Aerodynamic mods include vortex generators to increase aileron and rudder control authority at low speeds. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. Finally, the Riley Rocket 414 has two 400hp Lycoming IO-720 engines fitted. List price was $138,000 (thats over $740,000 in 2007 dollars)-$35,000 less than the Duke and some $50,000 less than both the 421 and Pipers P-Navajo.Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. Engines two 340-hp turbocharged Continentals. The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. 6,200: 6,430: Zero Fuel Weight - lbs. It is the first turboprop-engine aircraft designed and manufactured by Cessna in the 1970s. I use SimCom. 6,500. Mandatory power reductions during the climb above FL220 meant long climb times and getting above FL250 seemed to take forever at the 200 FPM climb rate that could be achieved up there. The length of the cabin was increased by 16 inches (40.64 cm), an extra window was installed, electronic propeller synchrophasing was made standard, and various ARC 400-series avionics equipment was included. ) The difference is that an -N engine uses 38 inches of manifold pressure, rather than 36 inches, and 2700 RPM to produce its rated 310 horsepower. [1], In 1974, American Jet Industries built a turboprop-powered conversion of the Cessna 414, named the Turbo Star Pressurized 414, using Allison 250-B17B engines. This is when Cessna decided to take advantage of Continental Motor's then-new, 225-horsepower O-470-A engine and develop the robust Cessna 180, which first flew in May 1952. The displacement and power output remained the same, but the manifold pressure was increased from 36 hPa to 38 hPa. Its important to note that a 414 is 7 knots slower than its little brother, the 340, which has the same engines and many of the same systems, but a notably smaller cabin. 5,500. .tdi_115.td-a-rec-img { Production aircraft were accessible in several optional seating configurations and avionics packages. The Cessna 414 was given a clean wing in 1978. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. It is our mission to be the go to leaders in the aviation industry. With the RAM IV, useful load is over 2100 pounds, which enables one to carry full fuel plus 900 pounds. Some low-time pilots might be approved for 340 insurance, but rejected for a 414/414A. Come join us! Flight planning or any other aircraft operations should only be done using official technical information provided Since 2017 he's been working as a content writer and loves that he can combine his love of aviation and writing here at Aviator Insider. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. The maximum takeoff weight went up to 400 pounds to yield a higher useful load. An AD that requires the propeller hubs to be filled with red indicator oil to make cracks more visible was also released. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. Empty wt. As has often been said, Cessna really got it right with the 414/414As. It has a take-off distance of 665 meters and a landing distance of 718 meters. In 1979, the 402s received a new wing, with a 5 feet (1.5 m) greater span. I own a 1978 Cessna 414A which I acquired in 1989. The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. Range 506- 1,325. Fuel capacity 202. There are only two fuel-. m. All data presented is only indicative and should not be used operationally. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. Frequently, a a buyer makes assumptions that arent correct. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. This piston engine is a six-cylinder, horizontally-opposed, direct drive, turbocharge, air-cooled, and fuel-injected type that produces a maximum thrust of 310 horsepower each. Landing Distance: 2393 ft: 729 m: Max Takeoff Weight: 6751 lbs: 3062 kg: Max Landing Weight: 6750 lbs: 3062 kg: Useful Weight: 2417 . Sure, many have been plowed up for houses or 2023 Aviation Publishing Group. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). Of course, any airplanes safety depends a great deal on the proficiency of its pilots. By continuing to use this website, you are agreeing to our Cookie Policy. Cruise mph 277. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. Otherwise, the periodicity is 1,600, or 200 hours depending on the mod state. Another great resource is the Cessna Pilots Association, it offers a monthly magazine, forums, technical information, and even training. Landing distance (50) 1,790. ft/min, IAS With full tanks-enough fuel for nearly 4.5 hours with IFR reserves-a well-equipped Chancellor will have room left in its weight-and-balance envelope to accommodate six FAA-standard people with their toothbrushes. One of the most distressing issues the Cessna 414A has is cracking along the forward wing spars. z-index: -1; Owners of 414As can opt for the series V conversion, which includes Continentals 350-HP liquid cooled Voyager engines, which have a TBO of 2000 hours. For example, the 414 may be powered by a standard 310-HP engine, a 325-HP RAM Series IV or a 335-HP RAM VI or VII. Auxiliary fuel pumps were placed outside the tanks, while the fuel flow gauge together with the fuel quantity gauge and the fuel low-level warning light is in the cockpit. Other modifications in 1978 included a longer nosecone, a redesigned undercarriage system, and an extended wing without the earlier tip tanks. The system left room for error, not only on the part of the pilot, but among line personnel. 100 PERFORMANCE: Top mph 273. With the rise in FAA-PMA approved manufacturers, many have niched down to support a particular aircraft type and finding trim (knots2u, Texas Aeroplastics or AvFab), landing gear components (Robair Repair), or lighting (Whelen Aerospace Technologies or AeroLeds) for your 414 is not hard. It is the flying carpet my wife always wanted, including a potty! Engines two 285-hp turbocharged Continentals. Preferred Airparts, based in Ohio, provide worldwide customers with surplus new Cessna original components and used parts from dismantled aircraft. The exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. Distances Takeoff Distance: 2185 ft Balanced Field Length: 2595 ft Landing Distance: 4000 ft Performance Rate of Climb: 1900 fpm Climb Rate One Engine Inop: 325 fpm Max Speed: 240 kts Normal Cruise: 230 kts Economy Cruise: 210 kts Cost per Hour: $ 522.43 Power Plant Engines: 2 Engine Mfg: Continental Engine Model: TSIOL-550A In 1978, an enhanced version was launched, designated as the 414A Chancellor. Currently, David flies twin retractables, notably the Pa44 Seminole and Pa30 Twin Comanche. 6,165: 6,165: SOURCE: Sources. According to BWI Fly, for liability coverage of $1,000,000, a qualified pilot of a 414A who aims to use the aircraft for private use can expect to pay around $840 $1,400 per year and $4,400 $5,800 per year for a combination of the liability and hull coverage of $225,000. The popularity of the aircraft ensures that there are enough aftermarket parts that can be bought if used parts are unavailable. Im required to attend an approved school for recurrent training. . Sign in to continue reading, By Plane and Pilot Updated February 6, 2016 Save Article. However, there are a number of airworthiness directives (AD) and service bulletins that have been published over the years. No warranty of The pressurized comfort of the 414A, which produces an 8000-foot cabin at 22,800 feet, cannot be overemphasized. EASY ACCESS Two large cabin doors allow for convenient entry and loading for student and instructor. fitness for any purpose is made or implied. Give me one three-hour cross country with any new owner and hell be able to teach the system. Though its Continental engines could maintain their rated power at higher altitudes, Cessna implemented manifold pressure limitations above 20,000 ft (6,096 m) to prevent excessive engine temperatures. Empty wt. In 1973 Cessna stretched the fuselage by 16 inches and added a fifth side window. They can be purchased from Micro Aerodynamics and VG Systems. Four variations are available, all of which offer a boost in useful load, increased TBOs and new props. Takeoff distance (50) 2,220. Cessna Caravan Maximum Range: 1,070 nm Maximum Occupants: 10 - 14 Cessna SkyCourier (Freighter) Maximum Range: 940 nm Payload: 6,000 lb Cessna SkyCourier (Passenger) Maximum Range: 920 nm Maximum Passengers: 19 Single Engine Aircraft Cessna Country: United States Manufactured: 1961 to: 1985 ICAO: C185 Price: US$.32 million (2019) Performance Weights Dimensions Avionics: Engine: 1x Continental IO-520-D Piston Power: 300 horsepower Max Cruise Speed: 145 knots 269 Km/h Approach Speed (Vref): 49 knots Travel range: 720 Nautical Miles 1,333 Kilometers Fuel Economy: Service Ceiling: Maintenance costs vary from year to year, but $300 to $350 direct per hour is a good estimate for the 125 to 150 hours per year I fly. There are only two fuel-288quantity indicators, both with three-position switches, to help the pilot keep track. The top of the line for the 414 is the series VI. Loading must be watched carefully to avoid going out of the rear CG limit. The aircraft can seat up to eight passengers and one or two crew. Cabin specifications: 04'03" cabin high, 04'07" cabin wide, and 11'03" cabin long. 1000 Description Initial climb rate 1,900. 