Cessna 414A Stock Airplane vs. RAM Series IV
Primary Specifications Cessna 414A RAM 325 hp Series IV
Engine Model: Continental TSIO-520-NB 310 hp 325 hp
TBO - hours 1,600 1,600
Fuel Capacity - useable - gallons 206 206
Takeoff Manifold Pressure @ 2700 rpm 38” 41”
Twin Engine Climb - ISA @ 7,105 lbs. NA 1486
Twin Engine Climb - ISA @ 6,750 lbs. 1500 1580
Single Engine Climb - ISA @ 7,105 lbs. NA 257
Single Engine Climb - ISA @ 6,750 lbs. 270 316
Cruise Climb Power - ISA + 30°F - RPM & MP 2450 & 31.5” 2500 & 35.0”
Cruise Climb - SL to 18,000 ft - minutes 24 19
Cruise @ 75% - ISA - 20,000 ft. - ktas 208 215
Cruise @ 65% - ISA - 20,000 ft. - ktas 192 203
Cruise @ 55% - ISA - 20,000 ft. - ktas 176 190
Useful Load Increase - lbs. NA +355
Ramp Weight - lbs. 6,785 7,140
Gross Weight - lbs. 6,750 7,105
Landing Weight - lbs. 6,750 6,750
Zero Fuel Weight - lbs. 6,515 6,515
With Winglets
Ramp Weight - lbs. 6,785 7,087
Gross Weight - lbs. 6,750 7,087
Zero Fuel Weight - lbs. 6,515 6,515
Wingspan, or Winglets Tip Top Span 44’-1.5” 45’- 4.8”
SOURCE: Sources
Cessna 414A Stock Airplane vs. RAM Series VII
Primary Specifications Cessna 414A RAM 414 VII
Engine Model: Continental TSIO-520 TSIO-520-N & -NB TSIO-520-NB
Horsepower & TBO hrs. 310 & 1400 / 1600 335 & 1600
Takeoff M.P. @ 2700 rpm (ISA + 30° F) 38” 38”
Twin engine climb @ S.L. (fpm) @ 7105 lbs. NA 1486
Twin engine climb @ S.L. (fpm) @ 6750 lbs. 1500 1580
Single engine climb @ S.L. (fpm) @ 7105 lbs. NA 257
Single engine climb @ S.L. (fpm) @ 6750 lbs. 270 316
Cruise climb power (rpm @ MP) (ISA + 30° F) 2450 @ 31.5” 2500 @ 33.0”
Cruise climb S.L. to 18,000 ft. (minutes) 24 18
75% / 65% / 55% Cruise @ 25,000 ft. (ktas) 214 / 202 / 190 230 / 220 / 210
Gross weight & Useful load increase (lbs.) NA +355 & +320
Gross weight & Ramp weight (lbs.) 6750 & 6785 7105 & 7140
Landing weight & Zero fuel weight (lbs.) 6750 & 6515 6750 & 6515
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.

414A-line-art-front-view copy.jpg
414A-line-art-side-view copy.jpg
414A-line-art-top-view copy.jpg