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Performance &
Specifications - 1964 Cessna 310 I |
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Radios:
KX-155A NAV/COMM
KY 196
COMM
KN-53 NAV
KMA-24 Audio Panel
KN-64 DME
KLN-94 Panel Mount IFR GPS
KX-76A Transponder
Collins - 650 ADF
Lightning Strikefinder
HSI as # 1 NAV
Dual Instrumentation includes:
Airspeed Indicator
Altimeter
Turn and Slip Indicator
Attitude Indicator
Heading Indicator |
| Speed @ 75% power and
9000 ft |
170 MPH indicated, 220MPH TAS |
| Horsepower @
2625 RPM |
260HP
per engine |
| Engines |
Two Continental, IO-470U |
| Fuel Capacity
(Usable) |
130 US. GAL. |
| Range
- no reserve |
1,130 SM |
| Endurance @
65%
power @
10,000ft. |
5.3 Hours |
| Fuel Burn @ 75%
power |
25 GPH |
| Useful Load |
3,354.3 lbs |
| Payload (with
full fuel) |
966
lbs |
| Empty Weight |
1,719 / 1,746 lbs
(determined by seat config.) |
| Maximum
Take-Off Weight |
5,100 lbs |
| Single Engine
Service
Ceiling |
7,500 FT |
| Service
Ceiling |
20,300 FT |
| Seating |
6 |
| Key
Airspeeds: |
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| Vy |
121 KIAS |
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Vx |
105 KIAS |
|
Best Glide |
110 KIAS (both engines inop) |
| Va @
5,100 lbs |
170 KIAS |
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