Evangel 4500

Evangel 4500

__NOTOC__ Infobox Aircraft
name=Evangel 4500


caption=
type=Light passenger/cargo
manufacturer=Evangel Aircraft Corporation
designer=
first flight=1964
introduced=1969
retired=
status=
primary user=
more users=
produced=
number built=8
variants with their own articles=

The Evangel 4500 was a 1960s American twin-engined light passenger/cargo monoplane built by the Evangel Aircraft Corporation.

Development

The Evangel Aircraft Corporation was established to design and build a bush aircraft particularly for use by missionary groups. For work in South America it had to have STOL capability and be simple to operate and maintain. The aircraft that was designed was designated the Evangel 4500-300 and was a twin-engined monoplane with a tailwheel configuration retractable landing gear. The prototype first flew in June 1964 and the first production aircraft in January 1969. The aircraft needs a very short take-off run and can achieve a take-off to 50ft (15m) within 375yds (343m).

Variants

;4500-300:Production variant;4500-300-II:Used to identify aircraft fitted with turbochargers.

pecifications

aerospecs
ref=
met or eng?= eng

crew=
capacity=
length m=9.6
length ft=31
length in=6
span m=12.57
span ft=31
span in=3
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=2.90
height ft=9
height in=6
wing area sqm=23.32
wing area sqft=251
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=1601
empty weight lb=3530
gross weight kg=2495
gross weight lb=5500
lift kg=
lift lb=

eng1 number=2
eng1 type=Avco Lycoming IO-540-K1B5 flat-six piston engine
eng1 kw= 224
eng1 hp= 300
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=
eng2 lbf-ab=

max speed kmh=370
max speed mph=230
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1127
range miles=300
endurance h=
endurance min=
ceiling m=6410
ceiling ft=21,030
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=

References

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

ee also

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