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. Takeoff distance (50) 2,220. Fuel cost per hour: Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. This plane was. The aircraft also featured a 28V, negative ground, direct current electrical system charged by an alternator on each engine, and a 24V battery. EASY ACCESS Two large cabin doors allow for convenient entry and loading for student and instructor. 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. }@media (max-width: 767px) { Developed from the 310, it utilizes a similar landing gear and tail unit. 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. Fuelburn: 34.0 GPH 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. One former owner even stated that anyone who says the aircraft is reliable is delusional. no data Answer: An STC refers to a Supplemental Type Certificate. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. According to the president of the Twin Cessna Flyer a society for owners of Cessna Twin aircraft Larry Ball, there are a few more problem areas of the 414A that have not been published but are common enough to talk about. This can be remedied by fitting the aircraft with speed brakes/spoilers or installing a liquid cooling system to the engines. 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. The RAM VII changed all that. RAM also makes winglets of their own design for the 414A to improve its aerodynamic performance. It is our mission to be the go to leaders in the aviation industry. The RAM IV struggled in the flight levels, especially in the summer. Controls consisted of on/off/crossfeed valves and a fuel flow computer/indicator was added. 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. Engines two 340-hp turbocharged Continentals. The engine is notorious for cracked cylinders and therefore requires periodic inspections. An STC is an approved modification to an aircraft, engine, or component. Fuel transferred too early is pumped overboard. - Aircraft specific reviews and articles. In 1978, an enhanced version was launched, designated as the 414A Chancellor. Top mentions include the true cabin class, reasonable cruise speed, and maintenance of sea-level pressure to 10,000 feet. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. Bringing the grand annual total to $240,785. Sure, many have been plowed up for houses or 2023 Aviation Publishing Group. Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. Fuel capacity 202. 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. There are several problems that the 414A has. 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. 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 exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. Buyers should be looking carefully for compliance. It featured major modifications, including a restructured and increased wingspan, incorporating integral fuel tanks, and a stretched nose to allow more space for baggage. 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. 130 All aircraft, engines, and components have type certificates that approve their use. Ceiling 27,400. Heres an even more interesting thing-normally, the RAM engines want to gulp down 19 to 22 GPH a side at higher power settings. Also worth joining is the Cessna Pilots Association (www.cessna.org and 805-934-0493). 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. Fuselage strakes improve yaw control, performance in turbulence, and a higher cruise speed. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. 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. 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. It is powered by two wing-mounted 310hp (231kW) Continental TSIO-520-J horizontally opposed, six-cylinder engines. Each of its 620 hp has to carry 10.8 lbs, which is quite poor. Landing distance over 50-ft obstacle: 2,393 ft: Landing distance, ground roll: 1,013 ft: Limiting and . 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. Smart design means a better ride. . 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. Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. 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 1970 to 77 Cessna 414 is often referred to as a straight 414, straight meaning no suffix A and not meaning a straight wing. - Features that would be useful to you. Most had the RAM VI engine conversion. 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. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. One of the most important came in 1973, when . 414,Chancellor Propeller- to-fuselage clearance is more than 31 inches for a very quiet cabin. Always remember where the wind is coming from and adjust the pattern accordingly. Range 1,284. In the early 414s, the main landing gear webbing is prone to cracking, requiring extensive rectification. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. It is the first GA airplane Ive ever owned or flown that treats passengers as comfort-seeking humans and not adventurous sardines. This is when Cessna decided to take advantage of Continental Motor's then-new, 225-horsepower O-470-A engine and develop the robust Cessna 180, which first flew in May 1952. This piston engine is a six-cylinder, horizontally-opposed, direct drive, turbocharge, air-cooled, and fuel-injected type that produces a maximum thrust of 310 horsepower each. 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. Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. Stall mph 82. 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. The owners of Cessna 414As have mixed reviews. Landing Distance: 2393 ft: 729 m: Max Takeoff Weight: 6751 lbs: 3062 kg: Max Landing Weight: 6750 lbs: 3062 kg: Useful Weight: 2417 . To better manage fuel, a fuel computer was added to the list of available options. In 1973, an updated 414 was released with major changes, this model was named the 414II. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. Cowl flaps can be fully closed for cruise on even ISO +30 degrees F days, while the cylinders rarely go much over 400 degrees F. At full gross takeoff weight, I see normal 69 percent power cruise speeds in the 195 to 205 KTAS range in the flight levels. Cessna 414 Performance & Handling Cited as an excellent IFR platform, you'll 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. All rights reserved. There are only two fuel-. Optional auxiliary and locker tanks were available to boost usable capacity to 180 gallons, then to 203 gallons in 1973. The crosswind characteristics are good, and its easy to make squeaker landings. The other category that brings the price up to the same number are the aircraft that have undergone a RAM conversion. Answer: Wing loading is the total aircraft mass divided by its wing area. 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. Become a member and get exclusive access to articles, contests and more! 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. Its wings are borrowed from the Model 414. The 1973 to 1977s are the long bodies. The popularity of the aircraft ensures that there are enough aftermarket parts that can be bought if used parts are unavailable. With its bigger nose and lockers, the 414A can carry 1500 pounds. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. Total Cost of Ownership: $39,555.22 Given the popularity of the 414 series, its fair to say that if you need a modification, you can find it. In my Cessna 152, a 20-knot headwind increases the glide angle from 5 degrees to 7.5 degrees, a 50-percent increase. Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners. Answer: The process of delivering compressed, denser air to a combustion engine is referred to as forced induction. 