document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Your email address will not be published. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. Answer: An STC refers to a Supplemental Type Certificate. Please send us your experiences on your aircraft. Answer: Maximum structural cruise, or Vno, refers to the airspeed above which the aircraft should be flown only in smooth air. - Features that would be useful to you. The basic 414 was born in 1970 with a 4.2 psi pressurization differential and ascended to become the Chancellor in 1978. https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds.In the years following its introduction, the airplane saw few major changes. To better manage fuel, a fuel computer was added to the list of available options. The original 414 aircraft retailed at US$138,000 in 1970. 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. It's also a myth. 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. . 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. 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. 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. These can be purchased by Sierra Industries. Speed brakes/spoilers are available from PowerPac Spoilers (www.powerpacspoilers.com) and more advanced intercoolers come from American Aviation (www.americanaviationinc.com). 5,500. Power. There are only two fuel-. Ball also says that heated windshields should be checked often to ensure there are no cracks. Retrieved October 5, 2021, from https://www.globalair.com/aircraft-for-sale/Specifications?specid=971. Landing distance (50) 1,815. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. 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! One of the most important came in 1973, when . Landing distance over 50-ft obstacle: 2,393 ft: Landing distance, ground roll: 1,013 ft: Limiting and . m. All data presented is only indicative and should not be used operationally. 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. 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. 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. Home > Aircraft Specs > Manufacturers > Cessna Aircraft > 414 pressurized-turbocharged Performance Information. 200 CESSNA, V2 (IAS) kts, ROC Landing Distance: 4000 ft; Performance. The variable costs such as maintenance for the airframe, as well as other costs such as landing and parking fees totaling $206,550. Also says to increase landing distance by 45% (doesn't seem to make sense). Down low under 10,000 feet, things are much slower, more like 170 to 175 KTAS. Baggage capacity of the 414 is 930 pounds, and cabin seating is available with an array of executive options. All rights reserved. Cruise mph 223. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); WORLD'S PREMIER INDEPENDENT AVIATION NEWS RESOURCE. One of the biggest weak points of the 414A is the problematic Continental TSIO-520-NB engine. Empty wt. After the Chancellor debuted, there were few further refinements. (n.d.). Refreshment centers can be aft or a vertical unit positioned behind the pilot or copilot seat. Service ceilings are above 30,000 feet, but few owners fly that high. Initial climb rate 1,610. Another great resource is the Cessna Pilots Association, it offers a monthly magazine, forums, technical information, and even training. The takeoff distance is 408 meters while the landing distance is 365 meters. With 1000 pounds of fuel, the payload may be 400 to 600 pounds. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. It featured major modifications, including a restructured and increased wingspan, incorporating integral fuel tanks, and a stretched nose to allow more space for baggage. According to BWI Fly, for liability coverage of $1,000,000, a qualified pilot of a 414A who aims to use the aircraft for private use can expect to pay around $840 $1,400 per year and $4,400 $5,800 per year for a combination of the liability and hull coverage of $225,000. The standard aviation insurance all aircraft owners take is liability coverage, while hull coverage is optional. Many of which have been addressed by ADs and service bulletins. Also, the big Cessnas have safety records that are unmatched by any other light twin./* custom css */ Features wing of CESSNA 402 and fuselage of CESSNA 421. GlobalAir.com is your partner in connecting you with relevant information and resources. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. It uses spent exhaust gases to run the compressor, which draws in and compresses clean air to deliver to the engine. It is a very stable instrument platform and I find it as easy to land as the T310 or any of the large singles Ive flown. )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. Their parts may seem expensive, but they continue supporting us owners, and for that I am very willing to see them earn afair profit. Answer: Wing loading is the total aircraft mass divided by its wing area. Currently, David flies twin retractables, notably the Pa44 Seminole and Pa30 Twin Comanche. 6,500. Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. One of the most distressing issues the Cessna 414A has is cracking along the forward wing spars. The average price for a used Cessna 414 at the time of print was US$230,000, having approximately 6,000 hours total time airframe (TTAF) and engine times of around 800 hours. For the Cessna 414A Chancellor, average pricing was US$280,000, having approximately 7,500 hours total time airframe (TTAF) and mid-life engines. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. When it comes time to overhaul the engine, the cylinders might have to be replaced, and a new set of Continental brand cylinders cost roughly $5,000 depending on the supplier, whereas an off-brand set costs around $2,000. All rights reserved. EASY ACCESS Two large cabin doors allow for convenient entry and loading for student and instructor. 