3,865. Bombardier Global 8000 Guide and Specs: Superior Sonic Transportation, Embraer Legacy 450 Guide and Specs: The Stepping Stone, Bombardier Challenger 300 Guide and Specs. Its wings are borrowed from the Model 414. The engines were taken from the 402, with the only changes made to the setup were the inclusion of parts for bleed-air cabin pressurization, and different intercoolers. Developed from the 310, it utilizes a similar landing gear and tail unit. To keep CHTs below red line I had to fly at no more than 55 percent power and with the cowl flaps open at high altitudes. It was developed to bridge the gap between the unpressurized Cessna 401 and the pressurized, more powerful Cessna 421. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). Balloons And Runway Calamities: Why Wait To Panic? Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. Mike Buschs Savvy Owners seminar is valuable. } It has a range of 1,328 nautical miles and a climb rate of 1,520 feet per minute. A typically equipped 414A has a full-fuel payload of about 500 to 700 pounds, depending on equipment. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. The main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. Seating is spacious and available in a variety of arrangements. In addition to the bare-bones model and the ARC 400-equipped 414AII, there was a III version with ARC 800- and 1000-series avionics, a Bendix RDR 160 weather radar and 100-amp alternators.After the Chancellor debuted, there were few further refinements. The aircraft has a remarkably high service ceiling of 30,800 ft (9387 m), but the normal operating range of a 414A is between 15,000 ft (4572 m) and FL250 (7,620 m). Go figure. Based on 450 hours a year and fuel cost at $5.00 per-gallon, the CESSNA 414A has total variable costs of $233,550.00, total fixed costs of $73,885.00, and hypothetical summary cost of $307,435.00. The 414 was meant to attract customers looking to upgrade from their unpressurized twin-engined aircraft and did so with limited success. Trevin is a licensed flight instructor and pilot with degrees in Commercial Aviation and Aviation Management. The first Cessna Chancellor - the 414 - took to the skies in 1968, and was produced from 1970 onwards. According to the president of the Twin Cessna Flyer a society for owners of Cessna Twin aircraft Larry Ball, there are a few more problem areas of the 414A that have not been published but are common enough to talk about. It did away with the extremely complicated and troublesome fuel system of the previous generations and replaced it with wet-wing fuel tanks that were 4.50 ft (1.37 m) longer and held 213 gal (968 l) total. NM, ROD The other category that brings the price up to the same number are the aircraft that have undergone a RAM conversion. MEL, in this case, refers to Multi-Engine Land. Six seats were standard; a seventh was available as an option. Distinguishing features are: retractable landing gear and three-bladed, constant speed, fully feathering propellers. However, some years, unexpected maintenance can eat your lunch. Prices range from low-hour models of 2,750 hours TTAF, selling for just over US$575,000, while older aircraft from the late-1970s are selling for approximately US$230,000. Americas owner-flown aircraft enthusiasts and active-pilot resource, delivered to your inbox! Even with the company is getting its feet wet in piston products again, there are no immediate plans to make any cabin-class piston twins to replace those being retired. LED landing and recognition lights offer enhanced visibility and strong illumination for night flying. Takeoff distance (50) 2,010. In a study of accident records some years ago, the 414 stood out as the safest light twin. Special Missions. For the Cessna 414A Chancellor, average pricing was US$280,000, having approximately 7,500 hours total time airframe (TTAF) and mid-life engines. One pilot and typical 6 passengers in main cabin. The fuel system composed of a pair of main tanks and fuel selectors, emergency cross-feed shutoff valves, and other crucial parts to complete the system. Initial climb rate 1,700. If you are looking for factory parts sites like CessnaParts, AircraftSpruce, and Knots2U have a large catalog of parts available for purchase.Cessna Chancellor (414A) Common Problems. Above this speed, turbulence or rapid control deflections increase the chance of structural damage. This AD has a compliance time of 400 to 800 total time. Quality initial and recurrent training is critical. Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. B. C. (2015, July 13). The engines on the 414II were upgraded to the newer Continental TSIO-520-Ns. If followed carefully, a mechanic wont miss anything. Aviation Consumer. When pilots are flying IFR, it means they are under the control of Air Traffic Control. (2001, February 26). However, only upon acquiring the 414 did I finally attain my goal-virtually complete independence from the airlines for domestic travel. This can be remedied by fitting the aircraft with speed brakes/spoilers or installing a liquid cooling system to the engines. Range 1,284. Those owners who try to operate an aircraft like the Cessna 414 on a shoestring are pursuing false savings. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. (See page 25 for an abbreviated AD list. One of the biggest weak points of the 414A is the problematic Continental TSIO-520-NB engine. Airworthiness Directives; Cessna Aircraft Company models 402C and 414A airplanes. Even with aging aircraft and occasional engine-related issues, the 414A offers a large cabin, the comfort and convenience of pressurization and the performance and safety of turbo charging. The landing gear is the standard electromechanical system that is on all tiptank twin Cessnas. It is powered by two wing-mounted 310hp (231kW) Continental TSIO-520-J horizontally opposed, six-cylinder engines. Like most all twin Cessnas, we give the 414 high marks for cockpit ergos, and the logical layout of systems and controls makes the flight deck a comfortable place to chew up the miles. text-align: center; The nose baggage compartment of the 414A made CG juggling easier. It can carry up to 8 passengers and baggage, or full fuel, but not both. Answer: TBO means Time Between Overhaul, which is the manufacturers recommended running time, in hours or calendar time, before overhaul. For the same liability coverage amount, pilots who dont meet the above criteria can expect to pay $1,100-$1,600 per year, and the cost increases to $5,700-$12,000 when hull coverage is brought in. Engine and aerodynamic modifications abound for the 414. The 414A has an issue with shock cooling of the engine that occurs during rapid descents. The Cessna 340 is a pressurized six-place twin featuring center-aisle seating, an air-stair door, and top cruise performance. Most accidents involve weather or overloading. - Send us pictures of your plane. 180 One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. Smart design means a better ride. 16 Power. The aircraft got heavier, with the MTOW and landing weight increasing by 400 lbs (181 kg) and 550 lbs (249 kg), respectively. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. So before buying one, you should ensure that there is an AMT with experience on pressurized Cessna twins in your area. The switch for that light is on the underside of a Tee fitting in the pressure line to the tail and thus fills with water, rust and crud and should be pulled and cleaned periodically, or it will fail. Once it reaches the cabin it is compressed enough to create an atmospheric pressure that mimics the desired altitude. by the manufacturer or FAA. The most significant and popular modifications that can be made to a 414A are the engine swaps by the RAM Aircraft Corporation. 3060 In service since 1969. The six- to seven-seat pressurized light transport is a step up for owners of the pressurized 340 and is fitted with the same 310-hp turbocharged engines. The Cessna 152 has a maximum cruise speed of 109 knots and a travel range of 415 nautical miles. These can be purchased by Sierra Industries. As an Amazon Associate I earn from qualifying purchases. By. Specs, range, speed, operating weights and performance for the Cessna 340 here . Pay attention to the fuel system in tip-tanked 414s.A simpler fuel system was among a host of improvements unveiled in 1978 with introduction of the Model 414A Chancellor. As far as handling goes, owners have reported that it is a stable aircraft that behaves in a very neutral manner and reacts to control inputs predictably. