Primary Specifications |
|
|
RAM T310
325 hp Series IV
|
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. |
| 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 - 18,000 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 Gross Weight - lbs. |
5,400 |
5,670 |
5,670 |
| T310Q Gross Weight - lbs. |
5,500 |
5,670 |
5,670 |
| T310R Gross Weight - lbs. |
5,500 |
5,500 |
5,500 |
| Performance should vary from airplane to airplane, atmospheric day to atmospheric day, one gross weight and CG to another, and pilot to pilot. |
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. |
