The aircraft factors are: These terms are all within the control of the owner. }.tdi_115 .td-element-style{ Of course, any airplanes safety depends a great deal on the proficiency of its pilots. Im required to attend an approved school for recurrent training. - Features that would be useful to you. 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 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. STANDARD DATA: (T310R) Seats 4-6. Thielert claims increased power and improved fuel economy over other available conventional piston engines. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. 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! 1970 - 1977 CESSNA 414 - Specifications, Performance - Planephd 5 CESSNA 340 - Plane & Pilot Magazine When we look at the power loading of the aircraft, the why becomes obvious: weight. It has a take-off distance of 665 meters and a landing distance of 718 meters. The standard aviation insurance all aircraft owners take is liability coverage, while hull coverage is optional. Although you could fly for about 1,100 miles, you would be able to bring only two friends and a few bags. These aircraft were called the 414A Chancellor. In addition to the bare-bones model and the ARC 400-equipped 414AII, there was a III version with ARC 800- and 1000-series avionics, a Bendix RDR 160 weather radar and 100-amp alternators. (Beginning in 1957, horsepower was modestly increased to 230.) Production aircraft were accessible in several optional seating configurations and avionics packages. Cessna 402 - Wikipedia 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/ 811 SMCruise speed:203 knots / 234 MPHAverage price:$344,804.81Number of passengers:7 people, Your email address will not be published. Its an $800 part.MODS, CLUBSAmong the most popular mods are the RAM Aircraft Corporation engine swaps. Cessna 414 - Aviation Consumer In the early 414s, the main landing gear webbing is prone to cracking, requiring extensive rectification. 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. Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. 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. Power was provided by twin 340-hp Continental engines, supercharged with AiResearch exhaust-driven compressors and turning full-feathering constant-speed propellers. Empty wt. 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. Features wing of CESSNA 402 and fuselage of CESSNA 421. Fuel capacity 213-270. airplane of this vintage, only slight trim changes are needed when flaps or landing gear are reconfigured, although single-engine handling, as with any piston twin, is demanding and requires regular practice. The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. These aircraft arent like the 172s. MEL, in this case, refers to Multi-Engine Land. Answer: TBO means Time Between Overhaul, which is the manufacturers recommended running time, in hours or calendar time, before overhaul. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds.In the years following its introduction, the airplane saw few major changes. I have owned a 1979 C414AW (a 414A with RAM winglets) for five years and about 2400 flight hours. Insurance costs have equaled $7000 per year for the last couple of years for $1 million smooth with a hull value of $350,000. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. . Required fields are marked *. Answer: An aircrafts service ceiling is defined as the height at which the aircraft cannot climb at a rate greater than 100 feet per minute. Answer:The flaps extend to 45 degreesThe TSIO-520-NBs red-line is 2700 RPM. Some low-time pilots might be approved for 340 insurance, but rejected for a 414/414A. 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. kts, Distance These can be purchased by Sierra Industries. 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. 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. When we're not in the air, we're here helping others how to join us here at Aviator Insider. CESSNA 310 - Plane & Pilot Magazine 110 kt, Vat (IAS) Derived from the Model 411, the Cessna 401 and 402 are essentially the same aircraft put to two different uses. Winglets aid climb and cruise speeds. Buyers should be looking carefully for compliance. Would like to understand why. Fuel transferred too early is pumped overboard. (n.d.). Initial climb rate 1,900. By continuing to use this website, you are agreeing to our Cookie Policy. The leaking exhaust gases can make the engine rails crack, a component that is extremely expensive to replace. 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: - Its important to note that a 414 is 7 knots slower than its little brother, the 340, which has the same engines and many of the same systems, but a notably smaller cabin. The change allowed the engine to produce 310 hp (228 kW) at 2700 RPM from sea level to 20,000 ft (6,096 m). There are several good training programs available to help keep 414 pilots in top form, something we feel to be quite important as, while the accident rate is low, the accidents seem primarily to occur on amateur flown airplanes and involve judgment errors on the part of the pilot rather than anything wrong with the airplane. The variable costs such as maintenance for the airframe, as well as other costs such as landing and parking fees totaling $206,550. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. 230 In the years following its introduction, the airplane saw few major changes. The 414 is a low-wing cantilever monoplane with a conventional tail section and a retractable tricycle undercarriage. Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. m. All data presented is only indicative and should not be used operationally. Those owners who try to operate an aircraft like the Cessna 414 on a shoestring are pursuing false savings. They are the Cadillacs of the piston line, with attention having been paid to detail; even on an. https://cessnaowner.org/414-chancellor/, estaff. 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. The landing gear is the same as the 414, but the horizontal and vertical stabilizer, elevator and rudder are the same as the 310; minor changes in the 310 tail make it interchangeable with the 340. Ceiling 26,000. Also, the big Cessnas have safety records that are unmatched by any other light twin. Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. ft/min, IAS kts, ROC NM, ROD It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. Liability coverage covers damage caused by the aircraft, including passengers, while hull coverage covers damage to the aircraft itself. no data 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. Cessna 414A Private Jet Charter - Paramount Business Jets In 1973 Cessna stretched the fuselage by 16 inches and added a fifth side window. Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. The 414 seats up to 6 passengers plus 1 pilot. There are four options, all of which provide a sizable increase in horsepower, increase the TBO, and newer, more powerful propellers. The takeoff distance is 408 meters while the landing distance is 365 meters. Please send us your experiences on your aircraft. Cessna 414 chancellor. 