But the average price of a 414A is around $300,000, while the price range is between $200,00 $500,000. It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. 100 Also, the big Cessnas have safety records that are unmatched by any other light twin. Engines two 340-hp turbocharged Continentals. Bringing the grand annual total to $240,785. The Chancellor utilizes the hydraulic components of the Golden Eagle gear and features a five-second retraction time. Three significant milestones in 414 development took place in 1973, 1976, and 1979. A pilot in a hurry will see 205 knots on 38 GPH at 75 percent power rich of peak, although few operate that way anymore. - Use this form or email to reach out to us: feedback@planephd.com. What a difference! 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. 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 package that gives the 414A the most significant boost in performance is the series V upgrade. 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. Empty wt. The 414A can be upgraded with the usual performance boosters such as vortex generators, which are highly recommended. BUILT FOR TRAINING Ideal for entry-level landings, the Skyhawk piston features a sturdy tricycle landing system and a resilient airframe. Take an early model 414 with -J engines and complete this upgrade to receive a 1600 hour TBO, up from the original 1400. Given the popularity of the 414 series, its fair to say that if you need a modification, you can find it. 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. Thielert has offered engine conversions using their Centurion Engines. 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. Mike Buschs Savvy Owners seminar is valuable. 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. The standard aviation insurance all aircraft owners take is liability coverage, while hull coverage is optional. How much does it cost to fly: $683.19 per hour. The 1970 to 1972 models are referred to as short-bodied 414s. Other modifications in 1978 included a longer nosecone, a redesigned undercarriage system, and an extended wing without the earlier tip tanks. 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. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. There are only two fuel-288quantity indicators, both with three-position switches, to help the pilot keep track. Four variations are available, all of which offer a boost in useful load, increased TBOs and new props. 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. When we're not in the air, we're here helping others how to join us here at Aviator Insider. Data from Jane's All The World's Aircraft 198283[8], Last edited on 27 February 2023, at 22:02, "RAM Altitude Performance Enhancing Winglets", "CENTURION ENGINES - Cessna 340, 414 & 421", "National Transportation Safety Board Aviation Accident Final Report Accident Number: FTW82AA299", https://en.wikipedia.org/w/index.php?title=Cessna_414&oldid=1141981287, This page was last edited on 27 February 2023, at 22:02. The most significant and popular modifications that can be made to a 414A are the engine swaps by the RAM Aircraft Corporation. There are only two fuel-. If Cessna Kit SK414-19-1 is incorporated, the inspection is due every 9,600 hours. Overall, the 414A is a capable aircraft. Derived from the Model 411, the Cessna 401 and 402 are essentially the same aircraft put to two different uses. I sell 25 Twin Cessnas a year, which usually includes six to eight 414s and 414As. The Cessna 414 Chancellor was produced from 1968 to 1985. I am a professional aircraft broker who specializes in Twin Cessnas. no data Six seats were standard; a seventh was available as an option. Flight planning cruise speeds appear to be between 190 to 200 knots with 37 to 38 mph fuel consumption while operating cost per hour for most owners is sub-$400. . The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. Accident statistics suggest that no common threads are pointing to the system or design problems on the 414. FL 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. Ensuring 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. Ive previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. The aircraft got heavier, with the MTOW and landing weight increasing by 400 lbs (181 kg) and 550 lbs (249 kg), respectively. Lightly loaded and at economic power settings, expect to get almost 1,300 nautical miles of range. 5,500. 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. 1200 In airplane engines, turbochargers are popularly used to achieve forced induction. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. The RAM VII changed all that. 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 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. Takeoff distance (50) 2,010. In the years following its introduction, the airplane saw few major changes. For 1976 the airplane was equipped with a propeller synchrophaser to control propeller RPM and phase relationship of the blades, engine-to-engine. 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. Home > Aircraft Specs > Manufacturers > Cessna Aircraft > 414 pressurized-turbocharged Performance Information. Initial climb rate 1,700. The more the industry drags out phasing out 100LL, the more susceptible it is to looking unconcerned about public health risks. 5 text-align: center; Another point of consideration for a 414 buyer is the SB/AD on the wing spar. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. Always remember where the wind is coming from and adjust the pattern accordingly. However, there are a number of airworthiness directives (AD) and service bulletins that have been published over the years. The popularity of the aircraft ensures that there are enough aftermarket parts that can be bought if used parts are unavailable. 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 aircraft was labeled the Chancellor in 1976. Its an $800 part. 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. Fuel capacity varies. