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Combining spacious cabins and relatively small, efficient engines, the 414 series can carry lots of fuel or a small crowd with their belongings-but not both. However, some years, unexpected maintenance can eat your lunch. 800 We are a collective group of airline instructors, and pilots dedicated to all things aviation. Retrieved October 7, 2021, from http://blog.overhaulbids.com/continental-overhaul-cost/continental-520-overhaul-cost/, Cox, B. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. Fuel capacity 202. The Chancellor utilizes the hydraulic components of the Golden Eagle gear and features a five-second retraction time. by Fuel capacity 202. 230 After the Chancellor debuted, there were few further refinements. 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. Takeoff distance (50) 2,010. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. PERFORMANCE: Top mph 268. Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. On November 1, 1968, the prototype registered N7170C, conducted its maiden flight. Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. It is powered by two wing-mounted 310hp (231kW) Continental TSIO-520-J horizontally opposed, six-cylinder engines. The older 414s are known as the short-bodied models. Initial climb rate 1,700. The Cessna 340 produced by Cessna. Best Cruise: 229 KIAS Takeoff distance (50) 1,700. Landing distance (50) 1,815. Come join us! 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. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. According to BWI Fly, for liability coverage of $1,000,000, a qualified pilot of a 414A who aims to use the aircraft for private use can expect to pay around $840 $1,400 per year and $4,400 $5,800 per year for a combination of the liability and hull coverage of $225,000. 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. Aerodynamic mods include vortex generators to increase aileron and rudder control authority at low speeds. All rights reserved. Ceiling 26,000. The STANDARD DATA: Seats 6-8. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). 200 (2001, February 26). In 1973 Cessna stretched the fuselage by 16 inches and added a fifth side window. No warranty of Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. 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. 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. Some low-time pilots might be approved for 340 insurance, but rejected for a 414/414A. Its wings are borrowed from the Model 414. 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. These aircraft arent like the 172s. 6,200: 6,430: Zero Fuel Weight - lbs. Cabin specifications: 04'03" cabin high, 04'07" cabin wide, and 11'03" cabin long. Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. 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 aircraft can seat up to eight passengers and one or two crew. - Send us pictures of your plane. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). He received his training at the University of North Dakota and has been in love with aviation for many years. 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. 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. 720 A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. Range 1,284. . The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. Engines two 375-hp turbocharged Continentals. Thus, it is an indication of age and use. According to Hangar 67, a very high-time 1979 model year 414A was recently sold at $129,900, which is the lowest price we have found. With a range of approximately 2,200 nautical miles and a relative low cost, the Conquest II was an unparalleled aircraft in its time. An STC is an approved modification to an aircraft, engine, or component. 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). 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. Find more About Us here! The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. The Chancellor 414A has an impeccable safety record. Engine and aerodynamic modifications abound for the 414. 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. I sell 25 Twin Cessnas a year, which usually includes six to eight 414s and 414As. We are a collective group of airline instructors, and pilots dedicated to all things aviation. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. 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. 1,580 FPM Rate of climb (1 engine out): 240 FPM Ceiling: 30,100 FT Ceiling (1 engine out): 11,350 FT Takeoff distance: 1,695 FT Landing distance: 805 FT Takeoff distance over 50ft obstacle: 2,350 FT Landing distance over 50ft obstacle: 1,865 FT Weights Gross Weight: 6,350 LBS Empty Weight: 4,039 LBS Maximum Payload: 1,769 LBS Fuel capacity: 102 GAL The landing gear was replaced, using the simpler system from the Cessna 414. While arguments rage today over whether the 414 or the 421 is the better aircraft, theres no doubt that with the 414, Cessna produced a comfortable, roomy, and stylish aircraft for personal and corporate travel. Fuel cost per hour: GlobalAir.com is your partner in connecting you with relevant information and resources. The displacement and power output remained the same, but the manifold pressure was increased from 36 hPa to 38 hPa. Cessna 414 chancellor. The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. Finally, the Riley Rocket 414 has two 400hp Lycoming IO-720 engines fitted. The design of the Cessna 414 was to bridge the gap between their unpressurized twin, the Cessna 402, and their pressurized flagship, the Cessna 421. The Cessna 414A is an improved 414 with narrower vertical tail, longer span bonded wet wing without tip tanks, a lengthened nose, re-designed landing gear and powered by two 310hp (231kW) TSIO-520-N engines. Stall mph 82. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. Real world speeds depend on engine configuration, but owners typically report 200 kts at about 38 gph in the upper teens. It also has a TBO of 1,400 hours which is low even for a turbocharged engine. Range 568-1,322. However, there are a number of airworthiness directives (AD) and service bulletins that have been published over the years. Most are the basic bucket.. Cessna 414 pressurized-turbocharged - Performance Data . Eight aircraft factors influence 414 resale plus many other economic factors. 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. Sure, many have been plowed up for houses or 2023 Aviation Publishing Group. We use cookies to help you get the best experience when using our website. In 1978, an enhanced version was launched, designated as the 414A Chancellor. As with all Twin Cessna's, the landing gear and exhaust systems must be maintained properly. 1000 In a study of accident records some years ago, the 414 stood out as the safest light twin. No warranty of 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 system left room for error, not only on the part of the pilot, but among line personnel. Since 2017 he's been working as a content writer and loves that he can combine his love of aviation and writing here at Aviator Insider. 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. To keep CHTs below red line I had to fly at no more than 55 percent power and with the cowl flaps open at high altitudes. In 1979, the 402s received a new wing, with a 5 feet (1.5 m) greater span. I have had my share of problems with turbos, turbo controllers, cylinders and cracked cases. There are only two fuel-288quantity indicators, both with three-position switches, to help the pilot keep track. 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. Cessna 182 vs 185 Compared: Which Is Better? He was a glider pilot for several years before obtaining his private license in taildraggers. 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. The nose baggage compartment of the 414A made CG juggling easier. One of our Planephd Experts will be in touch with you shortly. The remedy for this was increased visual inspections and the strengthening of the wing spars by adding spar straps. LED landing and recognition lights offer enhanced visibility and strong illumination for night flying. It's tempting to decry the disappearance of the classic country airport. Preferred Airparts, based in Ohio, provide worldwide customers with surplus new Cessna original components and used parts from dismantled aircraft. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. m, MTOW Both refer to ratings or approvals that a pilot must achieve to enable the operation of a multi-engined aircraft or flight under instrument flight rules. The 414A has a single-engine ceiling of 19,850 ft (6,050 m) which is the best among all its peers. Three significant milestones in 414 development took place in 1973, 1976, and 1979. Empty 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. FL Fuel capacity 213-270. Cruise mph 223. The biggest club for owners and operators of a 414A or any large Cessna twin is the Twin Cessna Flyer club. Airworthiness Directives; Cessna Aircraft Company models 402C and 414A airplanes. 310, Range 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 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. On the flip side, when fully loaded with eight passengers and baggage, there will be enough space for barely two hours of fuel. This can be remedied by fitting the aircraft with speed brakes/spoilers or installing a liquid cooling system to the engines. Im required to attend an approved school for recurrent training. 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. Checking the Cessna 152 POH it says to increase takeoff distance by 15% of ground roll (makes sense due to increased friction). Answer: Wing loading is the total aircraft mass divided by its wing area. The crosswind characteristics are good, and its easy to make squeaker landings. One of the most distressing issues the Cessna 414A has is cracking along the forward wing spars. Ive previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. RAM also makes winglets of their own design for the 414A to improve its aerodynamic performance. Best Range: 1106 NM The popularity of the aircraft ensures that there are enough aftermarket parts that can be bought if used parts are unavailable. The 414A has an issue with shock cooling of the engine that occurs during rapid descents. 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. Distinguishing features are: retractable landing gear and three-bladed, constant speed, fully feathering propellers. 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. Straight 414s with only 310-HP standard engines or even with a 325-HP RAM Series IV conversion will often have low useful loads. The aircraft was labeled the Chancellor in 1976. Otherwise, the periodicity is 1,600, or 200 hours depending on the mod state. The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. TAKE-OFF MTOW: WTC: RECAT-EU: Light Distance: V2 (IAS): 520 m 100 kts INITIAL CLIMB (to 5000 ft) IAS: ROC: 130 kts 1200 ft/min CLIMB (to FL 240) IAS: ROC: 150 kts 800 ft/min CLIMB (to FL 150) IAS: ROC: 150 kts 1000 ft/min MACH CLIMB MACH: ROC: - - CRUISE MACH: Ceiling: - 310 FL TAS: 230 kt Range: 1100 NM INITIAL DESCENT (to FL 240) MACH: - ROD: - The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. However, the eddy current method did not effectively identify the cracks until it was to the point where a load much lower than the published maximum load can cause catastrophic structural damage. They were the last of the pressurized, piston, 400-series airplanes Cessna developed, and pilots and mechanics will tell you that Cessna got it right with the Models 414 and 414A. https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). 