Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners. The 411A, produced from 1967-68, featured a redesigned nose and more baggage space. The pressurized comfort of the 414A, which produces an 8000-foot cabin at 22,800 feet, cannot be overemphasized. Cessna 414 Guide and Specs : Is It High Performance? by the manufacturer or FAA. Its an excellent idea, regardless of how much time you have. The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). We use cookies to help you get the best experience when using our website. Winglets aid climb and cruise speeds. Stall mph cabin is separated from the passenger compartment by a divider. Above this speed, turbulence or rapid control deflections increase the chance of structural damage. The air is run through a compressor connected to the intake manifold of the engine to create a more efficient fuel burn which will eventually produce more power. In 1973 Cessna stretched the fuselage by 16 inches and added a fifth side window. 3060 Once it reaches the cabin it is compressed enough to create an atmospheric pressure that mimics the desired altitude. Cruise mph 277. ft/min, TAS Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. The piping which directs the exhaust from the manifold to the turbo is also susceptible to cracking. It's also a myth. Some ADs have called for replacing faulty parts such as a set of vacuum pumps, and bolts on the fork of the main landing gear. With its bigger nose and lockers, the 414A can carry 1500 pounds. Refreshment centers can be aft or a vertical unit positioned behind the pilot or copilot seat. I sell 25 Twin Cessnas a year, which usually includes six to eight 414s and 414As. 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. Production aircraft were accessible in several optional seating configurations and avionics packages. The aircraft got heavier, with the MTOW and landing weight increasing by 400 lbs (181 kg) and 550 lbs (249 kg), respectively. 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. The variable costs such as maintenance for the airframe, as well as other costs such as landing and parking fees totaling $206,550. Of course, any airplanes safety depends a great deal on the proficiency of its pilots. (n.d.). Please send us your experiences on your aircraft. Citation Longitude - Cessna Cessna 414 - Wikipedia An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Aircraft of similar configuration, age, and role include the Beechcraft Queen Air, AeroCommander 690, Piper Cheyenne, Beechcraft Duke, and the Piper Pa-31 Navajo. 4,640. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Stall mph 81. 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. no data Remained in production until 1985. 1978 - 1985 CESSNA 414A Chancellor III - Planephd Although you could fly for about 1,100 miles, you would be able to bring only two friends and a few bags. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. 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. 150 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. fitness for any purpose is made or implied. Continental also published overhaul procedures to enable -NB engines to get the TBO boost.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). 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. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. 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. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. A typically equipped 414A has a full-fuel payload of about 500 to 700 pounds, depending on equipment. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. 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. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. Go figure. When discussing 414s and 414As, one must speak correctly. After the Chancellor debuted, there were few further refinements. Its the third model in the Chancellor line and the successor to the Cessna 414II. Any part that isnt new is all overhauled from the turbocharger to the fuel pressure regulator. }.tdi_115 .td-element-style{ Rate of Climb: 1650 fpm; Climb Rate One Engine Inop: 315 fpm; Max Speed: 243 kts; Normal Cruise: 229 kts . These aircraft were called the 414 Chancellor. 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. The exact specifications of the Cessna Chancellor 414A are: A hotch-potch of the Cessna 401 and 421, the Chancellor easily stole the limelight as the best of the 400-series, even though it was meant to simply fill the gap between the two, and became a hit among pilots everywhere, and in recent years has gained popularity with charter operators. The Cessna 340 produced by Cessna. ) . Derived from the Model 411, the Cessna 401 and 402 are essentially the same aircraft put to two different uses. Oh, and the aft toilet. There are only two fuel-. Pricing Cessna 195 Guide and Specs : All About The 195 Businessliner, Bombardier Challenger 300 Guide and Specs, Installed equipment, specially avionic fit-out. kt, Ceiling Cruise mph 223. 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. Coupled with smaller engines than the 421, you had an economical transport that could carry a couple of passengers and baggage over 1000 miles or six executives to a day meeting two hours away. 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. Ceiling 26,000. 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. ft/min, ROC Its wings are borrowed from the Model 414. 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. The remedy for this was increased visual inspections and the strengthening of the wing spars by adding spar straps. 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. Many of which have been addressed by ADs and service bulletins. Membership in and attending the Twin Cessna Flyer Organizations Pilot Seminars should be required. Finding replacement parts for a 414A is not as tough as one would think thanks to its shared parts with the 401 and 421. ( All data presented is for entertainment purposes and should not be used operationally. List price was $138,000 (thats over $740,000 in 2007 dollars)-$35,000 less than the Duke and some $50,000 less than both the 421 and Pipers P-Navajo.Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. AOPA. Answer: Pressurization is the creation of a false atmosphere in the cabin of the aircraft in order to allow us to breathe at higher altitudes without pure oxygen. The 414 does have AD97-26-16 requiring consideration, and those aircraft requiring regular x-ray and ultimate installation of the service kit will necessarily command a lower price. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. Much has been written about the 414s, but its no big deal. The 1970 to 1972 models are referred to as short-bodied 414s. Some low-time pilots might be approved for 340 insurance, but rejected for a 414/414A. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. During that period, I have exchanged two sets of engines (RAM IV), two props (one new set), two paint jobs, an interior and updated the avionics. Deserving of Respect and Praise: Cessna's 421C Cessna Country: United States Manufactured: 1972 to: 1984 ICAO: C340 Price: US$.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 1000 3,865. A brand new engine exchange from Continental costs an average of $60,000. With the O&N tanks in both nacelles, I can carry up to 260 gallons of fuel, good for over seven hours of endurance. Citation CJ4 Gen2 - Cessna 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. Cessna 414 pressurized-turbocharged - Performance Data . 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! 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. Another area that needs to be checked for corrosion is the firewall. Another point of consideration for a 414 buyer is the SB/AD on the wing spar. They can be purchased from Micro Aerodynamics and VG Systems. Kudos go to Cessna for rising to the occasion. 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. 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. By continuing to use this website, you are agreeing to our Cookie Policy. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. If you opt to go for a rebuilt engine from Continental will save you $6,000, for a total price of $54,000. Power was provided by twin 340-hp Continental engines, supercharged with AiResearch exhaust-driven compressors and turning full-feathering constant-speed propellers. A 414A RAM Series VII with Winglets (AW) will compete in many ways with a 421C. The change allowed the engine to produce 310 hp (228 kW) at 2700 RPM from sea level to 20,000 ft (6,096 m). Range 1,284. Technique: Landing like a pro - AOPA One former owner even stated that anyone who says the aircraft is reliable is delusional. 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. I have put in three different heaters over the past several years and changed out all the blower motors, ductwork, fuel pump, fuel pressure regulator, igniter, air flow sensor and thermostat at least once and I still plan for failure in flight. In a study of accident records some years ago, the 414 stood out as the safest light twin. The 414A has a combined 620 hp (456 kW), however, takeoff acceleration might not be as neck-snapping as one would assume.

Miracle Kaye Hall Mississippi Court Records, Last Person Hanged In Tasmania, Articles C