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Miles Merlin

From Wikipedia, the free encyclopedia

M.4A Merlin
RoleFive-seat cabin monoplane
Type of aircraft
ManufacturerMiles Aircraft Limited
DesignerFrederick George Miles
First flight11 May 1935
Number built4
Developed fromMiles M.3 Falcon

TheMiles M.4A Merlin was a 1930sBritish five-seat cabin monoplane built byMiles Aircraft Limited.

Design and development

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TheMerlin was designed by F.G. Miles ofPhilips and Powis, as a result of collaboration with G. Birkett of Birkett Air Service Ltd, and Tata Sons Ltd of India. It was based on the three-seat and four-seat versions of theM.3 Falcon, but with wider fuselage and consequent increased wing span. It was a low-wing monoplane, with fixed main undercarriage in trouser fairings plus a fixed tailwheel. Construction was mainly of wood, with spruce frames and three-ply birch covering, and the wings had hydraulically operated split flaps. It was powered by a 200 hpde Havilland Gipsy Six piston engine. It was first designated M.4 Merlin, but all four examples were completed as M.4A Merlin, with fixed pitch propeller instead of the intended variable pitch unit.[1][2][3]

Operational history

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On 11 May 1935, the prototype (U-8, later G-ADFE), built byPhilips and Powis (Miles Aircraft), first flew atWoodley Aerodrome, piloted by F.G. Miles. A few weeks later, the Merlin was delivered to Birkett Air Service, for its air taxi and charter business based atHeston Aerodrome. Two aircraft were built and delivered to Tata Sons Ltd for itsTata Air Lines service on theKarachi-Madras route. The fourth and final Merlin was delivered to E. Chaseling ofVictorian and Interstate Airways inAustralia, for itsMelbourne-Hay service. In 1940, the Australian Merlin was pressed into service with theRoyal Australian Air Force.[1][2]

Operators

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 Australia
 India
 United Kingdom
  • Birkett Air Services

Specifications (M.4A)

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3-view line drawing of the Miles M.4A
3-view line drawing of the Miles M.4A

Data from Lukins & Russell[4]

General characteristics

  • Crew: 1
  • Capacity: 4 passengers
  • Length: 25 ft 10 in (7.87 m)
  • Wingspan: 37 ft 0 in (11.27 m)
  • Height: 9 ft 7 in (2.92 m)
  • Wing area: 196 sq ft (18.21 m2)
  • Empty weight: 1,700 lb (770 kg)
  • Gross weight: 3,000 lb (1,360 kg)
  • Powerplant: 1 ×de Havilland Gipsy Six piston engine , 200 hp (150 kW)

Performance

  • Maximum speed: 155 mph (250 km/h, 135 kn)
  • Cruise speed: 145 mph (245 km/h, 126 kn)
  • Range: 700 mi (1,130 km, 610 nmi)
  • Service ceiling: 18,000 ft (5,490 m)
  • Rate of climb: 900 ft/min (4.6 m/s)

See also

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Notes

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  1. ^abBrown 1970, pp. 87-88
  2. ^abJackson 1988, pp. 57-58
  3. ^Flight, 4 April 1935, pp. 351-353
  4. ^Lukins & Russell 1945, p. 32

Bibliography

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Wikimedia Commons has media related toMiles Merlin.
  • Amos, Peter. and Brown, Don Lambert.Miles Aircraft Since 1925, Volume 1. Putnam, 2000.ISBN 0-85177-787-2.
  • Brown, Don Lambert.Miles Aircraft Since 1925. Putnam, 1970.ISBN 0-370-00127-3.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing.
  • Jackson, A.J.British Civil Aircraft since 1919. Putnam, 1974.ISBN 0-370-10014-X.
  • Jackson, A.J.British Civil Aircraft since 1919, Volume 3. Putnam, 1988.ISBN 0-85177-818-6.
  • Lukins, A.H. and Russell, D.A.The book of Miles aircraft. Harborough 1945.
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