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RAM - Series IV
325 horsepower |
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| A Cessna 414A can transport you and your people, from your airport, on your schedule. It’s truly a reliable airplane.
Featuring a 5.0 differential pressurized cabin, enjoy a sea level cabin to 10,000 ft., and hold a 6,000 ft. cabin at 20,000 ft. A Cessna 414A 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 four to five passengers and still have the fuel needed for a long business trip.
A Series IV can cruise climb to FL180 in 19 min. Maxumum cruise is at 20,000 ft. where 75% power cruise setting will deliver 215 ktas/247 mph on 20 gallons a side.
RAM overhauls dozens of TCM TSIO-520-NB engines to support the Cessna 414A 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 325 hp |
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Time Between Overhauls - TBO |
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Fuel Capacity: |
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Takeoff - Manifold Pressure @ 2700 rpm |
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Single Engine Climb: |
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Cruise Climb Power: |
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Cruise Climb: Sea Level to 18,000 ft. |
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Cruise Speed: @ 75% Power @ 20,000 ft. |
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Cruise Speed: @ 65% Power @ 20,000 ft. |
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Cruise Speed: @ 55% Power @ 20,000 ft. |
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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: |
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RAM Winglets: Winglets may be installed separately on any Cessna 414A, regardless of engine horsepower or RAM upgrades.
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Ramp Weight: |
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Gross Weight: |
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Zero Fuel Weight: |
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( Standard Cessna Wingspan is 44.12' )
(With Winglets Installed, the Hangar Clearance
top of tip to top of tip of the winglet's full span is: |
45 - 4.8
Winglet Span - top - tip to tip
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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. |
Cessna 414A - Dimensions:



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