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. Cessna Owner Organization. Email Seller Video Chat. The deice light on the panel illuminates only very briefly when the pneumatic deicing system is activated and only indicates that theres pressure to the tail boots. Given the popularity of the 414 series, its fair to say that if you need a modification, you can find it. They dedicated an engineer to my problem and working with my maintenance shop, they developed an approved repair for my wing, possibly saving the ship from the scrap yard! Coupled with smaller engines than the 421, you had an economical transport that could carry a couple of passengers and baggage over 1000 miles or six executives to a day meeting two hours away. The aircraft factors are: These terms are all within the control of the owner. Purchasing a Cessna 414A is considered to be cheap for the number of airplanes you get. That year, most limiting and recommended airspeeds were boosted a few knots (except Vmc, which was lowered from 84 to 82 knots), and the -J engines were replaced with TSIO-520-Ns. One owner reported discovering mis-drilled holes in the spar of his airplane when it was opened up to install the spar strap: ADs 2005-05-52 and 2005-12-13 are current. How much does it cost to fly: $683.19 per hour. AOPA. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. The AD 2005-05-52 was put in place to counteract this issue by using eddy currents to inspect the said struts and visually inspect the auxiliary and rearward struts. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. text-align: center; Interested in buying this aircraft click here. Its a combination of the airstair door, large cabin, air conditioning, abundant baggage space, large picture windows, pressurization and -not to be discounted-the potty! The Chancellors that cost close to $500,000 most often are pristine and like-new. Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. ft/min, ROC 2023 Madavor Media, LLC. Areas to watch on the pressurization system are to make sure the nine drain seals are changed regularly as they deteriorate and become brittle and to regularly check the pressurization ducts off of the heater, forward of the forward pressure bulkhead as they can develop major leaks. Compared to its biggest competitors-the 421 and Duke-a 414 provides a more room than the Duke, as much as the 421, travels a little slower, but does so more economically.MAINTENANCEEnsuring that all ADs have been complied with before buying a 414 will take work, because there have been several dozen of them (not counting a flurry of service bulletins), although the rate of issuance slowed down dramatically in the last 10 years.The current concern is with wing spar cracking in high-time airplanes; with a series of ADs calling for inspections and modifications to the spar-compliance is expensive. Other engine mods include a turboprop-powered conversion of the Cessna 414, named the Turbo Star Pressurized 414, using Allison 250-B17B engines, and the Thielert FADEC-controlled diesel Centurion piston engines that run on commonly available jet fuel. Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners.Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. Liability coverage covers damage caused by the aircraft, including passengers, while hull coverage covers damage to the aircraft itself. They were the last of the pressurized, piston, 400-series airplanes Cessna developed, and pilots and mechanics will tell you that Cessna got it right with the Models 414 and 414A. The 1970 to 77 Cessna 414 is often referred to as a straight 414, straight meaning no suffix A and not meaning a straight wing. Stall mph 79. Empty wt. Loading must be watched carefully to avoid going out of the rear CG limit. By continuing to use this website, you are agreeing to our Cookie Policy. As with all Twin Cessna's, the landing gear and exhaust systems must be maintained properly. All rights reserved. For a private pilot with 1,500 hours total time, an IFR/MEL rating, 500 hours on multi-engined aircraft, and 25 hours on type, the 2021 cost per year for US$1,000,000 liability coverage is in the range of US$850 to US$1,400 per year. The 401, introduced in 1966 and discontinued in 1972, was basically designed as a medium to . Gross wt. text-align: left; - Use this form or email to reach out to us: feedback@planephd.com. In the years following its introduction, the airplane saw few major changes. Cessna's 414 is among a large group of aircraft headed for extinction. Pressurization differential was increased to 5.0 PSI to enable the airplane to maintain cabin altitudes of 10,000 and 11,950 feet at cruising altitudes of 26,500 and 30,000 feet, respectively. Approaching and landing with minimal power is a good habit. Engines two 340-hp turbocharged Continentals. Twin engine piston aircraft with retractable landing gear. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Most had the RAM VI engine conversion. The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. Cited as an excellent IFR platform, youll guess the control forces on the 414 are heavy and stable, yet a great design means only minor trim changes are needed when extending landing gear or flaps. The leaking exhaust gases can make the engine rails crack, a component that is extremely expensive to replace. (RVSM rules have generally limited 414s to 28,000 feet.) These aircraft arent like the 172s. 414's will typically haul 5 people plus bags and full fuel. With the O&N tanks in both nacelles, I can carry up to 260 gallons of fuel, good for over seven hours of endurance. Cruise mph 223. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. You Tell Us, EAA To Host Webinar Event For Aspiring Aviators, National Museum Of The U.S. Air Force Celebrates 100 Years, FAA IACRA System Hit With Database Issues, FAA Nominee Quizzed On Aviation Knowledge, General Aviation Accident Bulletin, February 27, 2023, Pratt & Whitney Canada Passes One Billion Flight-Hour Milestone, AeroLEDs Introduces New Landing Light Series, Universal Avionics Receives TSO Approval For Aperture, MyGoFlights Head-Up Display Division Sold To Partner, AeroBrigham. All rights reserved. [2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. Save my name, email, and website in this browser for the next time I comment. }.tdi_115.td-a-rec-img img{ Empty wt. We previously highlighted engine mount beam fatigue cracking, main landing gear web cracking, and engine frame rail corrosion, all necessitating diligent maintenance inspections and AD compliance. With GAMIjectors and lean-of-peak operation owners report a reduction of about 3 gph per engine at all power settings as well as cooler operating temperatures.Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. The Cessna 414 is an incredibly popular pressurized cabin-class twin, with almost 650 registered in the US alone. (n.d.). Pressurization happens in the engine, where hot air is compressed and then directed to the cabin. Much has been written about the 414s, but its no big deal. The same long-stroke, trailing-link landing gear common to all Citation jets allows the softest landings and smooth taxiing. The 1970 to 1972 models are referred to as short-bodied 414s. All rights reserved. Buyers should be looking carefully for compliance. The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks. Power was provided by twin 340-hp Continental engines, supercharged with AiResearch exhaust-driven compressors and turning full-feathering constant-speed propellers. Answer:The flaps extend to 45 degreesThe TSIO-520-NBs red-line is 2700 RPM. Speed brakes/spoilers are available from PowerPac Spoilers (www.powerpacspoilers.com) and more advanced intercoolers come from American Aviation (www.americanaviationinc.com). The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. Electronic prop synchrophasers became standard equipment in 1976, when two versions of the airplane were put on the market: a bare-bones 414 and a 414II, which came with an assortment of ARC 400-series avionics equipment. The 375-HP 421Cs single engine ceiling is 14,900 feet. It is our mission to be the go to leaders in the aviation industry. However, a 414 RAM VI and VII can often have an excellent useful load with an impressive range/payload chart. ft/min, IAS The difference is that an -N engine uses 38 inches of manifold pressure, rather than 36 inches, and 2700 RPM to produce its rated 310 horsepower. The owners of Cessna 414As have mixed reviews. Fuel capacity 102-207. The 414 was built using parts from other 400-series aircraft. When changes are made to the configuration, such as the addition or reduction of flaps, the aircraft doesnt have to be wrestled back into place, rather small trim changes will do just fine. Answer: Wing loading is the total aircraft mass divided by its wing area. https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). (See page 25 for an abbreviated AD list.). (See www.ramaircraft.com.).