Alaparma Baldo

Infobox Aircraft
name=Baldo


caption=
type=Civil utility aircraft
manufacturer=Alaparma
designer=Adriano Mantelli
first flight=
introduced=
retired=
status=
primary user=
more users=
produced=1949-51
number built=~35
variants with their own articles=The Alaparma Baldo was an unusual two-seat light monoplane produced in Italy shortly after World War II. Designed by Adriano Mantelli, it featured an egg-shaped fuselage with cabin doors that hinged upwards and to the back. The conventional tailplane with single fin and rudder was carried on twin booms, either side of a pusher engine installation. The undercarriage consisted of a single mainwheel under the fuselage pod, a small tailwheel not far behind it, and outrigger wheels on the wingtips.

Variants

* AP.65 with Walter Mikron piston engine
* AP.75 with Praga D engine

pecifications (AP.75)

aerospecs
met or eng?= met
crew=one pilot
capacity=1 passenger
length m=5.1
length ft=16
length in=8
span m=7.0
span ft=23
span in=0
height m=1.5
height ft=4
height in=9
wing area sqm=
wing area sqft=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=490
gross weight lb=1,080
eng1 number=1
eng1 type=Praga D
eng1 kw= 56
eng1 hp= 75
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
max speed kmh=220
max speed mph=140
range km=660
range miles=410
endurance h=
ceiling m=4,800
ceiling ft=15,700
glide ratio=
climb rate ms=
climb rate ftmin=

References

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* [http://www.luftfahrt-archiv.de/Flugzeugtypen.asp?Type=Link&ID=T1354&SID=384204425 luftfahrt-archiv.de]

ee also

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