Agusta AZ8-L

__NOTOC__ Infobox Aircraft
name=AZ8-L


caption=
type=Airliner
manufacturer=Agusta
designer=Filippo Zappata
first flight=9 June 1958
introduced=
retired=
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produced=
number built=1
variants with their own articles=The Agusta AZ8-L was an Italian airliner prototype first flown on 9 June 1958. It was of conventional low-wing monoplane configuration with tricycle undercarriage and all-metal construction. Filippo Zappata's design grew out of a twin-engined transport designated AZ1 that was never built.

When the AZ8-L failed to attract customers, Agusta abandoned the project to focus on its helicopter manufacturing operations, in particular a new Zappata design, the A.101.

pecifications

aerospecs
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crew=two pilots
capacity=26 passengers
length m=19.44
length ft=63
length in=9
span m=25.50
span ft=83
span in=8
dia m=
dia ft=
dia in=
height m=6.66
height ft=21
height in=10
wing area sqm=66.8
wing area sqft=720
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=7,100
empty weight lb=15,700
gross weight kg=11,300
gross weight lb=25,000

eng1 number=4
eng1 type=Alvis Leonides 503/2 9-cylinder radials
eng1 kw= 350
eng1 hp= 470
eng1 kn=
eng1 lbf=
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max speed kmh=427
max speed mph=266
range km=2,500
range miles=
endurance h=
ceiling m=7,500
ceiling ft=1,560
glide ratio=
climb rate ms=5
climb rate ftmin=1,000
sink rate ms=
sink rate ftmin=

armament1=
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ee also

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similar aircraft=
* Handley Page Herald

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References

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