Cessna T310 Performance
Primary Specifications Cessna T310 RAM T310 300 hp Series I RAM T310 325 hp Series IV
Engine Model: Continental - TSIO-520 -B & -BB -E & -EB -NB
Horsepower: 285 300 325
TBO - hours 1,400 1,400 1,600
RAM STC’s allow for the installation of numerous propellers, all of which perform well.
Prop lines are removed. See Price sheets.
Fuel - T310 w/63 gal. Aux. useable - gallons 163 163 163
Takeoff Manifold Pressure @ 2700 rpm 32” 34.5” 41”
Takeoff Runway Acceleration 0 to 100 mph 25 sec. 20 sec. 15 sec.
Twin Engine Climb - ISA 1700 fpm 1900 fpm 2500 fpm
Single Engine Climb - ISA 400 fpm 490 fpm 640 fpm
Climb Power - ISA + 30°F - RPM & MP 2350 & 29.0” 2500 & 32.0” 2500 & 35.0”
Cruise Climb - SL to 18,000 ft - min. 25 19 12
Cruise @ 75% - ISA - 23,000 ft. - ktas 209 217
Cruise @ 75% - ISA - 12,000 ft. - ktas 200 209 217
Useful Load Increase - lbs. - T310P NA +270 +270
Useful Load Increase - lbs. - T310Q NA +170 +170
Useful Load Increase - lbs. - T310R NA NA NA
T310P Ramp Weight - lbs. NA 5,700 5,700
T310P Gross Weight - lbs. 5,400 5,670 5,670
T310Q Ramp Weight - lbs. NA 5,700 5,700
T310Q Gross Weight - lbs. 5,500 5,670 5,670
T310R Ramp Weight - lbs. 5,535 5,535 5,535
T310R Gross Weight - lbs. 5,500 5,500 5,500
SOURCE: Sources

Performance is based on a mid CG with mid cabin and fuel weight on an average day. Performance should always be calculated per flight environment while referring to the Manufacturer’s Pilots Operating Handbook and applicable Flight Manual Supplements for the particular airplane. Aircraft Manufacturer’s Pilot Operating Handbooks and Aircraft Owner’s Manuals should always be available and adhered to by the aircraft Pilot in Command, including attention to applicable FAA approved Flight Manual Supplements and emergency procedures for each individual aircraft. Performance should vary from airplane to airplane, atmospheric day to atmospheric day, one gross weight and CG to another, and pilot to pilot.

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