The Chancellor has a service ceiling of 30,800 feet and a maximum speed of 235 knots. Insurance costs have equaled $7000 per year for the last couple of years for $1 million smooth with a hull value of $350,000. Takeoff distance (50) 2,010. text-align: center; That is why an approval to modify them is classed as supplemental. At 11,350 feet, the 414s single-engine service ceiling was a bit below average; but, at 19,850, the 414A is tops in its class.Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. Plane and Pilot builds on more than 50 years of serving pilots and owners of aircraft with the goal of empowering our readers to improve their knowledge and enthusiasm for aviation. With its bigger nose and lockers, the 414A can carry 1500 pounds. Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. After the Chancellor debuted, there were few further refinements. It is the first GA airplane Ive ever owned or flown that treats passengers as comfort-seeking humans and not adventurous sardines. The popularity of the aircraft ensures that there are enough aftermarket parts that can be bought if used parts are unavailable. I have split my time about equally between the RAM IV 325-HP engines and the RAM VII 335-HP engines and Scimitar props that I had installed when the RAM IVs hit their TBO. 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. (RVSM rules have generally limited 414s to 28,000 feet.) Specs, range, speed, operating weights and performance for the Cessna 340 here . One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. (n.d.). ft/min, IAS Range 1,284. 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. 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. 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. Cessna Chancellor III (414A) Guide & Specs, Cessna Chancellor (414A) Performance and Handling, Piper Mirage Guide and Specs: All You Need To Know. One of the biggest weak points of the 414A is the problematic Continental TSIO-520-NB engine. Email Seller Video Chat. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Ceiling 29,800. 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. I own a 1978 Cessna 414A which I acquired in 1989. VGs are also available from Micro Aerodynamics (www.microaero.com) and V/G Systems, phone 800-328-4629. This can be a great aircraft and a good buy, but only for a pilot who doesnt need lots of payload. Ive previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. 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. With the RAM IV, useful load is over 2100 pounds, which enables one to carry full fuel plus 900 pounds. The 16 inches of extra length and the added side window do not directly mean much, but short-bodied 414s rarely have the typical cabin-class size refreshment center nor a potty. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. In service since 1969. Four different pressurization systems were offered during the run of the 414A, so its essential that the maintenance technician working on a pressurization glitch confirm which system by aircraft serial number. Kudos go to Cessna for rising to the occasion. Rate of Climb: 1650 fpm; Climb Rate One Engine Inop: 315 fpm; Max Speed: 243 kts; Normal Cruise: 229 kts . 414,Chancellor Bombardier Global 8000 Guide and Specs: Superior Sonic Transportation, Embraer Legacy 450 Guide and Specs: The Stepping Stone, Bombardier Challenger 300 Guide and Specs. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. The takeoff distance is 408 meters while the landing distance is 365 meters. . So, if its just pressurization youre looking for and youre going to be flying with only another person or two aboard, you might want to look at the 340 for a personal hot rod. Thielert has offered engine conversions using their Centurion Engines. The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. All told, Cessna built nearly 1000 of the airplanes-roughly a 50/50 split between early tip-tanked 414s and wet-wing 414A Chancellors-during 16 years of production. 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. kts, ROC In 1978, an enhanced version was launched, designated as the 414A Chancellor. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. Most accidents involve weather or overloading. (38.0 gallons/hr @ $5.40/gal), Misc: landing, parking, supplies,catering, etc, Typical Price: $307,752.00 STANDARD DATA: ( 411) Seats 6-8. We spoke with Michael Cook and Todd Voshell who direct maintenance at Rapid Air, in Grand Rapids, Michigan, which has been operating 300 and 400 series Cessna twins for over 25 years. With bigger turbochargers and intercoolers, much larger cowl flaps, new intake air scoops, and Scimitar props, the airplane becomes an entirely new animal within seconds of leaving the runway. I have put in three different heaters over the past several years and changed out all the blower motors, ductwork, fuel pump, fuel pressure regulator, igniter, air flow sensor and thermostat at least once and I still plan for failure in flight. Maximum operating altitude of 30,800, a optimal cruise speed of 203 knots/234 MPH, and a 705 NM/811 SM seats-full range. Range 1,284. The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. In 1979, the 402s received a new wing, with a 5 feet (1.5 m) greater span. (See www.ramaircraft.com.). Landing distance (50) 1,790. We use cookies to help you get the best experience when using our website. 