Fiat G.49

Fiat G.49

__NOTOC__ Infobox Aircraft
name=Fiat G.49


caption=
type=Two-seat basic trainer
manufacturer=Fiat
designer=Giuseppe Gabrielli
first flight=1952
introduced=
retired=
status=
primary user=Aeronautica Militare
more users=
produced=
number built=
variants with their own articles=
The Fiat G.49 was an Italian two-seat basic trainer aircraft designed by Giuseppe Gabrielli and built by Fiat.

Development

The G.49 was designed as a replacement for the World War II-era US North American T-6 advanced trainer by Gabrielli and was first flown in September 1952. The G.49 was an all-metal low-wing cantilever monoplane with retracting tailwheel landing gear. It had an enclosed cockpit with raised canopy for a pupil and instructor in tandem. Two variants were built with different engine installations; the G.49-1 with an Alvis Leonides radial engine and the G.49-2 with a Pratt & Whitney radial engine.

Operational history

The aircraft did not sell and only a small number were operated by the Italian Air Force.

Variants

;G.49-1:Variant powered by a 570hp (425kW) Alvis Leonides 502/4 Mk 24 radial engine.;G.49-2:Variant powered by a 610hp (455kW) Pratt & Whitney R-1340 radial engine.

Operators

;ITA
*"Aeronautica Militare"

pecifications (G.49-2)

aerospecs
ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1798

met or eng?= met

crew=2 (pupil, instructor)
capacity=
length m=9.50
length ft=31
length in=2
span m=13
span ft=42
span in=7¾
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=2.65
height ft=8
height in=8¼
wing area sqm=
wing area sqft=
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=2240
empty weight lb=4983
gross weight kg=2860
gross weight lb=6305
lift kg=
lift lb=

eng1 number=1
eng1 type=Pratt & Whitney R-1340-S3H1 Wasp 9-cylinder radial piston engine
eng1 kw= 455
eng1 hp= 610
eng1 kn=
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eng2 number=
eng2 type=
eng2 kw=
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max speed kmh=370
max speed mph=230
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1900
range miles=1181
endurance h=
endurance min=
ceiling m=6800
ceiling ft=22,310
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
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armament1=
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aircontent
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References

* The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1798


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