Given the popularity of the 414 series, its fair to say that if you need a modification, you can find 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 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. 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. One club offers extensive support for the 414, in addition to all other twin Cessnas. Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. 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. Propeller- to-fuselage clearance is more than 31 inches for a very quiet cabin. Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. Initial climb rate 1,900. 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 main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. Each of its 620 hp has to carry 10.8 lbs, which is quite poor. A $153,750.00 loan over 10 years including $640.62 per month in interest equates to a $7,709.60 per-month payment. 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. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. When we look at the power loading of the aircraft, the why becomes obvious: weight. Stall mph 79. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. The exhaust system sees a great deal of heat and vibration, thus components wear out. 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). There are only two fuel-288quantity indicators, both with three-position switches, to help the pilot keep track. 1970 - 1977 CESSNA 414 - Specifications, Performance - Planephd 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 two 375-hp turbocharged Continentals. The other category that brings the price up to the same number are the aircraft that have undergone a RAM conversion. By all accounts, vortex generators reduce Vmc and stall speeds. One of the biggest weak points of the 414A is the problematic Continental TSIO-520-NB engine. Phone: (305) 342-0760. Fuel transferred too early is pumped overboard. When pilots are flying IFR, it means they are under the control of Air Traffic Control. 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. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). RAM also makes winglets and vortex generators. The 414A has an issue with shock cooling of the engine that occurs during rapid descents. The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. 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. Other modifications in 1978 included a longer nosecone, a redesigned undercarriage system, and an extended wing without the earlier tip tanks. With rare exception, all 414As have an aft potty. Fuel capacity 202. 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. The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg. Would like to understand why. However, there are a number of airworthiness directives (AD) and service bulletins that have been published over the years. Total Cost of Ownership: $39,555.22 Loading must be watched carefully to avoid going out of the rear CG limit. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. Trevin is a licensed flight instructor and pilot with degrees in Commercial Aviation and Aviation Management. 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. 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. With its bigger nose and lockers, the 414A can carry 1500 pounds. Finally, in 1979 the -NB series TSIO-520 engines were installed, providing an improved crankshaft, and in time, an increased engine TBO of 1600 hours against the -Ns 1400. 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. Cruise mph 223. It is capable, comfortable, and performs well. The Cessna 340 is a pressurized six-place twin featuring center-aisle seating, an air-stair door, and top cruise performance. One of our Planephd Experts will be in touch with you shortly. 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. With the O&N tanks in both nacelles, I can carry up to 260 gallons of fuel, good for over seven hours of endurance. The 414A can be upgraded with the usual performance boosters such as vortex generators, which are highly recommended. 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. This AD has a compliance time of 400 to 800 total time. The first Cessna Chancellor the 414 took to the skies in 1968, and was produced from 1970 onwards. The engine is chock-full of new RAM components such as camshafts, cylinders, crankshaft, piston rods. In airplane engines, turbochargers are popularly used to achieve forced induction. (See page 25 for an abbreviated AD list.). Sure, many have been plowed up for houses or 2023 Aviation Publishing Group. They can be purchased from Micro Aerodynamics and VG Systems. Airworthiness Directives; Cessna Aircraft Company models 402C and 414A airplanes. Another point of consideration for a 414 buyer is the SB/AD on the wing spar. Cessna 152 - Price, Specs, Photo Gallery, History - Aero Corner 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 kt, MCS 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. .tdi_115.td-a-rec-img { A direct competitor of the 414A is the Beechcraft King Air. The pressure of the cabin is usually around 8,000 ft but can be less according to how the system is set up. Engine and aerodynamic modifications abound for the 414. 1978 - 1985 CESSNA 414A Chancellor III - Planephd After the Chancellor debuted, there were few further refinements. The 340 has a gross weight of 5,975 pounds, and an empty weight of 3,697 pounds. 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. He received his training at the University of North Dakota and has been in love with aviation for many years. I have had my share of problems with turbos, turbo controllers, cylinders and cracked cases. Kudos go to Cessna for rising to the occasion. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. The fuel system composed of a pair of main tanks and fuel selectors, emergency cross-feed shutoff valves, and other crucial parts to complete the system. 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 1970 to 77 Cessna 414 is often referred to as a straight 414, straight meaning no suffix A and not meaning a straight wing. Continental also published overhaul procedures to enable -NB engines to get the TBO boost. Overall, the 414A is a capable aircraft. Cessna 414A Private Jet Charter - Paramount Business Jets Flight planning or any other aircraft operations should only be done using official technical information provided z-index: -1; 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 owners of Cessna 414As have mixed reviews. STANDARD DATA: ( 411) Seats 6-8. Answer: Maximum structural cruise, or Vno, refers to the airspeed above which the aircraft should be flown only in smooth air. Stall mph 82. 1200 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. (See www.ramaircraft.com. Range 489-1,242. Features wing of CESSNA 402 and fuselage of CESSNA 421. 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. Cessna Skyhawk I have owned a 1979 C414AW (a 414A with RAM winglets) for five years and about 2400 flight hours. 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. 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 aircraft factors are: These terms are all within the control of the owner. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. The basic 414 was born in 1970 with a 4.2 psi pressurization differential and ascended to become the Chancellor in 1978. PERFORMANCE: Top mph 268. The STANDARD DATA: Seats 6-8. For the 414, the engines chosen were the 310hp TSIO-520-Js, with intercoolers and takeoffs for cabin bleed air pressurization. All data presented is for entertainment purposes and should not be used operationally. Some low-time pilots might be approved for 340 insurance, but rejected for a 414/414A. The 414A has a single-engine ceiling of 19,850 ft (6,050 m) which is the best among all its peers. Membership in and attending the Twin Cessna Flyer Organizations Pilot Seminars should be required. Empty wt. Aircraft of similar configuration, age, and role include the Beechcraft Queen Air, AeroCommander 690, Piper Cheyenne, Beechcraft Duke, and the Piper Pa-31 Navajo. Why is the landing distance increased on grass runways? Approaching and landing with minimal power is a good habit. By. 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. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. Some potties have a flushing feature. Cessna 414/414A Speed, Style, Class - AVweb Ceiling: 30,800 FT Ceiling (1 engine out): 19,850 FT Takeoff distance: 2,185 FT Landing distance: 1,013 FT Takeoff distance over 50ft obstacle: 2,595 FT Landing distance over 50ft obstacle: 2,393 FT Weights Gross Weight: 6,750 LBS Empty Weight: 4,543 LBS Maximum Payload: 1,769 LBS Fuel capacity: 213 GAL Ownership Costs 1978 Total Cost of Ownership: Its an $800 part.MODS, CLUBSAmong the most popular mods are the RAM Aircraft Corporation engine swaps. Cruise Speed: 224 kts: Fuel Capacity: 102 gal: Stall Speed (dirty): 70 kts: Range: 1090 nm: Takeoff: Landing: Ground Roll: 1695 ft: Ground Roll 805 ft: Over 50 ft obstacle . Its an excellent idea, regardless of how much time you have. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Federal Register. 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. Thus, it is an indication of age and use. Initial climb rate 1,610. Stall mph 81. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. ), 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. Cruise mph 277. These aircraft were called the 414A Chancellor. If followed carefully, a mechanic wont miss anything. The 421B tiptank twin Cessna has fuel carried in the mains (tips), auxiliary fuel cells in the wings and optional nacelle tanks. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. 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. 414 Chancellor | Cessna Owner Organization I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. 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. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Your email address will not be published. The biggest club for owners and operators of a 414A or any large Cessna twin is the Twin Cessna Flyer club. Retrieved October 5, 2021, from https://www.globalair.com/aircraft-for-sale/Specifications?specid=971. kt, Ceiling no data by the manufacturer or FAA. Six seats were standard; a seventh was available as an option. Cessna 180 Skywagon: Legendary popularity - AOPA Cessna's 414 is among a large group of aircraft headed for extinction. ( All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. Three significant milestones in 414 development took place in 1973, 1976, and 1979. The Chancellor utilizes the hydraulic components of the Golden Eagle gear and features a five-second retraction time. It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. Whats Going On with Cessna Denali Turboprop. (Beginning in 1957, horsepower was modestly increased to 230.)

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