An STC is an approved modification to an aircraft, engine, or component. The first Cessna Chancellor the 414 took to the skies in 1968, and was produced from 1970 onwards. Fuel capacity 102-207. Winglets aid climb and cruise speeds. These aircraft were called the 414A Chancellor. The applications are smaller and they have maintenance issues, so the price does fall. In a study of accident records some years ago, the 414 stood out as the safest light twin. . - Aircraft specific reviews and articles. For 1981, Chancellor refinements included a heated fuel manifold, frost panes for cockpit side windows, and threadless-blade propellers. Controls consisted of on/off/crossfeed valves and a fuel flow computer/indicator was added. The pressure of the cabin is usually around 8,000 ft but can be less according to how the system is set up. 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. Given the age and systems on the 414, plenty of airworthiness directives need reviewing for compliance. 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. Become a member and get exclusive access to articles, contests and more! Stall mph 82. Eight aircraft factors influence 414 resale plus many other economic factors. EASY ACCESS Two large cabin doors allow for convenient entry and loading for student and instructor. Retrieved October 7, 2021, from http://blog.overhaulbids.com/continental-overhaul-cost/continental-520-overhaul-cost/, Cox, B. In the early 414s, the main landing gear webbing is prone to cracking, requiring extensive rectification. The 414 and 414A truly provide a great family or business aircraft. no data Retrieved October 5, 2021, from https://www.aopa.org/go-fly/aircraft-and-ownership/aircraft-fact-sheets/cessna-414, Company, S. P. (n.d.). The older 414s are known as the short-bodied models. The 375-HP 421Cs single engine ceiling is 14,900 feet. That resulted in cruise speeds of only about 180 to 185 KTAS up high. 800 Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. 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. Answer: IFR means Instrument Flight Rules. Go figure. 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. 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. Their parts may seem expensive, but they continue supporting us owners, and for that I am very willing to see them earn afair profit. The Piper Seneca is also quite similar to the 414A, even though it is slightly smaller. So before buying one, you should ensure that there is an AMT with experience on pressurized Cessna twins in your area. Fuel capacity 213-270. The top of the line for the 414 is the series VI. A brand new engine exchange from Continental costs an average of $60,000. If followed carefully, a mechanic wont miss anything. The 414A has a combined 620 hp (456 kW), however, takeoff acceleration might not be as neck-snapping as one would assume. VGs are also available from Micro Aerodynamics (www.microaero.com) and V/G Systems, phone 800-328-4629. 414,Chancellor The RAM IV struggled in the flight levels, especially in the summer. Give me one three-hour cross country with any new owner and hell be able to teach the system. (38.0 gallons/hr @ $5.40/gal), Misc: landing, parking, supplies,catering, etc, Typical Price: $307,752.00 The aircraft also featured a 28V, negative ground, direct current electrical system charged by an alternator on each engine, and a 24V battery. Cessna 120 Guide and Specs : Is It Powerful Enough? Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners.Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. 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. }.tdi_115.td-a-rec-img{ 100 kt, ROD According to Aircraftcostoperator.com, the average total hourly cost of operating a Cessna 414A is roughly $535. Specs, range, speed, operating weights and performance for the Cessna 340 here . Range 506- 1,325. Landing Distance: 2393 ft: 729 m: Max Takeoff Weight: 6751 lbs: 3062 kg: Max Landing Weight: 6750 lbs: 3062 kg: Useful Weight: 2417 . 2023 Madavor Media, LLC. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Annual inspections, repairs and pre-buys must be conducted by specialists. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. Cessna 414 Guide and Specs : Is It High Performance? The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. The engines were taken from the 402, with the only changes made to the setup were the inclusion of parts for bleed-air cabin pressurization, and different intercoolers. Down low, performance is nothing to write home about, but get those superchargers working at altitude, and youll see some decent cruise speeds at acceptable fuel flows. Checking the Cessna 152 POH it says to increase takeoff distance by 15% of ground roll (makes sense due to increased friction). Engines two 340-hp turbocharged Continentals. A qualified pilot is considered to be one with a PPL license with IFR and MEL ratings, who have 1,500 total hours, 500 MEL hours, and 25 hours on type. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. Model 414 seats up to 7 passengers and 1 pilot. by the manufacturer or FAA. Improved version CESSNA 414A Chancellor (appeared in 1978) with bonded wet wing, without tip tanks. by the manufacturer or FAA. The fuselage and tail were essentially the same as the ones used on the 421B, while the wings were taken from the 401. As has often been said, Cessna really got it right with the 414/414As. The original 414 aircraft retailed at US$138,000 in 1970. Production aircraft were accessible in several optional seating configurations and avionics packages. kg, IAS ft/min, ROC With bigger turbochargers and intercoolers, much larger cowl flaps, new intake air scoops, and Scimitar props, the airplane becomes an entirely new animal within seconds of leaving the runway. m. All data presented is only indicative and should not be used operationally. 