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: 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. These aircraft were called the 414 Chancellor. Cessna 414 chancellor. Cessna made more room for roughly 410 lbs (185 kg) baggage and equipment such as avionics by fitting on the nose of the 421 onto the 414A to which made the aircraft longer. Built-in airline-like stairs are in the door. FL These aircraft were called the 414A Chancellor. Refreshment centers can be aft or a vertical unit positioned behind the pilot or copilot seat. Fuselage strakes improve yaw control, performance in turbulence, and a higher cruise speed. Sure, many have been plowed up for houses or 2023 Aviation Publishing Group. By continuing to use this website, you are agreeing to our Cookie Policy. ft/min, ROC Gross wt. The variable costs such as maintenance for the airframe, as well as other costs such as landing and parking fees totaling $206,550. 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. On a standard day, when loaded to MTOW, it needs 4,000 ft (1,219 m) to hit Vr and then come to a complete stop. 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. 4,640. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. Takeoff distance (50) 2,010. Come join us! All aircraft, engines, and components have type certificates that approve their use. 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. 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. 150 Many supplemental type certificates exist for the aircraft that allow upgrades to improve performance. Model 414 seats up to 7 passengers and 1 pilot. The pressurized 414 was developed to appeal to owners of unpressurized, twin-engined aircraft, and was based on the fuselage of the Cessna 421 and used the wing design of the Cessna 401. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. I cannot count the number of heater failures Ive suffered over the years and the number of maintenance folks who have done their best to help me. 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. 720 The name Chancellor was used for models marketed from 1976. The Cessna 414 Chancellor was produced from 1968 to 1985. The mod is expensive, but in my case we found serious factory mis-drilled wing spar attachment holes that could have caused a spar failure at any time! By continuing to use this website, you are agreeing to our Cookie Policy. For the Cessna 414A Chancellor, average pricing was US$280,000, having approximately 7,500 hours total time airframe (TTAF) and mid-life engines. 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. Thielert claims increased power and improved fuel economy over other available conventional piston engines. One of our Planephd Experts will be in touch with you shortly. 3,865. Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: However, only upon acquiring the 414 did I finally attain my goal-virtually complete independence from the airlines for domestic travel. Fuel transferred too early is pumped overboard. Thus, it is an indication of age and use. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. I use SimCom. By. ( Top mentions include the true cabin class, reasonable cruise speed, and maintenance of sea-level pressure to 10,000 feet. Interested in buying this aircraft click here. If followed carefully, a mechanic wont miss anything. }@media (max-width: 767px) { (n.d.). Their parts may seem expensive, but they continue supporting us owners, and for that I am very willing to see them earn afair profit. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. 2023 GlobalAir.com. 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. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. The Chancellor 414A has an impeccable safety record. Baggage capacity of the 414 is 930 pounds, and cabin seating is available with an array of executive options. Engines two 285-hp turbocharged Continentals. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). (RVSM rules have generally limited 414s to 28,000 feet.) 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. We use cookies to help you get the best experience when using our website. Stall mph 79. Gross wt. 310, Range 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. Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. Takeoff distance (50) 2,175. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. The number of maintenance problems that can and do arise can cost a lot of money in a short time frame. AOPA. Answer: Wing loading is the total aircraft mass divided by its wing area. Absolutely the Right 414A RAM IV, This Aircraft is Impeccable and reflects the condition and attention to details that this owner has given N414EM with Only 20 Hours on each RAM Engine and 20 Hours.See More Details. Most accidents involve weather or overloading. The updated Chancellor abolished the original tip tanks in favor of a longer wet wing, benefitted from a lengthened fuselage, mounted an improved 5.0 psi pressurization system, and enjoyed a 400-pound heavier gross weight. It is the first turboprop-engine aircraft designed and manufactured by Cessna in the 1970s. Introduced in 1978, the Cessna 414A or more commonly known as the Cessna Chancellor III, is a pressurized, twin-engined aircraft, with retractable landing gear. It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. The most significant and popular modifications that can be made to a 414A are the engine swaps by the RAM Aircraft Corporation. 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 flying carpet my wife always wanted, including a potty! The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg. How much does it cost to fly: $683.19 per hour. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. 3,865. 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. 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. Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. 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. It's the third model in the Chancellor line and the successor to the Cessna 414II. Email Seller Video Chat. In 1973, an updated 414 was released with major changes, this model was named the 414II. 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. Pricing 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 Cruise mph 223. A 414A RAM Series VII with Winglets (AW) will compete in many ways with a 421C. Range 1,284. (See www.ramaircraft.com.). The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. Landing distance (50) 1,815. 