| |
|
|
|
|
Alpha
160A (R 2160) |
|
| |
|
|
|
|
Alpha
160Ai (R 2160i) |
|
| |
|
|
|
|
|
|
|
|
Certification
category |
|
|
"A"
Acrobatic |
|
|
|
Engine,
Lycoming |
|
|
IO-320
(AEIO-320), 160 hp |
|
|
|
Propeller,
Sensenich |
|
|
fixed
pitch |
|
|
|
Gross
weight |
|
|
1224
lb |
|
|
|
Useful
load |
|
|
1984
lb |
|
|
|
Wing
span |
|
|
28
ft 7 in |
|
|
|
Fuel
capacity, standard |
|
|
31.7
US Gal |
|
| |
|
Fuel
capacity, optional |
|
|
42.2
US Gal |
|
|
|
Max.cruise,
at 75% power, best altitude |
|
|
131
kt |
|
| |
|
Max.
range, at 65% power, best altitude: |
|
|
|
|
| |
|
-with
standard tank |
|
|
430
Nm |
|
| |
|
-with.optional
160 l tank |
|
|
558
Nm |
|
|
|
Take-off
distance, over 50 ft obstacle |
|
|
1883
ft |
|
|
|
Landing
distance, over 50 ft obstacle |
|
|
1444
ft |
|
|