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. Americas owner-flown aircraft enthusiasts and active-pilot resource, delivered to your inbox! Thielert claims increased power and improved fuel economy over other available conventional piston engines. It is the flying carpet my wife always wanted, including a potty! no data Precise Flight and Spoilers, I. Loading must be watched carefully to avoid going out of the rear CG limit. Aerodynamic mods include vortex generators to increase aileron and rudder control authority at low speeds. Ball also says that heated windshields should be checked often to ensure there are no cracks. Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. 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. Cessna 120 Guide and Specs : Is It Powerful Enough? Speed brakes/spoilers are available from PowerPac Spoilers (www.powerpacspoilers.com) and more advanced intercoolers come from American Aviation (www.americanaviationinc.com). The cabin length is 3.5 meters, height is 1.3 meters, and width is 1.4 meters. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). 3,467. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. Landing distance (50) 1,850. Engines two 340-hp turbocharged Continentals. 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. Plane and Pilot expands upon the vast base of knowledge and experience from aviations most reputable influencers to inspire, educate, entertain and inform. Landing distance (50) 1,765. . The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. 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! Gross wt. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads. Optional auxiliary and locker tanks were available to boost usable capacity to 180 gallons, then to 203 gallons in 1973. Frequently, a a buyer makes assumptions that arent correct. ( Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. The aircraft also featured a 28V, negative ground, direct current electrical system charged by an alternator on each engine, and a 24V battery. However, the eddy current method did not effectively identify the cracks until it was to the point where a load much lower than the published maximum load can cause catastrophic structural damage. Cessna made the most significant changes to the Chancellor when it introduced the 414A. According to Cessna, 4.2-psi cabin pressure differential could be maintained by either engine operating at 60 percent power. by the manufacturer or FAA. Also, the big Cessnas have safety records that are unmatched by any other light twin. The owners of Cessna 414As have mixed reviews. Controls consisted of on/off/crossfeed valves and a fuel flow computer/indicator was added.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. There was a time in aviation history when aircraft manufacturers were falling over themselves to serve a seemingly insatiable demand for executive-level light twin-engined aircraft. Operating Costs. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. For the Cessna 414A Chancellor, average pricing was US$280,000, having approximately 7,500 hours total time airframe (TTAF) and mid-life engines. Also, corrosion on the engine frame rails is possible from exhaust leaks where the manifold exits into the turbocharger. 100 Landing distance (50) 1,815. The landing gear is the same as the 414, but the horizontal and vertical stabilizer, elevator and rudder are the same as the 310; minor changes in the 310 tail make it interchangeable with the 340. They are the Cadillacs of the piston line, with attention having been paid to detail; even on an288airplane of this vintage, only slight trim changes are needed when flaps or landing gear are reconfigured, although single-engine handling, as with any piston twin, is demanding and requires regular practice.The big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte. The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. It is our mission to be the go to leaders in the aviation industry. Range 568-1,322. Answer: The process of delivering compressed, denser air to a combustion engine is referred to as forced induction. 7,450. kg, IAS GlobalAir.com is your partner in connecting you with relevant information and resources. Approaching and landing with minimal power is a good habit. The 340 has a gross weight of 5,975 pounds, and an empty weight of 3,697 pounds. In a study of accident records some years ago, the 414 stood out as the safest light twin. The Chancellor is a popular aircraft, so it has an extensive range of aftermarket parts and modifications. Takeoff distance (50) 2,220. Answer: TBO means Time Between Overhaul, which is the manufacturers recommended running time, in hours or calendar time, before overhaul. When we look at the power loading of the aircraft, the why becomes obvious: weight. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. by Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. 