page_title: Payen PA-22
section_title: Specifications
hierarchical_section_title: Payen PA-22 / Specifications
caption_attribution_description: English: Payen Pa-112 3-view drawing from L'Aerophile October 1938
context_page_description: The Payen PA-22 was a French experimental aircraft designed by Nicolas Roland Payen.
  The aircraft had an unconventional design: it had a set of delta wings, in front of which were a set of short conventional wings. It had a fixed front landing gear and the cockpit was further back than usual.
context_section_description: General characteristics
  Crew: 1
  Length: 7.48 m (24 ft 6 in)
  Wingspan: 4.8 m (15 ft 9 in)
  Height: 2.35 m (7 ft 9 in)
  Wing area: 10 m² (110 sq ft)
  Empty weight: 560 kg (1,235 lb)
  Max takeoff weight: 955 kg (2,105 lb)
  Powerplant: 1 × Regnier R.6 6-cyl. inverted air-cooled in-line piston engine, 130 kW (180 hp)
  Performance
  Maximum speed: 360 km/h (220 mph, 190 kn)
  Cruise speed: 330 km/h (205 mph, 178 kn)
  Range: 1,200 km (750 mi, 650 nmi)
  Service ceiling: 5,600 m (18,500 ft)
caption: Payen Pa-112 3-view drawing from L'Aerophile October 1938
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