CAMS 46

__NOTOC__ Infobox Aircraft
name=46


caption=
type=Flying boat trainer
manufacturer=CAMS
designer=
first flight=1926
introduced=
retired=
status=
primary user=French Navy
more users=
produced=
number built=
variants with their own articles=

The CAMS 46 was a flying boat trainer aircraft built in France in the mid 1920s, essentially an updated version of the CAMS 30 that had flown in 1922. While retaining that aircraft's basic form, CAMS offered the French Navy two new versions with aerodynamic refinements over the earlier aircraft: the 46E primary trainer, and the 46ET intermediate trainer. Only the latter was selected for production and was built in quantity to supply one escadrille at the Naval training station at Hourtin.

Operators

;FRA
*French Navy

pecifications (46ET)

aerospecs
met or eng?= met

crew=Two, pilot and instructor
capacity=
length m=9.07
length ft=29
length in=9
span m=12.00
span ft=39
span in=5
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=2.97
height ft=9
height in=9
wing area sqm=37.0
wing area sqft=398
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=978
empty weight lb=2,156
gross weight kg=1,350
gross weight lb=2,976
lift kg=
lift lb=

eng1 number=1
eng1 type=Hispano-Suiza 8Ab
eng1 kw= 134
eng1 hp= 180
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
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max speed kmh=185
max speed mph=115
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1,200
range miles=748
endurance h=
endurance min=
ceiling m=3,500
ceiling ft=11,480
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
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References

*
*

ee also

aircontent

related=

similar aircraft=

sequence=
* ← 36 - 37 - 38 - 46 - 50 - 51 - 52 →

lists=

see also=