HAL Pushpak

__NOTOC__ Infobox Aircraft
name=HUL-26 Pushpak


caption=
type=Two-seat cabin monoplane
manufacturer=Hindustan Aeronautics Limited
designer=
first flight=1958
introduced=
retired=
status=
primary user=
more users=
produced=
number built=160+
variants with their own articles=The Hindustan HUL-26 Pushpak was a 1950s Indian two-seat cabin monoplane designed and built by Hindustan Aeronautics Limited. The Pushpak was a high-wing braced monoplane with a fixed tailwheel landing gear. The Pushpak first flew on the 28 September 1958 and was powered by a 90hp (67kW) Continental flat-four engine. Around 160 aircraft were produced for Indian flying clubs for use as basic trainers.

pecifications (HUL-26)

aerospecs
ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 2172
met or eng?= eng

crew=2
capacity=
length m=6.40
length ft=21
length in=0
span m=10.97
span ft=36
span in=0
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=2.77
height ft=9
height in=1
wing area sqm=16.26
wing area sqft=175
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=395
empty weight lb=870
gross weight kg=612
gross weight lb=1350
lift kg=
lift lb=

eng1 number=1
eng1 type=Continental C90-8F flat-four piston engine
eng1 kw= 67
eng1 hp= 90
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
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eng2 kw=
eng2 hp=
eng2 kn=
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max speed kmh=145
max speed mph=90
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
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aircontent
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References

* The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 2172