2023 GlobalAir.com. 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. Given the popularity of the 414 series, its fair to say that if you need a modification, you can find it. Developed from the 310, it utilizes a similar landing gear and tail unit. After the Chancellor debuted, there were few further refinements. ft/min, ROC There were significant changes made to the body of Chancellor 414A as well. by the manufacturer or FAA. Maintenance costs vary from year to year, but $300 to $350 direct per hour is a good estimate for the 125 to 150 hours per year I fly. .tdi_115.td-a-rec{ Winglets aid climb and cruise speeds. The aircraft factors are: These terms are all within the control of the owner. Most are the basic bucket.. z-index: -1; A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. In 1973 Cessna stretched the fuselage by 16 inches and added a fifth side window. Answer: TTAF stands for Total Time Airframe, which refers to the number of flying hours the airframe has accumulated since new. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Among the most popular mods are the RAM Aircraft Corporation engine swaps. kt, MCS David is a seasoned pilot and aviation expert. Landing distance (50) 1,850. ) text-align: left; All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. Ball also says that heated windshields should be checked often to ensure there are no cracks. Sure, many have been plowed up for houses or 2023 Aviation Publishing Group. 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. The 401, introduced in 1966 and discontinued in 1972, was basically designed as a medium to . Gross wt. Owners speak of the 414s smoothness, stability, and ease with which you can trim the aircraft out. Aircraft of similar configuration, age, and role include the Beechcraft Queen Air, AeroCommander 690, Piper Cheyenne, Beechcraft Duke, and the Piper Pa-31 Navajo. When pilots are flying IFR, it means they are under the control of Air Traffic Control. (See www.ramaircraft.com.). 130 The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. 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. Fuelburn: 34.0 GPH Arguably the most popular engine mod youll see on used aircraft is the engine upgrade to 335 hp offered by Ram Aircraft atwww.ramaircraft.com. Ive previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. Power was provided by twin 340-hp Continental engines, supercharged with AiResearch exhaust-driven compressors and turning full-feathering constant-speed propellers. 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). Fuel capacity 102-207. 6,500. Find more About Us here! Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. Would like to understand why. 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. kg, IAS The landing gear was replaced, using the simpler system from the Cessna 414. In 1973, an updated 414 was released with major changes, this model was named the 414II. The STANDARD DATA: Seats 6-8. We are a collective group of airline instructors, and pilots dedicated to all things aviation. Their parts may seem expensive, but they continue supporting us owners, and for that I am very willing to see them earn afair profit. Loading must be watched carefully to avoid going out of the rear CG limit. This means the aircraft will burn around 17 gph (64 lph) per engine at 65% power and FL250, which is enough to get you cruising at around 202 KTAS (232 mph / 374 kmph). 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 (Beginning in 1957, horsepower was modestly increased to 230.) [2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]. One club offers extensive support for the 414, in addition to all other twin Cessnas. In my Cessna 152, a 20-knot headwind increases the glide angle from 5 degrees to 7.5 degrees, a 50-percent increase. So newer, more powerful engines with stronger components and increased aerodynamics all of which boost performance greatly and increase the value. The takeoff distance is 408 meters while the landing distance is 365 meters. In 1978, an enhanced version was launched, designated as the 414A Chancellor. Given the age and systems on the 414, plenty of airworthiness directives need reviewing for compliance. There are only two fuel-288quantity indicators, both with three-position switches, to help the pilot keep track. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor. I bought it to replace a nice Cessna T310R, which I flew for about a year. Another area that needs to be checked for corrosion is the firewall. ft/min, IAS The package that gives the 414A the most significant boost in performance is the series V upgrade. Description Smart design means a better ride. These aircraft were called the 414 Chancellor. In the years following its introduction, the airplane saw few major changes. 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. quantity indicators, both with three-position switches, to help the pilot keep track. 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. 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 RAM VII changed all that. When discussing 414s and 414As, one must speak correctly. It was developed to bridge the gap between the unpressurized Cessna 401 and the pressurized, more powerful Cessna 421. The 414A has a single-engine ceiling of 19,850 ft (6,050 m) which is the best among all its peers. The aircraft is powered by two Continental TSIO-520-NB piston engines. Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. The main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. Answer: The process of delivering compressed, denser air to a combustion engine is referred to as forced induction. kt, Ceiling 2023 GlobalAir.com. The 411A, produced from 1967-68, featured a redesigned nose and more baggage space. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Checking the Cessna 152 POH it says to increase takeoff distance by 15% of ground roll (makes sense due to increased friction). Description }.tdi_115 .td-element-style{ 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. Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg. Speed brakes/spoilers are available from PowerPac Spoilers (www.powerpacspoilers.com) and more advanced intercoolers come from American Aviation (www.americanaviationinc.com). Ceiling 29,800. Soaring Good Looks. kts, ROC Handling, range, speed and fuel economy, and hourly costs are often considered to be at or exceeding the industry standard. I am a professional aircraft broker who specializes in Twin Cessnas. The aircraft can seat up to eight passengers and one or two crew. 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. Aerodynamic mods include vortex generators to increase aileron and rudder control authority at low speeds. With the O&N tanks in both nacelles, I can carry up to 260 gallons of fuel, good for over seven hours of endurance. Cessna 414 Stock Airplane vs. RAM Series IV; Primary Specifications Cessna 414 RAM 325 hp Series IV; Engine Model: Continental - TSIO-520-J-NB: Horsepower: 310: 325: . 414 chancellor. The pressurization and turbocharged nature of the aircraft mean it is complicated to work on, and specialization is needed. The piping which directs the exhaust from the manifold to the turbo is also susceptible to cracking. I have owned and flown a 1979 Cessna 414A for 14 months, accumulating 235 hours in all sorts of conditions. 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. Range 489-1,242. 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. Twin engine piston aircraft with retractable landing gear. kts, Distance 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. 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. 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. Common are engine and aerodynamic modifications, including winglets. Cessna borrowed components from existing 400-series airplanes to come out in 1970 with a model to bridge the price gap between unpressurized and pressurized twins. The fuselage and tail were essentially the same as the ones used on the 421B, while the wings were taken from the 401. 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. When we're not in the air, we're here helping others how to join us here at Aviator Insider. The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. }@media (max-width: 767px) { Refreshment centers can be aft or a vertical unit positioned behind the pilot or copilot seat. Bringing the grand annual total to $240,785. He received his training at the University of North Dakota and has been in love with aviation for many years. Otherwise, the periodicity is 1,600, or 200 hours depending on the mod state. By. All aircraft, engines, and components have type certificates that approve their use. GlobalAir.com is your partner in connecting you with relevant information and resources. It uses spent exhaust gases to run the compressor, which draws in and compresses clean air to deliver to the engine. The 414A, aka Chancellor, was introduced in model year 1978 with the last built in 1985. 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 engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. Heres an even more interesting thing-normally, the RAM engines want to gulp down 19 to 22 GPH a side at higher power settings. An engine rail replacement can cost an eye-watering $14,000. (RVSM rules have generally limited 414s to 28,000 feet.) Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. 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. Continental also published overhaul procedures to enable -NB engines to get the TBO boost. The crosswind characteristics are good, and its easy to make squeaker landings. All rights reserved. General characteristics Crew: one or two Capacity: four to six Length: 36 ft 4 12 in (11.09 m) Wingspan: 44 ft 1 12 in (13.45 m) Height: 11 ft 5 12 in (3.49 m) Wing area: 225.8 sq ft (20.98 m 2) Empty weight: 4,368 lb (1,981 kg) Max takeoff weight: 6,750 lb (3,062 kg) Fuel capacity: 213 US gal (177 imp gal; 810 L) usable https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). The standard aviation insurance all aircraft owners take is liability coverage, while hull coverage is optional. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. 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. 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. Kudos go to Cessna for rising to the occasion. It has a range of 1,328 nautical miles and a climb rate of 1,520 feet per minute. Those owners who try to operate an aircraft like the Cessna 414 on a shoestring are pursuing false savings. Average price for used aircraft CESSNA 414A is $344,804.81. Fuel cost per hour: Top mentions include the true cabin class, reasonable cruise speed, and maintenance of sea-level pressure to 10,000 feet. Once it reaches the cabin it is compressed enough to create an atmospheric pressure that mimics the desired altitude. The most significant and popular modifications that can be made to a 414A are the engine swaps by the RAM Aircraft Corporation. Range 1,284. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. 