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. PERFORMANCE: Top mph 268. ), 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. Oh, and the aft toilet. Twin engine piston aircraft with retractable landing gear. The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. Speed brakes/spoilers are available from PowerPac Spoilers (www.powerpacspoilers.com) and more advanced intercoolers come from American Aviation (www.americanaviationinc.com). Of course, any airplanes safety depends a great deal on the proficiency of its pilots. Answer: The process of delivering compressed, denser air to a combustion engine is referred to as forced induction. Interested in buying this aircraft click here. 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 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. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. Mandatory power reductions during the climb above FL220 meant long climb times and getting above FL250 seemed to take forever at the 200 FPM climb rate that could be achieved up there. Landing distance (50) 1,815. [2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]. Performance specifications Horsepower: 2 x 375 HP Best Cruise Speed: 241 KIAS Best Range (i): 1,197 NM Fuel Burn @ 75%: 47.0 GPH Stall Speed: 74 KIAS Rate of climb: 1,940 FPM Rate of climb (1 engine out): 350 FPM Ceiling: 30,200 FT Ceiling (1 engine out): 14,900 FT Takeoff distance: 1,786 FT Landing distance: 720 FT An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. The Chancellor 414A has an impeccable safety record. Stall mph cabin is separated from the passenger compartment by a divider. The more the industry drags out phasing out 100LL, the more susceptible it is to looking unconcerned about public health risks. 414 chancellor. GlobalAir.com is your partner in connecting you with relevant information and resources. https://www.federalregister.gov/documents/2005/06/14/05-11613/airworthiness-directives-cessna-aircraft-company-models-402c-and-414a-airplanes, Cessna 414. Cessna 414 Stock Airplane vs. RAM Series VII; Primary Specifications Cessna 414 Otherwise, the periodicity is 1,600, or 200 hours depending on the mod state. The landing gear is the standard electromechanical system that is on all tiptank twin Cessnas. Approaching and landing with minimal power is a good habit. Landing distance (50) 1,815. We previously highlighted engine mount beam fatigue cracking, main landing gear web cracking, and engine frame rail corrosion, all necessitating diligent maintenance inspections and AD compliance. Passengers love it for space, comfort, and low noise levels. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. 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. 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. With rare exception, all 414As have an aft potty. The Cessna 152 has a maximum cruise speed of 109 knots and a travel range of 415 nautical miles. 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). 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. 3,865. ft/min, IAS Ceiling 29,800. PERFORMANCE: Top mph 268. 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. kt, Distance The aircraft was labeled the Chancellor in 1976. 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. 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. Areas to watch on the pressurization system are to make sure the nine drain seals are changed regularly as they deteriorate and become brittle and to regularly check the pressurization ducts off of the heater, forward of the forward pressure bulkhead as they can develop major leaks. The new engine also has a TBO of 2,000 hours, which is a 600-hour increase from stock. 2023 GlobalAir.com. Cessna Country: United States Manufactured: 1978 to: 2006 ICAO: C550 Price: US$1.1 million (2019) Performance Weights Dimensions Avionics: Garmin 700 Engine: 2x Pratt & Whitney Canada JT15D-4B Turbofan Power: 2,500 pound-force Max Cruise Speed: 403 knots 746 Km/h Approach Speed (Vref): 82 knots Travel range: 2,000 Nautical Miles 3,704 Kilometers The aircraft got heavier, with the MTOW and landing weight increasing by 400 lbs (181 kg) and 550 lbs (249 kg), respectively. 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. He's worked on various aircraft from small two-seaters like Tomahawks or Boeing 767s. On a standard day, when loaded to MTOW, it needs 4,000 ft (1,219 m) to hit Vr and then come to a complete stop. 180 B. C. (2015, July 13). The exhaust system sees a great deal of heat and vibration, thus components wear out. Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. The first Cessna Chancellor - the 414 - took to the skies in 1968, and was produced from 1970 onwards. The deice light on the panel illuminates only very briefly when the pneumatic deicing system is activated and only indicates that theres pressure to the tail boots. 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.Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. It was developed to bridge the gap between the unpressurized Cessna 401 and the pressurized, more powerful Cessna 421. Fuel cost per hour: The aircraft factors are: These terms are all within the control of the owner. 1200 kt, MCS 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. The 340 has a gross weight of 5,975 pounds, and an empty weight of 3,697 pounds. I have split my time about equally between the RAM IV 325-HP engines and the RAM VII 335-HP engines and Scimitar props that I had installed when the RAM IVs hit their TBO. The piping which directs the exhaust from the manifold to the turbo is also susceptible to cracking. He received his training at the University of North Dakota and has been in love with aviation for many years. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. Power. The popularity of the aircraft ensures that there are enough aftermarket parts that can be bought if used parts are unavailable. How much does it cost to fly: $683.19 per hour. The Cessna Pilots Association, located at www.cessna.org, and the Twin Cessna Flyer, at www.twincessna.org. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. BUILT FOR TRAINING Ideal for entry-level landings, the Skyhawk piston features a sturdy tricycle landing system and a resilient airframe. Fuselage strakes improve yaw control, performance in turbulence, and a higher cruise speed. Bombardier Challenger 350 Guide and Specs: Is It Up to the Challenge? STANDARD DATA: (T310R) Seats 4-6. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. Best Cruise: 229 KIAS Answer: Wing loading is the total aircraft mass divided by its wing area. Those owners who try to operate an aircraft like the Cessna 414 on a shoestring are pursuing false savings. Cessna's 414 is among a large group of aircraft headed for extinction. There was a time in aviation history when aircraft manufacturers were falling over themselves to serve a seemingly insatiable demand for executive-level light twin-engined aircraft. 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). Cessna Caravan Maximum Range: 1,070 nm Maximum Occupants: 10 - 14 Cessna SkyCourier (Freighter) Maximum Range: 940 nm Payload: 6,000 lb Cessna SkyCourier (Passenger) Maximum Range: 920 nm Maximum Passengers: 19 Single Engine Aircraft 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. 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! I have owned and flown a 1979 Cessna 414A for 14 months, accumulating 235 hours in all sorts of conditions. (See page 25 for an abbreviated AD list.). (2001, February 26). 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. I own a 1978 Cessna 414A which I acquired in 1989. Controls consisted of on/off/crossfeed valves and a fuel flow computer/indicator was added.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. The nose baggage compartment of the 414A made CG juggling easier.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. A pilot in a hurry will see 205 knots on 38 GPH at 75 percent power rich of peak, although few operate that way anymore. It is our mission to be the go to leaders in the aviation industry. After the Chancellor debuted, there were few further refinements. Most of the ADs for the 414A have increased the frequency of inspections and services of systems that are problematic and if adequate preventative maintenance is not done, could lead to massive bills. Cruise mph 223. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. Any part that isnt new is all overhauled from the turbocharger to the fuel pressure regulator. Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. Remained in production until 1985. One of the most distressing issues the Cessna 414A has is cracking along the forward wing spars. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds.In the years following its introduction, the airplane saw few major changes. The cabin length is 3.5 meters, height is 1.3 meters, and width is 1.4 meters. 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 Another area that needs to be checked for corrosion is the firewall. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. Although you could fly for about 1,100 miles, you would be able to bring only two friends and a few bags. 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. (n.d.). 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. Power was provided by twin 340-hp Continental engines, supercharged with AiResearch exhaust-driven compressors and turning full-feathering constant-speed propellers. 520 One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. Less powerful, light and low cost model of CESSNA 421 Golden Eagle. Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: A cabin differential of 5.0 psi allows a 10,000-foot cabin at 26,500 feet. There are only two fuel-288quantity indicators, both with three-position switches, to help the pilot keep track. These can be purchased by Sierra Industries. The 414 was built using parts from other 400-series aircraft. Empty wt. Cruise mph 277. The 401, introduced in 1966 and discontinued in 1972, was basically designed as a medium to . 1000 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. 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. It has a range of 1,328 nautical miles and a climb rate of 1,520 feet per minute. Down low under 10,000 feet, things are much slower, more like 170 to 175 KTAS. The engines on the 414II were upgraded to the newer Continental TSIO-520-Ns. The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. The Chancellors that cost close to $500,000 most often are pristine and like-new. All data presented is for entertainment purposes and should not be used operationally. Required fields are marked *. (See www.ramaircraft.com. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. 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. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. Aerodynamic mods include vortex generators to increase aileron and rudder control authority at low speeds. The Chancellor replaced the former 414 in 1978 and offered a new level of payload performance, range, and fuel efficiency. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. 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. 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. Baggage capacity of the 414 is 930 pounds, and cabin seating is available with an array of executive options. By continuing to use this website, you are agreeing to our Cookie Policy. Based on 450 hours a year and fuel cost at $5.00 per-gallon, the CESSNA 414A has total variable costs of $233,550.00, total fixed costs of $73,885.00, and hypothetical summary cost of $307,435.00. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. Operating Costs. 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. 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.
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