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. I have owned a 1979 C414AW (a 414A with RAM winglets) for five years and about 2400 flight hours. The 375-HP 421Cs single engine ceiling is 14,900 feet. kts, ROC 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. It's tempting to decry the disappearance of the classic country airport. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. kts, ROC Go figure. Even though Cessna Chancellor 414A has a good safety record, the earlier 414s and their complicated fuel system have caused a few scares, the most recent one in 2018. Ceiling: 30,800 FT Ceiling (1 engine out): 19,850 FT Takeoff distance: 2,185 FT Landing distance: 1,013 FT Takeoff distance over 50ft obstacle: 2,595 FT Landing distance over 50ft obstacle: 2,393 FT Weights Gross Weight: 6,750 LBS Empty Weight: 4,543 LBS Maximum Payload: 1,769 LBS Fuel capacity: 213 GAL Ownership Costs 1978 Total Cost of Ownership: In 1978, an enhanced version was launched, designated as the 414A Chancellor. There were significant changes made to the body of Chancellor 414A as well. A cabin differential of 5.0 psi allows a 10,000-foot cabin at 26,500 feet. Aviation Consumer. ) 1000 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. It was developed to bridge the gap between the unpressurized Cessna 401 and the pressurized, more powerful Cessna 421. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. Cruise mph 277. The aircraft also featured a 28V, negative ground, direct current electrical system charged by an alternator on each engine, and a 24V battery. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. Empty wt. https://www.federalregister.gov/documents/2005/06/14/05-11613/airworthiness-directives-cessna-aircraft-company-models-402c-and-414a-airplanes, Cessna 414. If followed carefully, a mechanic wont miss anything. Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. One of the most distressing issues the Cessna 414A has is cracking along the forward wing spars. It is powered by two wing-mounted 310hp (231kW) Continental TSIO-520-J horizontally opposed, six-cylinder engines. ft/min, ROC In airplane engines, turbochargers are popularly used to achieve forced induction. Derived from the Model 411, the Cessna 401 and 402 are essentially the same aircraft put to two different uses. The 421B tiptank twin Cessna has fuel carried in the mains (tips), auxiliary fuel cells in the wings and optional nacelle tanks. The upgrade from the T310R came about because my family, including a dog, cannot all be wearing nosebags. The air is run through a compressor connected to the intake manifold of the engine to create a more efficient fuel burn which will eventually produce more power. 1000 All rights reserved. 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. The 414A has a combined 620 hp (456 kW), however, takeoff acceleration might not be as neck-snapping as one would assume. Therefore, finding parts to support the aircraft is not difficult. }.tdi_115.td-a-rec-img img{ Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. 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. Answer: The process of delivering compressed, denser air to a combustion engine is referred to as forced induction. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. However, as aircraft age, they dont get cheaper to own or operate, which the price will reflect. - Aircraft specific reviews and articles. Also says to increase landing distance by 45% (doesn't seem to make sense). 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. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. B. C. (2015, July 13). 200 That said, the aircraft is not a great load lifter, stack in the people, and theyd better have no baggage and be wishing to travel only short hops. The cabin length is 3.5 meters, height is 1.3 meters, and width is 1.4 meters. Above this speed, turbulence or rapid control deflections increase the chance of structural damage. Six seats were standard; a seventh was available as an option. Each of its 620 hp has to carry 10.8 lbs, which is quite poor. Over its production run the number of 414s and 414As were evenly split, with 516 and 554 built, respectively. The standard aviation insurance all aircraft owners take is liability coverage, while hull coverage is optional. Would like to understand why. Given the popularity of the 414 series, its fair to say that if you need a modification, you can find it. With its bigger nose and lockers, the 414A can carry 1500 pounds. kt, MCS RAM also makes winglets and vortex generators. Stall mph 81. Cessna Owner Organization. This plane was. Less powerful, light and low cost model of CESSNA 421 Golden Eagle. In the early 414s, the main landing gear webbing is prone to cracking, requiring extensive rectification. 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. Both refer to ratings or approvals that a pilot must achieve to enable the operation of a multi-engined aircraft or flight under instrument flight rules. 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! 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. The design of the Cessna 414 was to bridge the gap between their unpressurized twin, the Cessna 402, and their pressurized flagship, the Cessna 421. The 414A has an issue with shock cooling of the engine that occurs during rapid descents. Landing Weight - lbs. The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. 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. Special Missions. ft/min, IAS The Cessna Pilots Association, located at www.cessna.org, and the Twin Cessna Flyer, at www.twincessna.org. 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. Checking the Cessna 152 POH it says to increase takeoff distance by 15% of ground roll (makes sense due to increased friction). There are only two fuel-. The Chancellor utilizes the hydraulic components of the Golden Eagle gear and features a five-second retraction time. ( The 414 and 414A are popular aircraft with considerable numbers worldwide, and unless some economic or aircraft supply-side variable changes, you can expect your 414 to command a reasonable resale price from someone needing a serious, cabin-class, high-performance twin. 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.
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