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.HISTORYCessna borrowed components from existing 400-series airplanes to come out in 1970 with a model to bridge the price gap between unpressurized and pressurized twins. The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. The prices range from low-hour models with less than 4,000 hours TTAF, which are selling for just over US$385,000, while older aircraft from the early-1970s will sell for approximately US$150,000. Initial climb rate 1,610. Full fuel allows the Chancellor 414A to fly for roughly four and a half hours, IFR reserves included, and has enough load leftover to carry six standard passengers, and not a pound more. Preferred Airparts, based in Ohio, provide worldwide customers with surplus new Cessna original components and used parts from dismantled aircraft. Stall mph 82. Training is a must. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. This can be remedied by fitting the aircraft with speed brakes/spoilers or installing a liquid cooling system to the engines. It also has a TBO of 1,400 hours which is low even for a turbocharged engine. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). Find more About Us here! 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. At 11,350 feet, the 414's single-engine service ceiling is below average, but, at 19,850, the 414A is tops in its class. This AD has a compliance time of 400 to 800 total time. The cabin length is 3.5 meters, height is 1.3 meters, and width is 1.4 meters. In a study of accident records some years ago, the 414 stood out as the safest light twin. Landing distance (50) 1,790. Americas owner-flown aircraft enthusiasts and active-pilot resource, delivered to your inbox! One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. Answer: An STC refers to a Supplemental Type Certificate. Also, corrosion on the engine frame rails is possible from exhaust leaks where the manifold exits into the turbocharger. Landing distance (50) 1,765. . The AD 2005-05-52 was put in place to counteract this issue by using eddy currents to inspect the said struts and visually inspect the auxiliary and rearward struts. https://www.federalregister.gov/documents/2005/06/14/05-11613/airworthiness-directives-cessna-aircraft-company-models-402c-and-414a-airplanes, Cessna 414. 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! The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Range 568-1,322. Gross wt. 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. 3,467. 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. Oh, and the aft toilet. In the years following its introduction, the airplane saw few major changes. Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. The factory tends to be much pricier than third-party garages that overhaul your engine. Engine and aerodynamic modifications abound for the 414. Interested in buying this aircraft click here. Please send us your experiences on your aircraft. On November 1, 1968, the prototype registered N7170C, conducted its maiden flight. Fuel capacity 213-270. The same long-stroke, trailing-link landing gear common to all Citation jets allows the softest landings and smooth taxiing. - Send us pictures of your plane. ) The resale value increases greatly if a RAM conversion has been done and additional performance modifications have been fitted. 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. Ceiling 27,400. Then in 1976, Cessna upgraded the engines to the newer -N series TSIO-520 offering a higher manifold pressure at 2700rpm, allowing the engines to maintain rated horsepower to 20,000 feet. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. 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. Specs, range, speed, operating weights and performance for the Cessna 340 here . To get at the fuel in the wing locker tanks, it must first be transferred to the mains. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. The greater the experience of the owner/pilot, the lower the premiums. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Your email address will not be published. Initial climb rate 1,900. The six- to seven-seat pressurized light transport is a step up for owners of the pressurized 340 and is fitted with the same 310-hp turbocharged engines. It did away with the extremely complicated and troublesome fuel system of the previous generations and replaced it with wet-wing fuel tanks that were 4.50 ft (1.37 m) longer and held 213 gal (968 l) total. 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. Engines two 375-hp turbocharged Continentals. 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. 414's will typically haul 5 people plus bags and full fuel. The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. 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. A 414A RAM Series VII with Winglets (AW) will compete in many ways with a 421C. There are only two fuel-. 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 Chancellors that cost close to $500,000 most often are pristine and like-new. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. 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 CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. Though its Continental engines could maintain their rated power at higher altitudes, Cessna implemented manifold pressure limitations above 20,000 ft (6,096 m) to prevent excessive engine temperatures. Plane and Pilot expands upon the vast base of knowledge and experience from aviations most reputable influencers to inspire, educate, entertain and inform. 180 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. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. 5 The length of the cabin was increased by 16 inches (40.64 cm), an extra window was installed, electronic propeller synchrophasing was made standard, and various ARC 400-series avionics equipment was included.