
AVA-202
...what it takes to touch
heavens.
Pilot training , parcel carrying
, surveillance and recreational activities are the basic ideas
for
AVA-202
, a light two-seat airplane.
It meets certification
requirements of
JAR-VLA
in normal category, featuring all-metal
airframe of aluminum alloy with single spar wing and
glassfibre engine cowlings. State-of-the-art forward sliding
canopy of Plexiglas provides maximum rearward view.
The planned engine
is Textron Lycoming O-320-B2B (160hp) , driving a Sensenich two-blade fixed-pitch metal propeller. Engine jet
pipe deflected to carry exhaust clear of body. There are two
integral fuel tanks in wings with a total capacity of 120
liters. Other features are:
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Heated and ventilated cabin |
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Easy Access
baggage compartment |
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Dual flight control system and metal instrument panel. |
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Single-slotted electrical flaps. |
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Accommodation: Two seat side by side |
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Systems: 12V electrical system |
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Avionics: Bendix/King KX 125 VHF nav/com radio with
ELT plus |
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Instrumentation: ADF and GPS at customer' request |
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Landing gear: Fixed with
cantilever spring nose wheel and hydraulically actuated
disk brakes, castor nose wheel with shimmy damper and
streamline composite fairing over all three wheels. |
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Specification and performance characteristics
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Wing span |
8.74 m |
|
wing chord |
1.24 m |
|
Length overall |
6.02 m |
|
Height overall |
2.04 m |
|
Propeller diameter |
1.88 m |
|
Empty weight |
500 kg |
|
Max T-O and landing weight |
750 kg |
|
Max level speed at S/L |
140 Kts |
|
Max cruising speed (flaps down) |
138 Kts |
|
stalling speed (flaps down) |
45 Kts |
|
Service ceiling |
21000 fts (6400 m) |
|
T-O run |
250 m |
|
Range with maximum fuel |
1000 km |