The Cessna 180 Skywagon is not a beautiful airplane, but it is a classic-looking taildragger that became an . All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. Ownership and operating costs. No warranty of Range 489-1,242. Other modifications in 1978 included a longer nosecone, a redesigned undercarriage system, and an extended wing without the earlier tip tanks. The maximum takeoff weight went up to 400 pounds to yield a higher useful load. Faster aircraft generally have a higher wing loading as less area is required to carry the same mass. Home > Aircraft Specs > Manufacturers > Cessna Aircraft > 414 pressurized-turbocharged Performance Information. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. Landing distance (50) 1,815. Compared to its biggest competitors-the 421 and Duke-a 414 provides a more room than the Duke, as much as the 421, travels a little slower, but does so more economically.MAINTENANCEEnsuring 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.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. 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. 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. )We spoke with Michael Cook and Todd Voshell who direct maintenance at Rapid Air, in Grand Rapids, Michigan, which has been operating 300 and 400 series Cessna twins for over 25 years. 2023 Madavor Media, LLC. The change allowed the engine to produce 310 hp (228 kW) at 2700 RPM from sea level to 20,000 ft (6,096 m). The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Its a combination of the airstair door, large cabin, air conditioning, abundant baggage space, large picture windows, pressurization and -not to be discounted-the potty! The exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. 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. The top of the line for the 414 is the series VI. In 1973, an updated 414 was released with major changes, this model was named the 414II. Beginning in 1978, Cessna offered three basic equipment packages. Bombardier Challenger 350 Guide and Specs: Is It Up to the Challenge? ) The new engine also has a TBO of 2,000 hours, which is a 600-hour increase from stock. Precise Flight and Spoilers, I. 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. CESSNA 414A Ram V. Retrieved October 8, 2021, from https://www.aircraftcostcalculator.com/AircraftOperatingCosts/350/Cessna+414A+Ram+V, Continental 520 overhaul cost. Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: 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. The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. The Cessna 414 is an incredibly popular pressurized cabin-class twin, with almost 650 registered in the US alone. (Beginning in 1957, horsepower was modestly increased to 230.) 200
In general, all owners praise the performance and capability of the aircraft, especially ones that have a RAM conversion and STOL kit, because it makes the aircraft much more versatile. 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. m, MTOW
As an Amazon Associate I earn from qualifying purchases. z-index: -1; They can be purchased from Micro Aerodynamics and VG Systems. 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 Initial climb rate 1,900. Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. }googletag.cmd.push(function() { googletag.display('inline'); });288All 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 411A, produced from 1967-68, featured a redesigned nose and more baggage space. I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. There are four options, all of which provide a sizable increase in horsepower, increase the TBO, and newer, more powerful propellers. (RVSM rules have generally limited 414s to 28,000 feet.) The system left room for error, not only on the part of the pilot, but among line personnel. Common are engine and aerodynamic modifications, including winglets. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. Already a member? Oh, and the aft toilet. 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. Annual inspections, repairs and pre-buys must be conducted by specialists. 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 winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. David is a seasoned pilot and aviation expert. Power was provided by twin 340-hp Continental engines, supercharged with AiResearch exhaust-driven compressors and turning full-feathering constant-speed propellers. Although not required on my serial number for many thousands of more hours, I had the spar strap mod installed and I cant emphasize enough how happy I am that I did it. 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. Absolutely the Right 414A RAM IV, This Aircraft is Impeccable and reflects the condition and attention to details that this owner has given N414EM with Only 20 Hours on each RAM Engine and 20 Hours.See More Details. Engine and aerodynamic modifications abound for the 414. Range 506- 1,325. However, most owners report that after a few hours of flying, it requires little thought. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. The new design used the same fuselage and tail as the 421 and the wing from the 402. LED landing and recognition lights offer enhanced visibility and strong illumination for night flying. This can be remedied by fitting the aircraft with speed brakes/spoilers or installing a liquid cooling system to the engines. It is the first turboprop-engine aircraft designed and manufactured by Cessna in the 1970s. 230
