5,500. Although the 414s have a huge cabin-class interior, the stock airplane has never been a tremendous load hauler. 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 Buyers should be looking carefully for compliance. The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. Approaching and landing with minimal power is a good habit. Home > Aircraft Specs > Manufacturers > Cessna Aircraft > 414 pressurized-turbocharged Performance Information. Remained in production until 1985. 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. The longer fuselage now allowed for an eighth seat to be added as an option. kt, Ceiling While bad quality procedures in Wichita back in 1979 had probably caused my problem, the current staff at Cessna really impressed me with their efforts to help save this 27-year-old ship. Built-in airline-like stairs are in the door. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. One pilot and typical 6 passengers in main cabin. text-align: center; Cessna 414 for sale - Specs and History - ADN - FindAircraft.com 130 - Aircraft specific reviews and articles. Answer: IFR means Instrument Flight Rules. 414 Prospective Owners - twincessna.org (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. An engine rail replacement can cost an eye-watering $14,000. Operating and maintenance costs are attractive when compared with those of competing airplanes, such as the big-brother 421 and Beech Aircrafts Duke.In a study of accident records some years ago, the 414 stood out as the safest light twin. Production aircraft were accessible in several optional seating configurations and avionics packages. Description Engine and aerodynamic modifications abound for the 414. Go figure. Over its production run the number of 414s and 414As were evenly split, with 516 and 554 built, respectively. 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. Precise Flight and Spoilers, I. 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. Distinguishing features are: retractable landing gear and three-bladed, constant speed, fully feathering propellers. Cessna 414 pressurized-turbocharged - Performance Data . The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. ft/min, IAS Winglets aid climb and cruise speeds. Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. 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 change allowed the engine to produce 310 hp (228 kW) at 2700 RPM from sea level to 20,000 ft (6,096 m). Derived from the Model 411, the Cessna 401 and 402 are essentially the same aircraft put to two different uses. All rights reserved. All rights reserved. The owners of Cessna 414As have mixed reviews. Initial climb rate 1,610. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. MEL, in this case, refers to Multi-Engine Land. 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 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. 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. In addition, the Chancellors wet wing has an increased fuel capacity of 106 gallons of usable fuel. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. Aircraft of similar configuration, age, and role include the Beechcraft Queen Air, AeroCommander 690, Piper Cheyenne, Beechcraft Duke, and the Piper Pa-31 Navajo. 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. The RAM IV struggled in the flight levels, especially in the summer. Bringing the grand annual total to $240,785. The Cessna 414 is a high-performance aircraft requiring regular and comprehensive maintenance, and if looked after and regularly updated, the aircraft will hold its own on resale. Bombardier Challenger 350 Guide and Specs: Is It Up to the Challenge? The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. 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 Fuselage strakes improve yaw control, performance in turbulence, and a higher cruise speed. Ceiling 26,000. Stall mph 79. A $153,750.00 loan over 10 years including $640.62 per month in interest equates to a $7,709.60 per-month payment. Cessna 414 Chancellor - Price, Specs, Photo Gallery, History - Aero Corner For 1976 the airplane was equipped with a propeller synchrophaser to control propeller RPM and phase relationship of the blades, engine-to-engine. Speed brakes/spoilers are available from PowerPac Spoilers (www.powerpacspoilers.com) and more advanced intercoolers come from American Aviation (www.americanaviationinc.com). Specs, range, speed, operating weights and performance for the Cessna 340 here. }.tdi_115 .td-element-style{ Fuel transferred too early is pumped overboard. 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: - Finally, the Riley Rocket 414 has two 400hp Lycoming IO-720 engines fitted. Interested in buying this aircraft click here. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor. With the O&N tanks in both nacelles, I can carry up to 260 gallons of fuel, good for over seven hours of endurance. Propeller- to-fuselage clearance is more than 31 inches for a very quiet cabin. To better manage fuel, a fuel computer was added to the list of available options. The variable costs such as maintenance for the airframe, as well as other costs such as landing and parking fees totaling $206,550. A typically equipped 414A has a full-fuel payload of about 500 to 700 pounds, depending on equipment. Some potties have a flushing feature. The fuselage and tail were essentially the same as the ones used on the 421B, while the wings were taken from the 401. 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. Deserving of Respect and Praise: Cessna's 421C 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. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). 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. }.tdi_115.td-a-rec-img img{ Pressurization happens in the engine, where hot air is compressed and then directed to the cabin. The exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. In 1978, an enhanced version was launched, designated as the 414A Chancellor. 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. What a difference! It's also a myth. Otherwise, the periodicity is 1,600, or 200 hours depending on the mod state. Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. 2023 GlobalAir.com. Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. 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. The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Your email address will not be published. Initial climb rate 1,700. 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. 6,165: 6,165: SOURCE: Sources. Answer: Wing loading is the total aircraft mass divided by its wing area. Sure, many have been plowed up for houses or 2023 Aviation Publishing Group. No warranty of 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: Plane and Pilot expands upon the vast base of knowledge and experience from aviations most reputable influencers to inspire, educate, entertain and inform. Come join us! However, a 414 RAM VI and VII can often have an excellent useful load with an impressive range/payload chart. (See page 25 for an abbreviated AD list.). Four variations are available, all of which offer a boost in useful load, increased TBOs and new props. The engine is chock-full of new RAM components such as camshafts, cylinders, crankshaft, piston rods. m. All data presented is only indicative and should not be used operationally. With its bigger nose and lockers, the 414A can carry 1500 pounds. Six seats were standard; a seventh was available as an option. The 421B tiptank twin Cessna has fuel carried in the mains (tips), auxiliary fuel cells in the wings and optional nacelle tanks. They are the Cadillacs of the piston line, with attention having been paid to detail; even on an. 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. We are a collective group of airline instructors, and pilots dedicated to all things aviation. 1100 Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. Landing distance (50) 1,765. . 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. Six seats were standard; a seventh was available as an option. 200 Stall mph 81. Ownership and operating costs. The 414 was meant to attract customers looking to upgrade from their unpressurized twin-engined aircraft and did so with limited success. The package that gives the 414A the most significant boost in performance is the series V upgrade. )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. Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. Phone: (305) 342-0760. With rare exception, all 414As have an aft potty. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. 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. The Chancellor utilizes the hydraulic components of the Golden Eagle gear and features a five-second retraction time. If an owner has taken a maintenance only as required approach to their aircraft, they can expect a far lower resale value. The big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte. The main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. In a study of accident records some years ago, the 414 stood out as the safest light twin. 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. I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. Fuel cost per hour: 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. 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. 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. 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. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. Handling, range, speed and fuel economy, and hourly costs are often considered to be at or exceeding the industry standard. fitness for any purpose is made or implied. But the average price of a 414A is around $300,000, while the price range is between $200,00 $500,000. VGs are also available from Micro Aerodynamics (www.microaero.com) and V/G Systems, phone 800-328-4629. If followed carefully, a mechanic wont miss anything. Landing distance (50) 1,850. Gross wt. 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. Fuel transferred too early is pumped overboard. Purchasing a Cessna 414A is considered to be cheap for the number of airplanes you get. [4] This involves the installation of FADEC-controlled aviation diesel piston engines that run on commonly available jet fuel. 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. Its an $800 part. Ram also claims youll see an extra 5 takeoff manifold pressure, a 1900 fpm climb, 13 knots extra cruise speed, and a 415lb increase in useful load. 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. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. As we saw earlier, average prices sit between US$230,000 to US$280,000, yet highly modified and maintained aircraft command twice those figures. Answer: The process of delivering compressed, denser air to a combustion engine is referred to as forced induction. The 414 and 414A truly provide a great family or business aircraft. 100 However, there seem to be plenty that are not. GlobalAir.com is your partner in connecting you with relevant information and resources. Eight aircraft factors influence 414 resale plus many other economic factors. Seating is spacious and available in a variety of arrangements. Three significant milestones in 414 development took place in 1973, 1976, and 1979. Come join us! Cessna 414 Guide and Specs : Is It High Performance? This has made insuring a 414 tougher. By continuing to use this website, you are agreeing to our Cookie Policy. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. The compressed air is then cooled down, which makes it denser, on its way to the cabin. 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. I bought it to replace a nice Cessna T310R, which I flew for about a year. These aircraft arent like the 172s. In service since 1969. A cabin differential of 5.0 psi allows a 10,000-foot cabin at 26,500 feet. When we're not in the air, we're here helping others how to join us here at Aviator Insider. Cessna 414A Private Jet Charter - Paramount Business Jets The 414A, aka Chancellor, was introduced in model year 1978 with the last built in 1985. Distances Balanced Field Length: 1780 ft Landing Distance: 2358 ft Performance Rate of Climb: 920 fpm Max Speed: 156 kts Normal Cruise: 147 kts Economy Cruise: 117 kts Cost per Hour: $ 220.95 Power Plant Engines: 1 Engine Mfg: Continental Engine Model: IO-520-F Marketplace Information Interested in buying this aircraft click here!
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