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. Maximum operating altitude of 30,800, a optimal cruise speed of 203 knots/234 MPH, and a 705 NM/811 SM seats-full range. There are four options, all of which provide a sizable increase in horsepower, increase the TBO, and newer, more powerful propellers. Developed from the 310, it utilizes a similar landing gear and tail unit. 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 According to Cessna, 4.2-psi cabin pressure differential could be maintained by either engine operating at 60 percent power. [2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]. Initial climb rate 1,900. 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. (2005, June 14). Approaching and landing with minimal power is a good habit. Would like to understand why. Range 506- 1,325. 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. 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. The twin turbocharged 310-hp engines provide sea level power to 20,000 feet, while the twin-engine rate of climb is 1,580 fpm, and the single-engine rate is 290 fpm. In 1979, the 402s received a new wing, with a 5 feet (1.5 m) greater span. The takeoff distance is 408 meters while the landing distance is 365 meters. Pay attention to the fuel system in tip-tanked 414s. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads.The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. On the flip side, when fully loaded with eight passengers and baggage, there will be enough space for barely two hours of fuel. The top of the line for the 414 is the series VI. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. Some ADs have called for replacing faulty parts such as a set of vacuum pumps, and bolts on the fork of the main landing gear. Of course, any airplanes safety depends a great deal on the proficiency of its pilots. Improved version CESSNA 414A Chancellor (appeared in 1978) with bonded wet wing, without tip tanks. 130 https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). Most are the basic bucket.. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. One of the most important came in 1973, when cabin length was increased 16 inches and a fifth side window was installed. 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. ft/min, IAS The Cessna 414 Chancellor series gets high marks for its spacious dwelling, generous baggage space and favorable control response. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). The 414 was meant to attract customers looking to upgrade from their unpressurized twin-engined aircraft and did so with limited success. The first Cessna Chancellor - the 414 - took to the skies in 1968, and was produced from 1970 onwards. ft/min, IAS The 414A has an issue with shock cooling of the engine that occurs during rapid descents. Stall mph cabin is separated from the passenger compartment by a divider. Aircraft of similar configuration, age, and role include the Beechcraft Queen Air, AeroCommander 690, Piper Cheyenne, Beechcraft Duke, and the Piper Pa-31 Navajo. 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. 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. ) Quality initial and recurrent training is critical. The model 414, a 411 derivative introduced in 1970, utilized the 421s fuselage and tail unit with the 401s wings. 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. 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. GlobalAir.com is your partner in connecting you with relevant information and resources. This can be a great aircraft and a good buy, but only for a pilot who doesnt need lots of payload. Are COVID Vaccines Injuring Pilots? no data In service since 1969. The Chancellor 414A has an impeccable safety record. By continuing to use this website, you are agreeing to our Cookie Policy. Landing distance (50) 1,765. . Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. A simpler fuel system was among a host of improvements unveiled in 1978 with introduction of the Model 414A Chancellor. I have owned and flown a 1979 Cessna 414A for 14 months, accumulating 235 hours in all sorts of conditions. Thielert claims increased power and improved fuel economy over other available conventional piston engines. Distinguishing features are: retractable landing gear and three-bladed, constant speed, fully feathering propellers. Operating and maintenance costs are attractive when compared with those of competing airplanes, such as the big-brother 421 and Beech Aircrafts Duke. Baggage capacity of the 414 is 930 pounds, and cabin seating is available with an array of executive options. Some low-time pilots might be approved for 340 insurance, but rejected for a 414/414A. fitness for any purpose is made or implied. Over its production run the number of 414s and 414As were evenly split, with 516 and 554 built, respectively. 6,165: 6,165: SOURCE: Sources. 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). RAM also makes winglets and vortex generators. m. All data presented is only indicative and should not be used operationally. Twin engine piston aircraft with retractable landing gear. 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. All aircraft, engines, and components have type certificates that approve their use. Email Seller Video Chat. Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. The 414A has a combined 620 hp (456 kW), however, takeoff acceleration might not be as neck-snapping as one would assume. The Chancellors that cost close to $500,000 most often are pristine and like-new. Each engine spun a constant speed, three-blade McCauley propeller. 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: 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. However, a 414 RAM VI and VII can often have an excellent useful load with an impressive range/payload chart. Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. The RAM IV struggled in the flight levels, especially in the summer. Oh, and the aft toilet. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Distances Balanced Field Length: 2595 ft Landing Distance: 4000 ft Performance Rate of Climb: 1520 fpm Climb Rate One Engine Inop: 290 fpm Max Speed: 235 kts Normal Cruise: 203 kts Power Plant Engines: 2 Engine Mfg: Continental Engine Model: TSIO-520-NB Marketplace Information Interested in buying this aircraft click here! Continental also published overhaul procedures to enable -NB engines to get the TBO boost.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). Retrieved October 5, 2021, from https://www.aopa.org/go-fly/aircraft-and-ownership/aircraft-fact-sheets/cessna-414, Company, S. P. (n.d.). Kudos go to Cessna for rising to the occasion. Cessna 414 Performance & Handling Cited as an excellent IFR platform, you'll 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. 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. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. ft/min, TAS Pilots with less experience can expect this range to rise to between 1,100 to 1,600 per year. The aircraft can seat up to eight passengers and one or two crew. ( Annual inspections, repairs and pre-buys must be conducted by specialists. 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. 310, Range m, MTOW Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. 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. z-index: -1; Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. Providing six seats as standard and an optional seventh, the aircraft appeared to private owners needing a comfortable long-range aircraft and corporate or charter organizations shifting people over short legs. For 1981, Chancellor refinements included a heated fuel manifold, frost panes for cockpit side windows, and threadless-blade propellers. It is an approval granted to a parts manufacturer to manufacture specific aircraft components. The remedy for this was increased visual inspections and the strengthening of the wing spars by adding spar straps. The 401, introduced in 1966 and discontinued in 1972, was basically designed as a medium to . 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. 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. Performance specifications Horsepower: 2 x 375 HP Best Cruise Speed: 241 KIAS Best Range (i): 1,197 NM Fuel Burn @ 75%: 47.0 GPH Stall Speed: 74 KIAS Rate of climb: 1,940 FPM Rate of climb (1 engine out): 350 FPM Ceiling: 30,200 FT Ceiling (1 engine out): 14,900 FT Takeoff distance: 1,786 FT Landing distance: 720 FT Propeller- to-fuselage clearance is more than 31 inches for a very quiet cabin. Power was supplied by two horizontally opposed, six-cylinder, direct-drive, turbocharged, air-cooled, fuel-injected Continental TSIO-520-Js which produced 310 hp (228 kW). 16 Copyright permission must be sought from EUROCONTROL. B. C. (2015, July 13). Of course, any airplanes safety depends a great deal on the proficiency of its pilots. That resulted in cruise speeds of only about 180 to 185 KTAS up high. 200 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. Ball also says that heated windshields should be checked often to ensure there are no cracks. GlobalAir.com is your partner in connecting you with relevant information and resources. Heres an even more interesting thing-normally, the RAM engines want to gulp down 19 to 22 GPH a side at higher power settings. - Send us pictures of your plane. Cruise mph 277. Rate of Climb: 1650 fpm; Climb Rate One Engine Inop: 315 fpm; Max Speed: 243 kts; Normal Cruise: 229 kts . Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. Cessna 414 Stock Airplane vs. RAM Series VII; Primary Specifications Cessna 414 text-align: center; Many of which have been addressed by ADs and service bulletins. Answer:The flaps extend to 45 degreesThe TSIO-520-NBs red-line is 2700 RPM. Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. 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. The Piper Seneca is also quite similar to the 414A, even though it is slightly smaller. fitness for any purpose is made or implied. Best Range: 1106 NM With 1000 pounds of fuel, the payload may be 400 to 600 pounds. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours.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.PERFORMANCE, LOADINGService ceilings are above 30,000 feet, but few owners fly that high. By continuing to use this website, you are agreeing to our Cookie Policy. When discussing 414s and 414As, one must speak correctly. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. 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. A cabin differential of 5.0 psi allows a 10,000-foot cabin at 26,500 feet. Answer: TTAF stands for Total Time Airframe, which refers to the number of flying hours the airframe has accumulated since new. Average price for used aircraft CESSNA 414A is $344,804.81. One former owner even stated that anyone who says the aircraft is reliable is delusional. Also says to increase landing distance by 45% (doesn't seem to make sense). All rights reserved. And $34,235 for fixed costs such as insurance. MEL, in this case, refers to Multi-Engine Land. It's the third model in the Chancellor line and the successor to the Cessna 414II. Finally, the Riley Rocket 414 has two 400hp Lycoming IO-720 engines fitted. 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. It was developed to bridge the gap between the unpressurized Cessna 401 and the pressurized, more powerful Cessna 421. 2023 GlobalAir.com. Chancellors are as roomy as 421B/Cs. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. Training is a must. The new engine also has a TBO of 2,000 hours, which is a 600-hour increase from stock. The 414A, aka Chancellor, was introduced in model year 1978 with the last built in 1985. )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. CESSNA 414A Ram V. Retrieved October 8, 2021, from https://www.aircraftcostcalculator.com/AircraftOperatingCosts/350/Cessna+414A+Ram+V, Continental 520 overhaul cost. 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. Engine and aerodynamic modifications abound for the 414. The CESSNA CITATION LONGITUDE aircraft was designed with your business and return on investment in mind: transatlantic range, advanced engineering and an unforgettable cabin experience all come together with the lowest direct operating costs of any super-midsize jet.

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