Distances Balanced Field Length: 2595 ft Landing Distance: 4000 ft Performance Rate of Climb: 1520 fpm Climb Rate One Engine Inop: 290 fpm Max Speed: 235 kts Normal Cruise: 203 kts Power Plant Engines: 2 Engine Mfg: Continental Engine Model: TSIO-520-NB Marketplace Information Interested in buying this aircraft click here! Reaching fever pitch in the 1980s, Cessna had positioned itself well for the demand, offering light twins for almost every conceivable subsection of the market. Best Range: 1106 NM Distances Takeoff Distance: 2185 ft Balanced Field Length: 2595 ft Landing Distance: 4000 ft Performance Rate of Climb: 1900 fpm Climb Rate One Engine Inop: 325 fpm Max Speed: 240 kts Normal Cruise: 230 kts Economy Cruise: 210 kts Cost per Hour: $ 522.43 Power Plant Engines: 2 Engine Mfg: Continental Engine Model: TSIOL-550A However, there seem to be plenty that are not. Fuel cost per hour: Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. It featured major modifications, including a restructured and increased wingspan, incorporating integral fuel tanks, and a stretched nose to allow more space for baggage. Currently, David flies twin retractables, notably the Pa44 Seminole and Pa30 Twin Comanche. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. Of course, any airplanes safety depends a great deal on the proficiency of its pilots. Despite that, cylinder head cracking has been a persistent problem for the -N and -NB engines (as well as for other IO-, TSIO- and GTSIO-520s). Trevin is a licensed flight instructor and pilot with degrees in Commercial Aviation and Aviation Management. Landing distance (50) 1,850. I bought it to replace a nice Cessna T310R, which I flew for about a year. However, it takes a longer distance high wing loading aircraft to takeoff and land. 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. Even with aging aircraft and occasional engine-related issues, the 414A offers a large cabin, the comfort and convenience of pressurization and the performance and safety of turbo charging. The aircraft was labeled the Chancellor in 1976. The aircraft can seat up to eight passengers and one or two crew. Takeoff distance (50) 2,220. 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. 4,640. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. 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. The pressure of the cabin is usually around 8,000 ft but can be less according to how the system is set up. MicroAerodynamics VGs provide a 350-pound gross-weight increase. Its wings are borrowed from the Model 414. 520
It can carry up to 8 passengers and baggage, or full fuel, but not both. (See www.ramaircraft.com.). The efficiency of the 414As long high-aspect ratio wing is highlighted by noting the 414As single-engine service ceiling is 19,850 feet. Preferred Airparts, based in Ohio, provide worldwide customers with surplus new Cessna original components and used parts from dismantled aircraft. no data
The Cessna 340 produced by Cessna. Initial climb rate 1,700. 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. Training is a must. text-align: center; For the 414, the engines chosen were the 310hp TSIO-520-Js, with intercoolers and takeoffs for cabin bleed air pressurization. Takeoff distance (50) 2,010. The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. They are the Cadillacs of the piston line, with attention having been paid to detail; even on an288airplane 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 big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte. Limiting speed for the extension of 15 degrees of flap was raised from 164 to 177 knots; Vlo and Vle were increased to an impressive 177 knots, from 143 knots.Beginning in 1978, Cessna offered three basic equipment packages. }.tdi_115.td-a-rec-img{ 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. 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! The Cessna 414 Chancellor series gets high marks for its spacious dwelling, generous baggage space and favorable control response. Otherwise, the periodicity is 1,600, or 200 hours depending on the mod state. Aircraft of similar configuration, age, and role include the Beechcraft Queen Air, AeroCommander 690, Piper Cheyenne, Beechcraft Duke, and the Piper Pa-31 Navajo. A typically equipped 414A has a full-fuel payload of about 500 to 700 pounds, depending on equipment. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. 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. Range 1,284. Owners recommend two groups. Finding replacement parts for a 414A is not as tough as one would think thanks to its shared parts with the 401 and 421. 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.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 takeoff distance is 408 meters while the landing distance is 365 meters. The 414A has an issue with shock cooling of the engine that occurs during rapid descents. Cabin specifications: 04'03" cabin high, 04'07" cabin wide, and 11'03" cabin long. 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. Retrieved October 5, 2021, from https://www.aopa.org/go-fly/aircraft-and-ownership/aircraft-fact-sheets/cessna-414, Company, S. P. (n.d.). Ive previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. 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. Gross wt. The 414A can be upgraded with the usual performance boosters such as vortex generators, which are highly recommended. If an owner has taken a maintenance only as required approach to their aircraft, they can expect a far lower resale value. These can be purchased by Sierra Industries. 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. 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. This has made insuring a 414 tougher. Based on the data collected from the available listings on the market, the average total time of a Cessna 414A is around 6,500 hours. In addition, the Chancellors wet wing has an increased fuel capacity of 106 gallons of usable fuel. Engines two 285-hp turbocharged Continentals. 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. The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg.