- Farman F.300
__NOTOC__ Infobox Aircraft
name=F.300 and F.310
caption=
type=Airliner
manufacturer=Farman Aviation Works
designer=
first flight=13 January avyear|1930
introduced=
retired=
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variants with their own articles=The Farman F.300 and F.310 were airliners built in France in the early 1930s. Built to the same general trimotor layout popular with manufacturers of the time, they were high-wing strut braced monoplanes with fixed tailskid undercarriage. The cockpit and passenger compartment were fully enclosed. Most went to equip Farman's own airline, whose twelve F.300 variants made up half its fleet in 1931.One variant, the F.302, was specially built as a single-engine machine to make an attempt at a number of world records. On 9 March 1931,
Jean Réginensi andMarcel Lalouette set new distance and duration records over a closed circuit with a 2,000 kg payload, flying 2,678 km (1,674 miles) in 17 hours. Another, the F.304 was built as a special trimotor forMarcel Goulette to make a long-distance flight the same month fromParis toTananarive and back.The F.310 was a seaplane version of the same basic design. The prototype was destroyed while landing during trials, and no further examples were built.
Variants
F.300
* F.300 - prototype with
Gnome et Rhône 5B a engines (1 built)
* F.301 - production version withSalmson 9A b engines (6 built)
* F.302 - version powered with singleHispano-Suiza 12N b for record attempt (1 built, later re-engined withHispano-Suiza 12L br
* F.303 - production version with Gnome et Rhône 5Ba engines (6 built)
* F.304 - long-range version withLorraine 9N engines (1 built)
* F.305 - production version withGnome et Rhône 9A engines (2 built)
* F.306 - production version withLorraine 7M e engines (4 built)F.310
* F.310 - seaplane version with Salmson 9Ab engines (1 built)
Operators
;FRA
*Air Orient operated four aircraft.
*Farman Line operated 12 aircraft.;flag|Yugoslavia|kingdom:
*Aeroput operated 1 F.306 aircraft.pecifications (F.301)
aerospecs
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met or eng?= metcrew=Two pilots
capacity=8 passengers
length m=13.35
length ft=43
length in=10
span m=19.12
span ft=62
span in=9
swept m=
swept ft=
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rot dia ft=
rot dia in=
dia m=
dia ft=
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width m=
width ft=
width in=
height m=3.3
height ft=10
height in=10
wing area sqm=71.0
wing area sqft=764
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=2,610
empty weight lb=5,754
gross weight kg=4,350
gross weight lb=9,590
lift kg=
lift lb=eng1 number=3
eng1 type=Salmson 9A b
eng1 kw= 170
eng1 hp= 230
eng1 kn=
eng1 lbf=
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eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
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eng2 lbf-ab=max speed kmh=230
max speed mph=140
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=975
range miles=600
endurance h=
endurance min=
ceiling m=4,500
ceiling ft=14,800
glide ratio=
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sink rate ftmin=armament1=
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armament6=aircontent
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lists=References
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* [http://www.aviafrance.com/constructeur.php?ID_CONSTRUCTEUR=501 aviafrance.com]
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