,680 lb (762 kg)
  • Gross weight: 2,875 lb (1,304 kg)
  • Powerplant: 2 × Pobjoy Niagara II 7-cyl. air-cooled radial piston engine, 90 hp (67 kW) each
  • Performance

  • Maximum speed: 142 mph (229 km/h; 123 kn)
  • Range: 585 mi (508 nmi; 941 km)
  • Service ceiling: 16,000 ft (4,900 m)
  • Rate of climb: 800 ft/min (4.1 m/s)
  • References

    General Aircraft Monospar ST-25 Wikipedia