414 chancellor. It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. The Chancellor is a popular aircraft, so it has an extensive range of aftermarket parts and modifications. Production aircraft were accessible in several optional seating configurations and avionics packages. 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. 3060 However, there seem to be plenty that are not. Utility twin aircraft. 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. The other category that brings the price up to the same number are the aircraft that have undergone a RAM conversion. Answer:The flaps extend to 45 degreesThe TSIO-520-NBs red-line is 2700 RPM. Operating Costs. The number of maintenance problems that can and do arise can cost a lot of money in a short time frame. In addition to the bare-bones model and the ARC 400-equipped 414AII, there was a III version with ARC 800- and 1000-series avionics, a Bendix RDR 160 weather radar and 100-amp alternators. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Your email address will not be published. Smart design means a better ride. 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. It is the first GA airplane Ive ever owned or flown that treats passengers as comfort-seeking humans and not adventurous sardines. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. kg, IAS 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 we look at the power loading of the aircraft, the why becomes obvious: weight. 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 aircraft got heavier, with the MTOW and landing weight increasing by 400 lbs (181 kg) and 550 lbs (249 kg), respectively. Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners. 6,500. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds.In the years following its introduction, the airplane saw few major changes. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. Landing Weight - lbs. Many of which have been addressed by ADs and service bulletins. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. Maximal total range:705 NM / 811 SMCruise speed:203 knots / 234 MPHAverage price:$344,804.81Number of passengers:7 people, Your email address will not be published. Six seats were standard; a seventh was available as an option. Specs, range, speed, operating weights and performance for the Cessna 340 here. Description Engines two 285-hp turbocharged Continentals. The new engine also has a TBO of 2,000 hours, which is a 600-hour increase from stock. Special Missions. 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. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. 1200 Its the third model in the Chancellor line and the successor to the Cessna 414II. }.tdi_115 .td-element-style{ For the Cessna 414A Chancellor, average pricing was US$280,000, having approximately 7,500 hours total time airframe (TTAF) and mid-life engines. Description The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. There are only two fuel-. To reach a cruising speed of 214 KTAS (246 mph / 396 kmph) 75% power is required, which will cause the 414A to burn around 19 gph (72 lph) per engine. Landing distance (50) 1,850. 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: If you are looking for factory parts sites like CessnaParts, AircraftSpruce, and Knots2U have a large catalog of parts available for purchase.Cessna Chancellor (414A) Common Problems. Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. 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: . ( Any part that isnt new is all overhauled from the turbocharger to the fuel pressure regulator. ft/min, IAS . Landing distance (50) 2,393. The Chancellor replaced the former 414 in 1978 and offered a new level of payload performance, range, and fuel efficiency. 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. The most significant and popular modifications that can be made to a 414A are the engine swaps by the RAM Aircraft Corporation. They can be purchased from Micro Aerodynamics and VG Systems. CESSNA, V2 (IAS) In the years following its introduction, the airplane saw few major changes. How much does it cost to fly: $683.19 per hour. 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. kts, ROC 130 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). My flights range from an hour to four hours and while I have flown the airplane from coast to coast, I find trips of three hours or less are well suited for the airplane. 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. It has a range of 1,328 nautical miles and a climb rate of 1,520 feet per minute. Propeller- to-fuselage clearance is more than 31 inches for a very quiet cabin. The two main tanks were essential sections of the sealed wet wing. The fuselage and tail were essentially the same as the ones used on the 421B, while the wings were taken from the 401. 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 longer fuselage now allowed for an eighth seat to be added as an option. However, it takes a longer distance high wing loading aircraft to takeoff and land. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. Range 1,284. }.tdi_115.td-a-rec-img{ With the rise in FAA-PMA approved manufacturers, many have niched down to support a particular aircraft type and finding trim (knots2u, Texas Aeroplastics or AvFab), landing gear components (Robair Repair), or lighting (Whelen Aerospace Technologies or AeroLeds) for your 414 is not hard. Take an early model 414 with -J engines and complete this upgrade to receive a 1600 hour TBO, up from the original 1400. }@media (max-width: 767px) { The figures show that the demand for Dakotas has increased causing prices to rise by about 40 percent. All rights reserved. I have owned a 1979 C414AW (a 414A with RAM winglets) for five years and about 2400 flight hours. Takeoff distance (50) 1,662. (n.d.). A brand new engine exchange from Continental costs an average of $60,000. 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. 6,165: 6,165: SOURCE: Sources. Service ceilings are above 30,000 feet, but few owners fly that high.