|
SPECIFICATIONS
|
|
CA-65B |
|
CA-65 and CA65W |
|
With 100 HP Rotax 912S Engine |
|
With 125 HP Lycoming - Sesenich 66-68 Propeller |
|
Maximum
level speed |
150 |
mph |
. |
Maximum
Level Speed |
180 |
mph |
|
Normal
cruising speed |
130 |
mph |
. |
Normal
cruising speed |
155 |
mph |
|
Stalling
speed |
50 |
mph |
. |
Stalling
speed |
55 |
mph |
|
Rate of
climb |
600 |
fpm |
. |
Rate of
climb |
1000 |
fpm |
|
Take off
run |
640 |
ft. |
. |
Take off
run |
450 |
ft. |
|
Service
ceiling |
12,000 |
ft. |
. |
Landing
run |
600 |
ft. |
|
Span |
25 |
ft. |
. |
Service
ceiling |
15,000 |
ft. |
|
Length |
20 |
ft. |
. |
Span |
25 |
ft. |
|
Height
(in flight position) |
7 |
ft. 4 in. |
. |
Length |
19 |
ft. |
|
Wheel
tread |
6 |
ft. 11 in. |
. |
Height
(in flight position) |
7 |
ft. 4 in. |
|
Wing
area |
108 |
sq.ft. |
. |
Wheel
tread |
6 |
ft. 11 in. |
|
Wing
loading (maximum) |
11.1 |
lbs./sq.ft. |
. |
Wing
area |
108 |
sq.ft. |
|
Empty
weight |
681 |
lbs. |
. |
Wing
loading (maximum) |
13.9 |
lbs./sq.ft. |
|
Gross
weight |
1,200 |
lbs. |
. |
Empty
weight |
900 |
lbs. |
|
Fuel
capacity |
16.3 |
gals. |
. |
Gross
weight |
1,500 |
lbs. |
|
. |
. |
. |
. |
Fuel
capacity |
28 |
gals. |
|
|
