Macchi M.71

Macchi M.71
Role	Flying boat fighter
National origin	Italy
Manufacturer	Macchi
First flight	1930
Primary user	Regia Marina (Italian Royal Navy)
Number built	No more than 12
Variants	Macchi M.41bis

The Macchi M.71 was an Italian flying boat fighter of the 1930s designed and manufactured by Macchi.

Design and development

In 1930, Macchi built a new version of its M.41bis flying boat fighter designed for launching by catapult from warships of the Regia Marina (Italian Royal Navy). The new aircraft, the M.71, built to the same dimensions as the M.41bis and aerodynamically very clean for an aircraft of its type, was identical to the M.41bis in most ways, being a wooden, single-seat, single-bay biplane armed with two fixed, forward-firing 7.7 mm (0.303 in) machine guns, plywood and fabric skinning, unstaggered wings of equal span, a 313 kW (420 hp) Fiat A.20 engine driving a pusher propeller mounted on struts above the hull and below the upper wing, and fitted with a vertical radiator.

The M.71 differed from the M.41bis in having a stronger wing cellule and catapult pick-up points and, to facilitate rapid assembly and disassambly during shipboard operations, it had inclined steel tube struts between the hull, interplane struts, and upper wing section instead of the M.41bis's bracing wires.^[1]

Operational history

The Regia Marina accepted the M.71 for service, and Macchi built a small number of them, probably no more than twelve. They briefly saw service aboard Regia Marina warships during the 1930s until the IMAM Ro.43 reconnaissance floatplane and IMAM Ro.44 floatplane fighter replaced them.^[2]

Operators

Kingdom of Italy

Regia Marina

Specifications

Data from Italian Civil & Military Aircraft 1930-1945^[3] and The Complete Book of Fighters^[4]

General characteristics

Crew: 1
Length: 8.66 m (28 ft 5 in)
Wingspan: 11.12 m (36 ft 6 in)
Height: 3.12 m (10 ft 3 in)
Wing area: 31.901 m² (343.38 sq ft)
Empty weight: 1,260 kg (2,778 lb)
Gross weight: 1,690 kg (3,726 lb)
Powerplant: 1 × Fiat A.20 V-12 liquid-cooled piston engine, 313 kW (420 hp)

Performance

Maximum speed: 256 km/h (159 mph, 138 kn)
Stall speed: 80 km/h (50 mph, 43 kn)
Range: 700 km (435 mi, 378 nmi)
Service ceiling: 6,000 m (19,680 ft)
Rate of climb: 5.9 m/s (1,160 ft/min)
Time to altitude:
5 min 39s to 2,000 m (6,562 ft)
9 min 34s to 3,000 m (9,843 ft)
14 min 8s to 4,000 m (13,123 ft)
20 min 25s to 5,000 m (16,404 ft)

Armament

Guns: 2 × fixed forward-firing 7.7 mm (0.303 in) machine guns

Notes

^ Green and Swanborough, pp. 358.
^ Green and Swanborough, p. 358.
^ Thompson, Jonathan (1963). Italian Civil & Military Aircraft 1930-1945 (1st ed.). New York: Aero Publishers Inc. pp. 178. ISBN 0-8168-6500-0.
^ Green, William; Gordon Swanborough (1994). The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Aircraft Built and Flown. SMITHMARK Publishers. ISBN 0-8317-3939-8.

References

Green, William, and Gordon Swanborough. The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Aircraft Built and Flown. New York: SMITHMARK Publishers, 1994. ISBN 0-8317-3939-8.

[1] Green and Swanborough, pp. 358.

[2] Green and Swanborough, p. 358.

[Thompson-3] Thompson, Jonathan (1963). Italian Civil & Military Aircraft 1930-1945 (1st ed.). New York: Aero Publishers Inc. pp. 178. ISBN 0-8168-6500-0.

[Green-4] Green, William; Gordon Swanborough (1994). The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Aircraft Built and Flown. SMITHMARK Publishers. ISBN 0-8317-3939-8.

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