Cessna 414
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RAM - Series VII
335 horsepower |
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| A Cessna 414 can transport you and your people, from your airport, on your schedule. It’s truly a reliable airplane.
Featuring a 4.2 differential pressurized cabin, enjoy a sea level cabin to 9,000 ft., and hold a 10,000 ft. cabin at 23,000 ft. A Cessna 414 can be updated with the latest high tech avionics and instrumentation.
An airstair door makes it easy to step inside the Cessna wide oval cabin where you can handle business with your associates and customers in comfortable club seating.
Single pilot or owner flown, bring along three to four passengers and still have the fuel needed for a long trip.
A RAM Series VII Cessna 414 can cruise climb to FL230 in 25 minutes. At FL230, a 260 horsepower cruise setting will deliver 223 ktas/256 mph on 20.3 gallons a side.
RAM overhauls dozens of TCM TSIO-520-NB engines to support the Cessna 414 fleet. In the process we upgrade their engine horsepower and install new propellers. Critical engine and installation accessories are replaced with new and quality overhauled parts, beginning with RAM’s Nickel New Cylinder Package.
Behind each of our engine overhauls and performance upgrades stands the Industry respected trust and integrity of RAM’s TBO Warranty Support Program. |
Engine Model: TCM TSIO-520-NB |
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Horsepower: RAM STC from 310 hp to 335 hp |
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Time Between Overhauls - TBO |
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Fuel Capacity with use of Auxiliary Tanks |
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Takeoff - Manifold Pressure @ 2700 rpm |
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Runway Acceleration: 0 to 100 mph |
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Single Engine Climb:
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Cruise Climb Power:
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Cruise Climb: Sea Level to 23,000 ft.
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Cruise Speed @ 260 hp @ 23,000 ft.
Fuel consumption per engine/per hour: |
223 ktas / 256 mph
20.3 gallons
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Cruise Speed @ 230 hp @ 23,000 ft.
Fuel consumption per engine/per hour: |
212 ktas / 243 mph
17.9 gallons
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CruiseSpeed @ 200 hp @ 23,000 ft.
Fuel consumption per engine/per hour: |
190 ktas / 218 mph
14.7 gallons
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Useful Load Increased by an additional: |
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Ramp Weight: |
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Gross Weight: |
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Landing Weight
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Zero fuel weight (lbs.) |
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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. |