- 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=
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primary user=Aeronautica Militare
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produced=
number built=
variants with their own articles=The Fiat G.49 was an Italian two-seat basictrainer aircraft designed byGiuseppe Gabrielli and built byFiat .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-wingcantilever 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 anAlvis 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=TheIllustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1798met 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=
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rot dia m=
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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=
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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=
eng1 lbf=
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eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
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eng2 lbf-ab=max speed kmh=370
max speed mph=230
max speed mach=
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cruise speed mph=
range km=1900
range miles=1181
endurance h=
endurance min=
ceiling m=6800
ceiling ft=22,310
glide ratio=
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lists=References
* The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1798
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