6,200: 6,430: Zero Fuel Weight - lbs. B. C. (2015, July 13). Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. TAKE-OFF MTOW: WTC: RECAT-EU: Light Distance: V2 (IAS): 520 m 100 kts INITIAL CLIMB (to 5000 ft) IAS: ROC: 130 kts 1200 ft/min CLIMB (to FL 240) IAS: ROC: 150 kts 800 ft/min CLIMB (to FL 150) IAS: ROC: 150 kts 1000 ft/min MACH CLIMB MACH: ROC: - - CRUISE MACH: Ceiling: - 310 FL TAS: 230 kt Range: 1100 NM INITIAL DESCENT (to FL 240) MACH: - ROD: - A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. The original 414 aircraft retailed at US$138,000 in 1970. 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. The Cessna 414 was given a clean wing in 1978. Landing Distance: 2393 ft: 729 m: Max Takeoff Weight: 6751 lbs: 3062 kg: Max Landing Weight: 6750 lbs: 3062 kg: Useful Weight: 2417 . The Piper Seneca is also quite similar to the 414A, even though it is slightly smaller. RAM also makes winglets and vortex generators. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. 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. Phone: (305) 342-0760. 2023 GlobalAir.com. An AD that requires the propeller hubs to be filled with red indicator oil to make cracks more visible was also released. However, single-engine performance at sea level is lower than the competition, with the aircraft only being able to climb 290 ft (88 m) per minute. A brand new engine exchange from Continental costs an average of $60,000. The V upgrade swaps out the Continental TSIO-520-NB for a more powerful big-bore, liquid-cooled Continental TSIOL-550A Voyager engine which produces 350 hp. The other category that brings the price up to the same number are the aircraft that have undergone a RAM conversion. To reach a cruising speed of 214 KTAS (246 mph / 396 kmph) 75% power is required, which will cause the 414A to burn around 19 gph (72 lph) per engine. The fuel economy of the 414A depends on the altitude, conditions, and power setting, but the general specific fuel consumption is approximately 0.44 lbs/hp/hr. Ball at 219-749-2520. It uses spent exhaust gases to run the compressor, which draws in and compresses clean air to deliver to the engine. Aviation Consumer. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. 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. And $34,235 for fixed costs such as insurance. 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. fitness for any purpose is made or implied. In addition to 335-HP engines, new props and intercooler scoops, it includes a set of vortex generators and gives an increase in useful load of 415 pounds. In the years following its introduction, the airplane saw few major changes. Maximal total range:705 NM / 811 SMCruise speed:203 knots / 234 MPHAverage price:$344,804.81Number of passengers:7 people, Your email address will not be published. Checking the Cessna 152 POH it says to increase takeoff distance by 15% of ground roll (makes sense due to increased friction). Six seats were standard; a seventh was available as an option. However, some years, unexpected maintenance can eat your lunch. The Cessna 414 Chancellor was produced from 1968 to 1985. I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. All rights reserved. Ceiling 27,400. Stall mph 82. These aircraft were called the 414A Chancellor. Baggage capacity of the 414 is 930 pounds, and cabin seating is available with an array of executive options. Service ceilings are above 30,000 feet, but few owners fly that high. However, it takes a longer distance high wing loading aircraft to takeoff and land. There are several problems that the 414A has. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. Operating and maintenance costs are attractive when compared with those of competing airplanes, such as the big-brother 421 and Beech Aircrafts Duke. NM, ROD 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. Top mentions include the true cabin class, reasonable cruise speed, and maintenance of sea-level pressure to 10,000 feet. Owners speak of the 414s smoothness, stability, and ease with which you can trim the aircraft out. Down low under 10,000 feet, things are much slower, more like 170 to 175 KTAS. In 1973 Cessna stretched the fuselage by 16 inches and added a fifth side window. During that period, I have exchanged two sets of engines (RAM IV), two props (one new set), two paint jobs, an interior and updated the avionics. No warranty of 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. There are several good training programs available to help keep 414 pilots in top form, something we feel to be quite important as, while the accident rate is low, the accidents seem primarily to occur on amateur flown airplanes and involve judgment errors on the part of the pilot rather than anything wrong with the airplane. It is a less powerful and lighter evolution of the Cessna 421. The 411A, produced from 1967-68, featured a redesigned nose and more baggage space. 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. In general, all owners praise the performance and capability of the aircraft, especially ones that have a RAM conversion and STOL kit, because it makes the aircraft much more versatile. Flight planning or any other aircraft operations should only be done using official technical information provided 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. MEL, in this case, refers to Multi-Engine Land. 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. According to Cessna, 4.2-psi cabin pressure differential could be maintained by either engine operating at 60 percent power. A 414A RAM Series VII with Winglets (AW) will compete in many ways with a 421C. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. 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. The 375-HP 421Cs single engine ceiling is 14,900 feet. The RAM IV struggled in the flight levels, especially in the summer. 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. Pricing So, if its just pressurization youre looking for and youre going to be flying with only another person or two aboard, you might want to look at the 340 for a personal hot rod.A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. ), Please tell us: Send feedback comments to the EUROCONTROL Training Institute. However, thanks to GAMIjectors and the graphic engine monitor, I can set the fuels flows at 13 to 14 GPH (thats not a typo) at altitude, watch the TAS sink to 195 KTS and drive the aircraft for nearly seven hours. 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 original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. He received his training at the University of North Dakota and has been in love with aviation for many years. Cessna Country: United States Manufactured: 1978 to: 2006 ICAO: C550 Price: US$1.1 million (2019) Performance Weights Dimensions Avionics: Garmin 700 Engine: 2x Pratt & Whitney Canada JT15D-4B Turbofan Power: 2,500 pound-force Max Cruise Speed: 403 knots 746 Km/h Approach Speed (Vref): 82 knots Travel range: 2,000 Nautical Miles 3,704 Kilometers He's worked on various aircraft from small two-seaters like Tomahawks or Boeing 767s. Four variations are available, all of which offer a boost in useful load, increased TBOs and new props. It can carry up to 8 passengers and baggage, or full fuel, but not both. Continental also published overhaul procedures to enable -NB engines to get the TBO boost. Pressurization happens in the engine, where hot air is compressed and then directed to the cabin. He was a glider pilot for several years before obtaining his private license in taildraggers. Fuel cost per hour: Passengers love it for space, comfort, and low noise levels. The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. The Cessna 152 has a maximum cruise speed of 109 knots and a travel range of 415 nautical miles. Another great resource is the Cessna Pilots Association, it offers a monthly magazine, forums, technical information, and even training. Combining spacious cabins and relatively small, efficient engines, the 414 series can carry lots of fuel or a small crowd with their belongings-but not both. In the years following its introduction, the airplane saw few major changes. The remedy for this was increased visual inspections and the strengthening of the wing spars by adding spar straps. Empty wt. airplane of this vintage, only slight trim changes are needed when flaps or landing gear are reconfigured, although single-engine handling, as with any piston twin, is demanding and requires regular practice. By. For 1981, Chancellor refinements included a heated fuel manifold, frost panes for cockpit side windows, and threadless-blade propellers. Over its production run the number of 414s and 414As were evenly split, with 516 and 554 built, respectively. The landing gear was replaced, using the simpler system from the Cessna 414. They are the Cadillacs of the piston line, with attention having been paid to detail; even on an. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. Load a six-person marketing staff with 800 pounds of equipment, and there will be room left for only about 1.5 hours of fuel. The Cessna 180 Skywagon is not a beautiful airplane, but it is a classic-looking taildragger that became an . Handling, range, speed and fuel economy, and hourly costs are often considered to be at or exceeding the industry standard. The first Cessna Chancellor - the 414 - took to the skies in 1968, and was produced from 1970 onwards. The standard aviation insurance all aircraft owners take is liability coverage, while hull coverage is optional. We are a collective group of airline instructors, and pilots dedicated to all things aviation. The Chancellor replaced the former 414 in 1978 and offered a new level of payload performance, range, and fuel efficiency. RAM also makes winglets and vortex generators. The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. The 414 and 414A truly provide a great family or business aircraft. The applications are smaller and they have maintenance issues, so the price does fall. Answer: Pressurization is the creation of a false atmosphere in the cabin of the aircraft in order to allow us to breathe at higher altitudes without pure oxygen. How much does it cost to fly: $683.19 per hour. 16
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