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. } I cannot count the number of heater failures Ive suffered over the years and the number of maintenance folks who have done their best to help me. It is an approval granted to a parts manufacturer to manufacture specific aircraft components. 3,865. ( Down low under 10,000 feet, things are much slower, more like 170 to 175 KTAS. (2005, June 14). Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. 6,165: 6,165: SOURCE: Sources. Six seats were standard; a seventh was available as an option. With rare exception, all 414As have an aft potty. Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. Interested in buying this aircraft click here. 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 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. Rate of Climb: 1650 fpm; Climb Rate One Engine Inop: 315 fpm; Max Speed: 243 kts; Normal Cruise: 229 kts . fitness for any purpose is made or implied. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. 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. Distinguishing features are: retractable landing gear and three-bladed, constant speed, fully feathering propellers. Preferred Airparts, based in Ohio, provide worldwide customers with surplus new Cessna original components and used parts from dismantled aircraft. The maximum takeoff weight went up to 400 pounds to yield a higher useful load. It has a take-off distance of 665 meters and a landing distance of 718 meters. 1000 Prices range from low-hour models of 2,750 hours TTAF, selling for just over US$575,000, while older aircraft from the late-1970s are selling for approximately US$230,000. Fuel capacity 213-270. The aircraft was labeled the Chancellor in 1976. 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. The number of maintenance problems that can and do arise can cost a lot of money in a short time frame. Then in 1976, Cessna upgraded the engines to the newer -N series TSIO-520 offering a higher manifold pressure at 2700rpm, allowing the engines to maintain rated horsepower to 20,000 feet. The Achilles heel of the airplane for me has been the cabin heater. The main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. Cessna made more room for roughly 410 lbs (185 kg) baggage and equipment such as avionics by fitting on the nose of the 421 onto the 414A to which made the aircraft longer. no data Also, the big Cessnas have safety records that are unmatched by any other light twin./* custom css */ The system left room for error, not only on the part of the pilot, but among line personnel. 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-$400. However, thanks to GAMIjectors and the graphic engine monitor, I can set the fuels flows at 13 to 14 GPH (thats not a typo) at altitude, watch the TAS sink to 195 KTS and drive the aircraft for nearly seven hours. My flights range from an hour to four hours and while I have flown the airplane from coast to coast, I find trips of three hours or less are well suited for the airplane. text-align: left; Ball at 219-749-2520. I have owned a 1979 C414AW (a 414A with RAM winglets) for five years and about 2400 flight hours. Initial climb rate 1,700. STANDARD DATA: (T310R) Seats 4-6. Gross wt. Since 2017 he's been working as a content writer and loves that he can combine his love of aviation and writing here at Aviator Insider. Fuel capacity 202. 1200 This means the aircraft will burn around 17 gph (64 lph) per engine at 65% power and FL250, which is enough to get you cruising at around 202 KTAS (232 mph / 374 kmph). The pressure of the cabin is usually around 8,000 ft but can be less according to how the system is set up. Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. However, the eddy current method did not effectively identify the cracks until it was to the point where a load much lower than the published maximum load can cause catastrophic structural damage. Empty wt. Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: The displacement and power output remained the same, but the manifold pressure was increased from 36 hPa to 38 hPa. Cessna Country: United States Manufactured: 1972 to: 1984 ICAO: C340 Price: US$.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 by the manufacturer or FAA. Cessna Country: United States Manufactured: 1961 to: 1985 ICAO: C185 Price: US$.32 million (2019) Performance Weights Dimensions Avionics: Engine: 1x Continental IO-520-D Piston Power: 300 horsepower Max Cruise Speed: 145 knots 269 Km/h Approach Speed (Vref): 49 knots Travel range: 720 Nautical Miles 1,333 Kilometers Fuel Economy: Service Ceiling: The Cessna 414 Chancellor series gets high marks for its spacious dwelling, generous baggage space and favorable control response. Engines two 340-hp turbocharged Continentals. 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. It also has a TBO of 1,400 hours which is low even for a turbocharged engine. Cessna's 414 is among a large group of aircraft headed for extinction. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. Whats Going On with Cessna Denali Turboprop. PERFORMANCE: Top mph 268. 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. For 1981, Chancellor refinements included a heated fuel manifold, frost panes for cockpit side windows, and threadless-blade propellers. In the years following its introduction, the airplane saw few major changes. The big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte. It was developed to bridge the gap between the unpressurized Cessna 401 and the pressurized, more powerful Cessna 421. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. . Landing distance (50) 1,815. This AD has a compliance time of 400 to 800 total time. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. 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. It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. The Cessna 414 is an incredibly popular pressurized cabin-class twin, with almost 650 registered in the US alone. Federal Register. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads. ), 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. Other engine mods include a turboprop-powered conversion of the Cessna 414, named the Turbo Star Pressurized 414, using Allison 250-B17B engines, and the Thielert FADEC-controlled diesel Centurion piston engines that run on commonly available jet fuel. .tdi_115.td-a-rec{ Cessna Owner Organization. The exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. Retrieved October 7, 2021, from http://blog.overhaulbids.com/continental-overhaul-cost/continental-520-overhaul-cost/, Cox, B. Beginning in 1978, Cessna offered three basic equipment packages. Email Seller Video Chat. 3,467. The compressed air is then cooled down, which makes it denser, on its way to the cabin. The six- to seven-seat pressurized light transport is a step up for owners of the pressurized 340 and is fitted with the same 310-hp turbocharged engines. Stall mph cabin is separated from the passenger compartment by a divider. 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. .tdi_115.td-a-rec-img { Ceiling 26,000. 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. Winglets aid climb and cruise speeds. 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. 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. A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. The resale value increases greatly if a RAM conversion has been done and additional performance modifications have been fitted. The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. Cessna Chancellor III (414A) Guide & Specs, Cessna Chancellor (414A) Performance and Handling, Piper Mirage Guide and Specs: All You Need To Know. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads.The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. quantity indicators, both with three-position switches, to help the pilot keep track.