AS-5.0
Scientific-production association «AeroVolga» has prepared the promising project of budget aircraft for agricultural operation and also for pilots training and cargo transportation, general aviation.
The aircraft belongs to JAR-VLA category. The aircraft prototype had state license for crop dusting.
Chief designer –Dmitriy Suslakov
Two prototype models have total flying time of more than 1500 hours and have proven themselves perfect during the crop dusting.
The aircraft has high maneuverability and it is safe at low speeds.
The price of the basic version of the aircraft: EXW – AeroVolga, Krasniy Yar aerodrome, Samarskaya oblast.
Version Agro – USD 115 000
Version Trainer – USD 85 000 (VFR)
Version Cargo – USD 120 000 (VFR+GPS)
Version General Aviation – USD 80 000 (VFR)
Version Hydro – USD 100 000 (VFR) (floats)
The price is valid on December, 1st, 2013
Aircraft performance characteristics of AS – 5.0
(for maximum take-off weight in standard conditions)
|
Modification
|
АS 50Т
|
АS 50А
|
АS 50Н
|
АS 50 C
|
|
Designation
|
Trainer aircraft
|
Agricultural aircraft
|
Hydroplane
|
General aviation/Cargo aircraft
|
|
|
|
|
|
|
|
Take-off weight, kg
|
600
|
750
|
660
|
715/750
|
|
Empty weight, kg
|
330
|
365
|
390
|
335/350
|
|
Fuel capacity, kg
|
50
|
50
|
75/100
|
100
|
|
Useful load, kg
|
270
|
385
|
270
|
380/400
|
|
Commercial load
|
220
|
-
|
195/170
|
280/300
|
|
Chemicals capacity, kg
|
-
|
335
|
-
|
-
|
|
|
|
|
|
|
|
Wingspan, m
|
10,2
|
10,2
|
10,2
|
10,6
|
|
Wing area, m2
|
14,3
|
14,3
|
14,3
|
14,4
|
|
Length, m
|
6,57
|
6,57
|
6,67
|
6,67
|
|
|
|
|
|
|
|
Stall speed Vso, km/h
|
65
|
72
|
70
|
68
|
|
Cruise speed, km/h
|
220
|
155
|
160
|
220
|
|
Maximum speed Vne
|
270
|
200
|
200
|
270
|
|
|
|
|
|
|
|
Rate of climb m/s
|
4,2
|
2,5
|
3,5
|
3,5
|
|
|
|
|
|
|
|
Take-off run, m
|
90
|
140
|
200
|
140
|
|
Roll length, m
|
90
|
70*
|
90
|
70
|
|
Take-off distance, m
|
190
|
400
|
300
|
400
|
|
Landing distance, m
|
190
|
150*
|
200
|
150
|
|
|
|
|
|
|
|
G-units
|
-2/+4
|
-1,9/+3,8
|
-1,9/+3,8
|
-2/+4
|
|
|
|
|
|
|
|
Max. range, km
|
800
|
500
|
650
|
1200
|
|
Engine project
|
LOM-332
|
ROTAX-912
|
LOM-332
|
LOM-332
|
|
Max. engine power, hp
|
140
|
100
|
140
|
140
|
Note
*- landing characteristics with empty chemicals tank and maximum fueling
|
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