A 30-square-foot increase in wing area accommodated a 400-pound increase in maximum takeoff weight and a 550-pound increase in landing weight. (RVSM rules have generally limited 414s to 28,000 feet.) I bought it to replace a nice Cessna T310R, which I flew for about a year. z-index: -1; 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. Engine and aerodynamic modifications abound for the 414. Cessna's 414 is among a large group of aircraft headed for extinction. 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.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. AOPA. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. With its bigger nose and lockers, the 414A can carry 1500 pounds. The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners. Fuel transferred too early is pumped overboard. Engines two 340-hp turbocharged Continentals. Also, the big Cessnas have safety records that are unmatched by any other light twin. Ceiling 29,800. Seating is spacious and available in a variety of arrangements. Copyright permission must be sought from EUROCONTROL. 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 414A can be upgraded with the usual performance boosters such as vortex generators, which are highly recommended. By continuing to use this website, you are agreeing to our Cookie Policy. Answer:The flaps extend to 45 degreesThe TSIO-520-NBs red-line is 2700 RPM. 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. Annual inspections, repairs and pre-buys must be conducted by specialists. And $34,235 for fixed costs such as insurance. Cessna 414 pressurized-turbocharged - Performance Data . Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. Americas owner-flown aircraft enthusiasts and active-pilot resource, delivered to your inbox! by
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! The main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. 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. 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. If the insurance includes additional hull cover for US$225,000, the annual premium for the experienced pilot will be between US$4,400 to US$5,800 per year, while the lesser experienced pilot can expect US$5,700 to US$12,000 per year. 4,640. Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. Cessna made the most significant changes to the Chancellor when it introduced the 414A. Training is a must. Cessna 414As that comply with all their service bulletins and airworthiness directives, have been maintained well, and dont have too much time can fetch a good price. Save my name, email, and website in this browser for the next time I comment. The Cessna Pilots Association, located at www.cessna.org, and the Twin Cessna Flyer, at www.twincessna.org. 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. Ownership and operating costs. Ball reports that the pressurization controller diaphragms only last for about five years and the cabin pressure dump switch on the right landing gear should be checked often as well. He received his training at the University of North Dakota and has been in love with aviation for many years. It is a very stable instrument platform and I find it as easy to land as the T310 or any of the large singles Ive flown. The gear system of the 414A is easy to maintain, with one spot to watch: When assembling the center bolt on the main landing gear scissors, the correct washers must be installed in the correct sequence or the bolt can pull out, allowing the main gear wheel to turn sideways.Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. It is the first turboprop-engine aircraft designed and manufactured by Cessna in the 1970s. The system left room for error, not only on the part of the pilot, but among line personnel. Aerodynamic mods include vortex generators to increase aileron and rudder control authority at low speeds. That is why an approval to modify them is classed as supplemental. The exact specifications of the Cessna Chancellor 414A are: A hotch-potch of the Cessna 401 and 421, the Chancellor easily stole the limelight as the best of the 400-series, even though it was meant to simply fill the gap between the two, and became a hit among pilots everywhere, and in recent years has gained popularity with charter operators. Fuel burn is the same, 34 GPH in cruise at all altitudes, with the RAM VII at 69 percent. .tdi_115.td-a-rec{ Initial climb rate 1,700. Specs, range, speed, operating weights and performance for the Cessna 340 here . The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. The figures show that the demand for Dakotas has increased causing prices to rise by about 40 percent. [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. Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. 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. 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. 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. The piping which directs the exhaust from the manifold to the turbo is also susceptible to cracking. 3060
)A potential buyer should carefully investigate the compliance status of the airplane by flight time and serial number, especially if the airplane is high time. Buyers should be looking carefully for compliance. 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. Empty wt. 230
All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. }.tdi_115 .td-element-style{ It is the flying carpet my wife always wanted, including a potty! The STANDARD DATA: Seats 6-8. Limiting speed for the extension of 15 degrees of flap was raised from 164 to 177 knots; Vlo and Vle were increased to an impressive 177 knots, from 143 knots.Beginning in 1978, Cessna offered three basic equipment packages. Rate of Climb: 1650 fpm; Climb Rate One Engine Inop: 315 fpm; Max Speed: 243 kts; Normal Cruise: 229 kts . Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. The aircraft is powered by two Continental TSIO-520-NB piston engines. The Cessna 411, first delivered in 1965, was one of Wichitas first ventures into the airliner market. kg, IAS
It's tempting to decry the disappearance of the classic country airport. by the manufacturer or FAA. The 414A has a combined 620 hp (456 kW), however, takeoff acceleration might not be as neck-snapping as one would assume. So newer, more powerful engines with stronger components and increased aerodynamics all of which boost performance greatly and increase the value. 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. The older 414s are known as the short-bodied models. Go figure. Answer: TTAF stands for Total Time Airframe, which refers to the number of flying hours the airframe has accumulated since new. With the RAM IV, useful load is over 2100 pounds, which enables one to carry full fuel plus 900 pounds. Purchasing a Cessna 414A is considered to be cheap for the number of airplanes you get. The RAM VII changed all that. Cessna 414A Ram V - TAKEOFF and LANDING (Short Flight) Evan Luft 29.3K subscribers Description 92K views 6 years ago Flying a Cessna 414A with Ram V liquid cooled engines! 1000
Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. All rights reserved. Despite that, cylinder head cracking has been a persistent problem for the -N and -NB engines (as well as for other IO-, TSIO- and GTSIO-520s). In the years following its introduction, the airplane saw few major changes. They are the Cadillacs of the piston line, with attention having been paid to detail; even on an. The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks.This makes room in the mains because all return fuel and vapor from the engines is routed back to the mains rather than to the tank selected. Handling, range, speed and fuel economy, and hourly costs are often considered to be at or exceeding the industry standard. The basic 414 was born in 1970 with a 4.2 psi pressurization differential and ascended to become the Chancellor in 1978. The greater the experience of the owner/pilot, the lower the premiums. Baggage capacity of the 414 is 930 pounds, and cabin seating is available with an array of executive options. Optional auxiliary and locker tanks were available to boost usable capacity to 180 gallons, then to 203 gallons in 1973.The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. Flight planning or any other aircraft operations should only be done using official technical information provided 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. The Cessna 340 is a pressurized six-place twin featuring center-aisle seating, an air-stair door, and top cruise performance. . The name Chancellor was used for models marketed from 1976. Its an $800 part. Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. Both were quick to praise the 414 and especially the 414A as the best of the Cessna piston twins, with good systems, particularly the hydraulic gear on the 414A. Engines two 375-hp turbocharged Continentals. 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. kt, Distance
The same long-stroke, trailing-link landing gear common to all Citation jets allows the softest landings and smooth taxiing. At 11,350 feet, the 414's single-engine service ceiling is below average, but, at 19,850, the 414A is tops in its class.
