For
general reference only.
The following specifications are
for the Cessna 310.
They do not consider the altered
weight-and-balance characteristics
or resulting restrictions on inflight
performance with installed camera
mounting systems.
|
|
|
13'
11"
(9.7 m)
|
|
|
36'
11"
(11.2 m)
|
|
|
10'
8"
(3.3 m)
|
|
|
3,347 lbs
(1,518 kg) |
|
|
5,500 lbs
(2,495 kg) |
|
|
238
mph
(383 km/h)
|
|
|
1,440
mi (2,668 km)
|
|
|
2
Continental IO-520-M
piston engines
|
Thrust: |
570 hp (424 kW) |
|
|
|
 |
- Aircraft is currently configured for only
one type of system.
- May be only limited to three personnel
onboard during a mission.
|
|