310, Range 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. 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. Initial climb rate 1,900. The aircraft got heavier, with the MTOW and landing weight increasing by 400 lbs (181 kg) and 550 lbs (249 kg), respectively. The airplanes bonded wet wing is 4-1/2 feet longer than previous models and lifts an airframe that is 2 feet 8 inches longer from nose to tail. By. Crew-6 Launch Scrubbed For Ground Systems Issue, The Drip, Drip Of Bad Publicity About 100LL. The top of the line for the 414 is the series VI. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. 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. }@media (max-width: 767px) { 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. Come join us! Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: I own a 1978 Cessna 414A which I acquired in 1989. The Cessna Pilots Association, located at www.cessna.org, and the Twin Cessna Flyer, at www.twincessna.org. We highly recommend them. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Takeoff distance (50) 2,175. NM, ROD It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. 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. The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. This has made insuring a 414 tougher. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. Stall mph cabin is separated from the passenger compartment by a divider. Replacing the cylinder heads requires money and time, which will increase your engine overhaul costs by $6,000 bringing your grand total to $39,000. 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. By all accounts, vortex generators reduce Vmc and stall speeds. Owners speak of the 414s smoothness, stability, and ease with which you can trim the aircraft out. 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. The name Chancellor was used for models marketed from 1976. In the years following its introduction, the airplane saw few major changes. Required fields are marked *. Aircraft of similar configuration, age, and role include the Beechcraft Queen Air, AeroCommander 690, Piper Cheyenne, Beechcraft Duke, and the Piper Pa-31 Navajo. Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. 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. 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. Its wings are borrowed from the Model 414. Takeoff distance (50) 2,220. However, almost all owners complain about the maintenance, and most say that the low acquisition cost of the aircraft will be offset by the cost of maintenance a few years down the line. It's the third model in the Chancellor line and the successor to the Cessna 414II. Answer:The flaps extend to 45 degreesThe TSIO-520-NBs red-line is 2700 RPM. Improved version CESSNA 414A Chancellor (appeared in 1978) with bonded wet wing, without tip tanks. For 1976 the airplane was equipped with a propeller synchrophaser to control propeller RPM and phase relationship of the blades, engine-to-engine. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. Its an $800 part.MODS, CLUBSAmong the most popular mods are the RAM Aircraft Corporation engine swaps. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. Fuel transferred too early is pumped overboard. ft/min, IAS 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. I am a professional aircraft broker who specializes in Twin Cessnas. Top mentions include the true cabin class, reasonable cruise speed, and maintenance of sea-level pressure to 10,000 feet. Specs, range, speed, operating weights and performance for the Cessna 340 here . ) The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Pilots with less experience can expect this range to rise to between 1,100 to 1,600 per year. The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. m, MTOW With its bigger nose and lockers, the 414A can carry 1500 pounds. The Chancellor is a popular aircraft, so it has an extensive range of aftermarket parts and modifications. To ensure the aircraft you are buying is airworthy and will be reliable in the future, spend a bit more on an in-depth inspection. kg, IAS Also, corrosion on the engine frame rails is possible from exhaust leaks where the manifold exits into the turbocharger. He was a glider pilot for several years before obtaining his private license in taildraggers. 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. One former owner even stated that anyone who says the aircraft is reliable is delusional. The turbocharger is connected to both the exhaust and intake manifolds of the engine. Finally, in 1979 the -NB series TSIO-520 engines were installed, providing an improved crankshaft, and in time, an increased engine TBO of 1600 hours against the -Ns 1400. [4] This involves the installation of FADEC-controlled aviation diesel piston engines that run on commonly available jet fuel. Flight planning or any other aircraft operations should only be done using official technical information provided 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! margin: 0 auto 0 0; By continuing to use this website, you are agreeing to our Cookie Policy. Distinguishing features are: retractable landing gear and three-bladed, constant speed, fully feathering propellers. The Cessna 411, first delivered in 1965, was one of Wichitas first ventures into the airliner market. If followed carefully, a mechanic wont miss anything. (RVSM rules have generally limited 414s to 28,000 feet.) The Cessna 180 Skywagon is not a beautiful airplane, but it is a classic-looking taildragger that became an . 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.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. Production aircraft were accessible in several optional seating configurations and avionics packages. 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.