With full tanks-enough fuel for nearly 4.5 hours with IFR reserves-a well-equipped Chancellor will have room left in its weight-and-balance envelope to accommodate six FAA-standard people with their toothbrushes. Even with the company is getting its feet wet in piston products again, there are no immediate plans to make any cabin-class piston twins to replace those being retired. Become a member and get exclusive access to articles, contests and more! I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. The Cessna 414 Chancellor series gets high marks for its spacious dwelling, generous baggage space and favorable control response. However, as aircraft age, they dont get cheaper to own or operate, which the price will reflect. The prototype, registered N7170C, first flew on 1 November 1968, and production aircraft were available in a number of optional seating arrangements and avionics packages. Approaching and landing with minimal power is a good habit. All rights reserved. The more generic components such as filters, wheels, tires, and brakes are off the shelf and stocked by large aviation suppliers like Aircraft Spruce & Specialty or Wag Aero. The Chancellor is a popular aircraft, so it has an extensive range of aftermarket parts and modifications. A brand new engine exchange from Continental costs an average of $60,000. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. 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. Once it reaches the cabin it is compressed enough to create an atmospheric pressure that mimics the desired altitude. 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 To get at the fuel in the wing locker tanks, it must first be transferred to the mains. The aircraft was labeled the Chancellor in 1976. fitness for any purpose is made or implied. If youre one of the lucky owners who have to overhaul their engine without replacing the cylinder heads, a shop will only charge an average of $33,000 nearly half of what the factory charges. 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. The displacement and power output remained the same, but the manifold pressure was increased from 36 hPa to 38 hPa. PERFORMANCE: Top mph 268. text-align: center; Buyers should be looking carefully for compliance. By continuing to use this website, you are agreeing to our Cookie Policy. - Aircraft data that you believe is inaccurate or have specific experiences. Cowl flaps can be fully closed for cruise on even ISO +30 degrees F days, while the cylinders rarely go much over 400 degrees F. At full gross takeoff weight, I see normal 69 percent power cruise speeds in the 195 to 205 KTAS range in the flight levels. The more the industry drags out phasing out 100LL, the more susceptible it is to looking unconcerned about public health risks. Optional auxiliary and locker tanks were available to boost usable capacity to 180 gallons, then to 203 gallons in 1973. Home > Aircraft Specs > Manufacturers > Cessna Aircraft > 414 pressurized-turbocharged Performance Information. This plane was. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. The model 414, a 411 derivative introduced in 1970, utilized the 421s fuselage and tail unit with the 401s wings. 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. 1000 The first Cessna Chancellor the 414 took to the skies in 1968, and was produced from 1970 onwards. Its an $800 part.MODS, CLUBSAmong the most popular mods are the RAM Aircraft Corporation engine swaps. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. 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 pilot in a hurry will see 205 knots on 38 GPH at 75 percent power rich of peak, although few operate that way anymore. (RVSM rules have generally limited 414s to 28,000 feet.) ( After the Chancellor debuted, there were few further refinements. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. With a range of approximately 2,200 nautical miles and a relative low cost, the Conquest II was an unparalleled aircraft in its time. This has made insuring a 414 tougher. The factory tends to be much pricier than third-party garages that overhaul your engine. It has a take-off distance of 665 meters and a landing distance of 718 meters. Handling, range, speed and fuel economy, and hourly costs are often considered to be at or exceeding the industry standard. 3,865. Cessna 195 Guide and Specs : All About The 195 Businessliner, Bombardier Challenger 300 Guide and Specs, Installed equipment, specially avionic fit-out. The top of the line for the 414 is the series VI. 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. All rights reserved. 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. 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. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. 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. 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. 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. Would like to understand why. STOL kits can also be purchased to help reduce the field length of the aircraft. 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. Six seats were standard; a seventh was available as an option. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. In the years following its introduction, the airplane saw few major changes. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. Six seats were standard; a seventh was available as an option. The new engine also has a TBO of 2,000 hours, which is a 600-hour increase from stock. 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. Training is a must. Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. Accident statistics suggest that no common threads are pointing to the system or design problems on the 414. 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 CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. Cessna Country: United States Manufactured: 1972 to: 1984 ICAO: C340 Price: US$.36 million (1982) Performance Weights Dimensions Avionics: Garmin G500 PFD Engine: 2x Continental TSIO-520-NB Piston Power: 310 horsepower Max Cruise Speed: 244 knots 452 Km/h Approach Speed (Vref): 71 knots Travel range: 1,406 Nautical Miles 2,604 Kilometers Engines two 340-hp turbocharged Continentals. If you opt to go for a rebuilt engine from Continental will save you $6,000, for a total price of $54,000. As far as handling goes, owners have reported that it is a stable aircraft that behaves in a very neutral manner and reacts to control inputs predictably. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. 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. Pricing No warranty of Landing distance (50) 1,850. With the O&N tanks in both nacelles, I can carry up to 260 gallons of fuel, good for over seven hours of endurance. However, there seem to be plenty that are not. Landing distance (50) 1,815. 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: They are the Cadillacs of the piston line, with attention having been paid to detail; even on an. The 414A can be upgraded with the usual performance boosters such as vortex generators, which are highly recommended. kt, Vat (IAS) To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). 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! 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. 2023 GlobalAir.com. ft/min, IAS Bombardier Challenger 350 Guide and Specs: Is It Up to the Challenge? Its an $800 part. Cessna Country: United States Manufactured: 1961 to: 1985 ICAO: C185 Price: US$.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: It featured major modifications, including a restructured and increased wingspan, incorporating integral fuel tanks, and a stretched nose to allow more space for baggage.