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Avro 641 Commodore

The Avro 641 Commodore was a British single-engine five-seat cabin biplane built by Avro in the mid-1930s for private use. A total of only six were built, including the prototype.

Commodore
Role Tourer
National origin United Kingdom
Manufacturer Avro
First flight 1934
Introduction 24 May 1934
Retired 1942
Number built 6

Design and development

After building the three seat Avro 639 Cabin Cadet, Avro then designed a larger, five seat cabin biplane, the Avro 641 Commodore. The Commodore had a similar steel tube structure to the Tutor, with heavily staggered single bay wings and a spatted undercarriage. The first Commodore was delivered to its owner on 24 May 1934.[1]

Operational history

Only six Commodores were built, with one being sold to the Maharajah of Vizianagram. This was found to be unsuitable for Indian conditions and was returned to Britain and scrapped.[2] Two were sold to private owners in Egypt and were later taken over by the Egyptian Army Air Force.[1]

The two Commodores that remained in service in England on the outbreak of World War II were impressed into service with the Royal Air Force and the Air Transport Auxiliary. One crashed fatally in 1941, with the last being struck off charge in 1942.[1]

Operators

  Egypt
  United Kingdom

Specifications (Commodore)

 
Avro 641 Commodore 3-view drawing from NACA-AC-193

Data from Avro Aircraft since 1908 [1]

General characteristics

  • Crew: 1
  • Capacity: 4 pax
  • Length: 27 ft 3 in (8.31 m)
  • Wingspan: 37 ft 4 in (11.38 m)
  • Height: 10 ft 0 in (3.05 m)
  • Wing area: 307 sq ft (28.5 m2)
  • Empty weight: 2,237 lb (1,015 kg)
  • Gross weight: 3,500 lb (1,588 kg)
  • Fuel capacity: 50 imp gal (60 US gal; 227 l)
  • Powerplant: 1 × Armstrong Siddeley Lynx IVC 7-cylinder air-cooled radial piston engine, 215 hp (160 kW)
  • Propellers: 2-bladed Fairey-Reed fixed-pitch metal propeller

Performance

  • Maximum speed: 130 mph (210 km/h, 110 kn)
  • Cruise speed: 110 mph (180 km/h, 96 kn)
  • Range: 500 mi (800 km, 430 nmi)
  • Service ceiling: 11,500 ft (3,500 m)
  • Rate of climb: 700 ft/min (3.6 m/s)
  • Wing loading: 11.4 lb/sq ft (56 kg/m2)
  • Power/mass: 0.061 hp/lb (0.100 kW/kg)

See also

Related lists

References

  1. ^ a b c d Jackson, A J (1990). Avro Aircraft since 1908 (2nd ed.). London: Putnam Aeronautical Books. ISBN 0-85177-834-8.
  2. ^ Jackson, A.J. (1974). British Civil Aircraft since 1919 Volume 1. London: Putnam. ISBN 0-370-10006-9.

avro, commodore, british, single, engine, five, seat, cabin, biplane, built, avro, 1930s, private, total, only, were, built, including, prototype, commodorerole, tourernational, origin, united, kingdommanufacturer, avrofirst, flight, 1934introduction, 1934reti. The Avro 641 Commodore was a British single engine five seat cabin biplane built by Avro in the mid 1930s for private use A total of only six were built including the prototype CommodoreRole TourerNational origin United KingdomManufacturer AvroFirst flight 1934Introduction 24 May 1934Retired 1942Number built 6 Contents 1 Design and development 2 Operational history 3 Operators 4 Specifications Commodore 5 See also 6 ReferencesDesign and development EditAfter building the three seat Avro 639 Cabin Cadet Avro then designed a larger five seat cabin biplane the Avro 641 Commodore The Commodore had a similar steel tube structure to the Tutor with heavily staggered single bay wings and a spatted undercarriage The first Commodore was delivered to its owner on 24 May 1934 1 Operational history EditOnly six Commodores were built with one being sold to the Maharajah of Vizianagram This was found to be unsuitable for Indian conditions and was returned to Britain and scrapped 2 Two were sold to private owners in Egypt and were later taken over by the Egyptian Army Air Force 1 The two Commodores that remained in service in England on the outbreak of World War II were impressed into service with the Royal Air Force and the Air Transport Auxiliary One crashed fatally in 1941 with the last being struck off charge in 1942 1 Operators Edit EgyptEgyptian Army Air Force United KingdomAir Transport Auxiliary Royal Air ForceSpecifications Commodore Edit Avro 641 Commodore 3 view drawing from NACA AC 193 Data from Avro Aircraft since 1908 1 General characteristicsCrew 1 Capacity 4 pax Length 27 ft 3 in 8 31 m Wingspan 37 ft 4 in 11 38 m Height 10 ft 0 in 3 05 m Wing area 307 sq ft 28 5 m2 Empty weight 2 237 lb 1 015 kg Gross weight 3 500 lb 1 588 kg Fuel capacity 50 imp gal 60 US gal 227 l Powerplant 1 Armstrong Siddeley Lynx IVC 7 cylinder air cooled radial piston engine 215 hp 160 kW Propellers 2 bladed Fairey Reed fixed pitch metal propellerPerformance Maximum speed 130 mph 210 km h 110 kn Cruise speed 110 mph 180 km h 96 kn Range 500 mi 800 km 430 nmi Service ceiling 11 500 ft 3 500 m Rate of climb 700 ft min 3 6 m s Wing loading 11 4 lb sq ft 56 kg m2 Power mass 0 061 hp lb 0 100 kW kg See also EditRelated lists List of aircraft of the Royal Air ForceReferences Edit Wikimedia Commons has media related to Avro 641 Commodore a b c d Jackson A J 1990 Avro Aircraft since 1908 2nd ed London Putnam Aeronautical Books ISBN 0 85177 834 8 Jackson A J 1974 British Civil Aircraft since 1919 Volume 1 London Putnam ISBN 0 370 10006 9 Retrieved from https en wikipedia org w index php title Avro 641 Commodore amp oldid 1065823398, wikipedia, wiki, book, books, library,

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