The 1970 to 1972 models are referred to as short-bodied 414s. One club offers extensive support for the 414, in addition to all other twin Cessnas. NM, ROD
The big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte. Ball at 219-749-2520. 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. On November 1, 1968, the prototype registered N7170C, conducted its maiden flight. The 414A has an excellent safety record for good reason. 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. Initial climbout increased by at least 200 FPM to more than 1000 FPM. When discussing landing distance, two categories must be considered: Actual landing distance is the distance used in landing and braking to a complete stop (on a dry runway) after crossing the runway threshold at 50 feet; and, Required landing distance is the distance derived by applying a factor to the actual landing distance. Email Seller Video Chat. The 414 seats up to 6 passengers plus 1 pilot. https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). Faster aircraft generally have a higher wing loading as less area is required to carry the same mass. All rights reserved. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Continental also published overhaul procedures to enable -NB engines to get the TBO boost. He's worked on various aircraft from small two-seaters like Tomahawks or Boeing 767s. 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.The exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. However, there seem to be plenty that are not. The other category that brings the price up to the same number are the aircraft that have undergone a RAM conversion. The Cessna 152 has a maximum cruise speed of 109 knots and a travel range of 415 nautical miles. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. The 414 does have AD97-26-16 requiring consideration, and those aircraft requiring regular x-ray and ultimate installation of the service kit will necessarily command a lower price. So before buying one, you should ensure that there is an AMT with experience on pressurized Cessna twins in your area. Answer: An STC refers to a Supplemental Type Certificate. Come join us! Empty wt. According to Hangar 67, a very high-time 1979 model year 414A was recently sold at $129,900, which is the lowest price we have found. The top of the line for the 414 is the series VI. The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. Developed from the 310, it utilizes a similar landing gear and tail unit. Landing distance (50) 2,393. fitness for any purpose is made or implied. Bombardier Challenger 350 Guide and Specs: Is It Up to the Challenge? Reaching fever pitch in the 1980s, Cessna had positioned itself well for the demand, offering light twins for almost every conceivable subsection of the market. RAM also makes winglets and vortex generators. The Cessna 414 is an incredibly popular pressurized cabin-class twin, with almost 650 registered in the US alone. Landing Distance: 3,170 ft (966 m) Maximum Operating Altitude 45,000 ft . When told to top off the mains, a line person may not realize that the mains are the tip tanks and will fuel only the aux tanks. We use cookies to help you get the best experience when using our website. Currently, David flies twin retractables, notably the Pa44 Seminole and Pa30 Twin Comanche. The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks. But the average price of a 414A is around $300,000, while the price range is between $200,00 $500,000. To better manage fuel, a fuel computer was added to the list of available options. 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. Precise Flight and Spoilers, I. Thus, it is an indication of age and use. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. The pressurized comfort of the 414A, which produces an 8000-foot cabin at 22,800 feet, cannot be overemphasized. 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 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. Lots of external baggage in the nose and wing lockers, a pressurized aft cabin baggage area for desired in-flight items, like food, toys/games, cosmetics and a roomy pressurized 6000-foot cabin at 20,000 feet. 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. STANDARD DATA: (T310R) Seats 4-6. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. It's also a myth. Handling is good, too. Stall mph 82. The owners of Cessna 414As have mixed reviews. Cessna 414 Stock Airplane vs. RAM Series VII; Primary Specifications Cessna 414 Give me one three-hour cross country with any new owner and hell be able to teach the system. 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. Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. Another point of consideration for a 414 buyer is the SB/AD on the wing spar. ( 2023 Madavor Media, LLC. The standard aviation insurance all aircraft owners take is liability coverage, while hull coverage is optional. The cabin length is 3.5 meters, height is 1.3 meters, and width is 1.4 meters. Landing Distance: 2393 ft: 729 m: Max Takeoff Weight: 6751 lbs: 3062 kg: Max Landing Weight: 6750 lbs: 3062 kg: Useful Weight: 2417 . As an Amazon Associate I earn from qualifying purchases. 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. 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. Cessna 195 Guide and Specs : All About The 195 Businessliner, Bombardier Challenger 300 Guide and Specs, Installed equipment, specially avionic fit-out. Pressurization happens in the engine, where hot air is compressed and then directed to the cabin. Landing distance (50) 1,765. . An improved variant the Cessna 414A Chancellor was introduced in 1978 with the major change being a redesigned and increased-span wing with integral fuel tanks and an extended nose to give more baggage space.