1000 [2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]. We highly recommend them. Oh, and the aft toilet. Range 489-1,242. Given the popularity of the 414 series, its fair to say that if you need a modification, you can find it. 4,640. It uses spent exhaust gases to run the compressor, which draws in and compresses clean air to deliver to the engine. Many of which have been addressed by ADs and service bulletins. PERFORMANCE: Top mph 273. Sure, many have been plowed up for houses or 2023 Aviation Publishing Group. Four years later, Continental incorporated some changes to the -NBs cylinders, valve lifters and piston pins, and increased the engines recommended TBO from 1400 to 1600 hours. The crosswind characteristics are good, and its easy to make squeaker landings. You Tell Us, EAA To Host Webinar Event For Aspiring Aviators, National Museum Of The U.S. Air Force Celebrates 100 Years, FAA IACRA System Hit With Database Issues, FAA Nominee Quizzed On Aviation Knowledge, General Aviation Accident Bulletin, February 27, 2023, Pratt & Whitney Canada Passes One Billion Flight-Hour Milestone, AeroLEDs Introduces New Landing Light Series, Universal Avionics Receives TSO Approval For Aperture, MyGoFlights Head-Up Display Division Sold To Partner, AeroBrigham. Initial climb rate 1,700. The factory tends to be much pricier than third-party garages that overhaul your engine. 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. The remedy for this was increased visual inspections and the strengthening of the wing spars by adding spar straps. Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: Takeoff distance (50) 2,220. Come join us! The popularity of the aircraft ensures that there are enough aftermarket parts that can be bought if used parts are unavailable. 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. 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. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. The new design used the same fuselage and tail as the 421 and the wing from the 402. The Cessna 340 is a pressurized six-place twin featuring center-aisle seating, an air-stair door, and top cruise performance. 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. Go figure. . Also, the big Cessnas have safety records that are unmatched by any other light twin./* custom css */ The 1973 to 1977s are the long bodies. I use SimCom. 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. The 340 has a gross weight of 5,975 pounds, and an empty weight of 3,697 pounds. 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. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. 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. Cessna 340 Specifications, Cabin Dimensions, Performance - GlobalAir.com 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. 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. 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. 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. The piping which directs the exhaust from the manifold to the turbo is also susceptible to cracking. Another great resource is the Cessna Pilots Association, it offers a monthly magazine, forums, technical information, and even training. Gross wt. The Piper Seneca is also quite similar to the 414A, even though it is slightly smaller. Landing distance (50) 2,393. The 375-HP 421Cs single engine ceiling is 14,900 feet. The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks. Frequently, a a buyer makes assumptions that arent correct. Three significant milestones in 414 development took place in 1973, 1976, and 1979. 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. 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. CESSNA 414 Aircraft For Sale - 33 Listings | Controller.com There are several problems that the 414A has. Special Missions. The efficiency of the 414As long high-aspect ratio wing is highlighted by noting the 414As single-engine service ceiling is 19,850 feet. For a private pilot with 1,500 hours total time, an IFR/MEL rating, 500 hours on multi-engined aircraft, and 25 hours on type, the 2021 cost per year for US$1,000,000 liability coverage is in the range of US$850 to US$1,400 per year. One former owner even stated that anyone who says the aircraft is reliable is delusional. Real world speeds depend on engine configuration, but owners typically report 200 kts at about 38 gph in the upper teens. - Send us pictures of your plane. 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. As has often been said, Cessna really got it right with the 414/414As. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. Pressurization happens in the engine, where hot air is compressed and then directed to the cabin. . Built-in airline-like stairs are in the door. There are only two fuel-. Model 414 seats up to 7 passengers and 1 pilot. 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! All data presented is for entertainment purposes and should not be used operationally. With the same fuselage as the 421, the 414 was roomy with huge baggage space. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. margin: 0 auto 0 0; Beginning in 1978, Cessna offered three basic equipment packages. 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. Training is a must. Cessna 206 Specifications, Cabin Dimensions, Performance - GlobalAir.com 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. Fuel cost per hour: 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. An STC is an approved modification to an aircraft, engine, or component. 16 Send feedback comments to the EUROCONTROL Training Institute. The 414A has a single-engine ceiling of 19,850 ft (6,050 m) which is the best among all its peers. 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. 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 exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. By. If followed carefully, a mechanic wont miss anything. Many supplemental type certificates exist for the aircraft that allow upgrades to improve performance. However, there seem to be plenty that are not. Service ceilings are above 30,000 feet, but few owners fly that high. The greater the experience of the owner/pilot, the lower the premiums. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. Initial climbout increased by at least 200 FPM to more than 1000 FPM. The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. Description No warranty of Approaching and landing with minimal power is a good habit. Each model has different after-market engine/prop conversions and when other performance-enhancing modifications are factored in, weights and other performance criteria vary. Federal Register. 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. 100 Some potties have a flushing feature. 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. 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. Utility twin aircraft. BUILT FOR TRAINING Ideal for entry-level landings, the Skyhawk piston features a sturdy tricycle landing system and a resilient airframe. The switch for that light is on the underside of a Tee fitting in the pressure line to the tail and thus fills with water, rust and crud and should be pulled and cleaned periodically, or it will fail. Cessna 180 Skywagon: Legendary popularity - AOPA A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup.