page_title: Aviméta 88
section_title: Specifications
hierarchical_section_title: Aviméta 88 / Specifications
caption_attribution_description: English: Aviméta 88 3-view drawing from L'Aéronautique December,1926
context_page_description: The Aviméta 88 was an all-metal French two-seat reconnaissance-fighter or heavy fighter tested in 1927.
context_section_description: Data from Flight (2 December 1926)
  General characteristics
  Crew: two
  Length: 9.76 m (32 ft 0 in)
  Wingspan: 17.00 m (55 ft 9 in)
  Height: 3.55 m (11 ft 8 in)
  Wing area: 40 m² (430 sq ft)
  Empty weight: 1,550 kg (3,417 lb)
  Gross weight: 2,400 kg (5,291 lb)
  Fuel capacity: 310 kg (680 lb) (420 l (92 imp gal; 110 US gal)) in crash proof and in-flight jettisonable tank
  Powerplant: 1 × Hispano-Suiza 12Hb water-cooled V-12, 444 kW (595 hp)
  Propellers: 2-bladed
  Performance
  Maximum speed: 240 km/h (150 mph, 130 kn) at sea level, 220 km/h (140 mph) at 5,000 m (16,000 ft)
  Service ceiling: 7,500 m (24,600 ft)
  Time to altitude: 16 min to 5,000 m (16,000 ft)
  Armament
  two fixed, synchronised 7.7 mm (0.303 in) Vickers machine guns firing through propeller disc and two more mounted on the wing.
  pair of Lewis guns on flexible mounting in rear cockpit.
caption: Aviméta 88 3-view drawing from L'Aéronautique December,1926
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