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Gourdou-Leseurre GL-820 HY

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GL-820 HY
Role Shipborne reconnaissance / torpedo floatplane
National origin France
Manufacturer Gourdou-Leseurre
First flight

GL-820 HY 10 May 1935
GL-821 HY 28 January 1936
GL-821 HY 02 5 October 1937

Number built

1x GL-820 HY
1 x GL-821 HY
1 x GL-821 HY 02

The Gourdou-Leseurre GL-820 HY family of four-seat single-engined floatplanes were designed and built in France during the latter half of the 1930s by Gourdou-Leseurre. The GL-820 HY and GL-821 HY 02 were shipborne reconnaissance / obeservation aircraft, while the sole GL-821 HY was built as a torpedo carrier.

Design and development

The Gl-820 and GL-821 were low-wing monoplane floatplanes with four tandem open cockpits, (the Cockpits on the GL-821 HY 02 were enclosed). The wings, tailplanes and floats were all supported by a system of streamlined struts.

Variants

GL-820 HY
The initial reconnaissance aircraft prototype, powered by a 730 hp (540 kW) Hispano-Suiza 9Vb driving a two-bladed fixed-pitch wooden propeller.[1]
GL-821 HY
The second aircraft built as a torpedo carrier, powered by a 750 hp (560 kW) Gnome & Rhône 9Kfr.[2]
GL-821 HY 02
The third aircraft, powered by a 750 hp (560 kW) Gnome & Rhône 9Kfr driving a three-bladed metal propeller.[3]

Specifications (GL-821 HY)

Data from Aviafrance : Gourdou Leseurre GL-821 HY[2], Gourdou Leseurre GL-821 HY 02[3], Gourdou Leseurre GL-820 HY[1]

General characteristics

  • Crew: 4
  • Length: 11 m (36 ft 1 in)
  • Wingspan: 16 m (52 ft 6 in)
  • Height: 5.2 m (17 ft 1 in)
  • Wing area: 44 m2 (470 sq ft)
  • Empty weight: 1,950 kg (4,299 lb)
  • Gross weight: 3,200 kg (7,055 lb)
  • Powerplant: 1 × Gnome & Rhône 9Kfr 9-cylinder air-cooled radial piston engine, 560 kW (750 hp)
GL-820 HY: 1 x 730 hp (540 kW) Hispano-Suiza 9Vb 9-cylinder radial

Performance

  • Maximum speed: 220 km/h (140 mph, 120 kn)
Gl-820 HY: 215 km/h (134 mph; 116 kn)
Gl-821 HY 02: 235 km/h (146 mph; 127 kn)
  • Range: 1,000 km (620 mi, 540 nmi)
  • Service ceiling: 7,000 m (23,000 ft)

Armament

  • Guns: 1 × fixed forward firing 7.5 mm (0.295 in) Darne machine gun in the starboard wing; 2x 7.75 mm (0.305 in) Lewis guns on a flexible mount in the rearmost cockpit
  • Bombs: 300 kg (660 lb) of bombs (GL-820 HY and GL-821 HY 02) or one torpedo (GL-821 HY)

References

  1. ^ a b Parmentier, Bruno (29 April 2003). "Gourdou Leseurre GL-820 HY". Aviafrance (in French). Paris. Retrieved 1 February 2019.
  2. ^ a b Parmentier, Bruno (5 August 2001). "Gourdou Leseurre GL-821 HY". Aviafrance (in French). Paris. Retrieved 1 February 2019.
  3. ^ a b Parmentier, Bruno (29 April 2003). "Gourdou Leseurre GL-821 HY 02". Aviafrance (in French). Paris. Retrieved 1 February 2019.
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