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Fuelburn: 34.0 GPH 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. Fuel burn is the same, 34 GPH in cruise at all altitudes, with the RAM VII at 69 percent. Also, corrosion on the engine frame rails is possible from exhaust leaks where the manifold exits into the turbocharger. 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. Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. Buyers should be looking carefully for compliance. 3,865. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. Otherwise, the periodicity is 1,600, or 200 hours depending on the mod state. The 414A can be upgraded with the usual performance boosters such as vortex generators, which are highly recommended. The same long-stroke, trailing-link landing gear common to all Citation jets allows the softest landings and smooth taxiing. text-align: left; 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. Fuel capacity 102-207. An engine rail replacement can cost an eye-watering $14,000. It has a take-off distance of 665 meters and a landing distance of 718 meters. The first Cessna Chancellor the 414 took to the skies in 1968, and was produced from 1970 onwards. The older 414s are known as the short-bodied models. All rights reserved. So newer, more powerful engines with stronger components and increased aerodynamics all of which boost performance greatly and increase the value. 3,467. He's worked on various aircraft from small two-seaters like Tomahawks or Boeing 767s. It is capable, comfortable, and performs well. All rights reserved. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. It featured major modifications, including a restructured and increased wingspan, incorporating integral fuel tanks, and a stretched nose to allow more space for baggage. The new engine also has a TBO of 2,000 hours, which is a 600-hour increase from stock. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. ), Please tell us: The aircraft can seat up to eight passengers and one or two crew. For the 414, the engines chosen were the 310hp TSIO-520-Js, with intercoolers and takeoffs for cabin bleed air pressurization. Its the third model in the Chancellor line and the successor to the Cessna 414II. Most accidents involve weather or overloading. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. 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. A simpler fuel system was among a host of improvements unveiled in 1978 with introduction of the Model 414A Chancellor. Loading must be watched carefully to avoid going out of the rear CG limit. Utility twin aircraft. - Aircraft specific reviews and articles. The factory tends to be much pricier than third-party garages that overhaul your engine. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. 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 414 was built using parts from other 400-series aircraft. Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. 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. Pilots with less experience can expect this range to rise to between 1,100 to 1,600 per year. } The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. However, it takes a longer distance high wing loading aircraft to takeoff and land. Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. PERFORMANCE: Top mph 268. In service since 1969. Above this speed, turbulence or rapid control deflections increase the chance of structural damage. 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. 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. Annual inspections, repairs and pre-buys must be conducted by specialists. CESSNA, V2 (IAS) All told, Cessna built nearly 1000 of the airplanes-roughly a 50/50 split between early tip-tanked 414s and wet-wing 414A Chancellors-during 16 years of production. These aircraft were called the 414 Chancellor. 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). 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. STANDARD DATA: (T310R) Seats 4-6. Answer: Maximum structural cruise, or Vno, refers to the airspeed above which the aircraft should be flown only in smooth air. Passengers love it for space, comfort, and low noise levels. 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. Training is a must. The model 414, a 411 derivative introduced in 1970, utilized the 421s fuselage and tail unit with the 401s wings. Stall mph cabin is separated from the passenger compartment by a divider. The efficiency of the 414As long high-aspect ratio wing is highlighted by noting the 414As single-engine service ceiling is 19,850 feet. Many supplemental type certificates exist for the aircraft that allow upgrades to improve performance. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. With rare exception, all 414As have an aft potty. It is our mission to be the go to leaders in the aviation industry. Maximum operating altitude of 30,800, a optimal cruise speed of 203 knots/234 MPH, and a 705 NM/811 SM seats-full range. 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 PERFORMANCE: Top mph 297. ( Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners. An STC is an approved modification to an aircraft, engine, or component. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. If the insurance includes additional hull cover for US$225,000, the annual premium for the experienced pilot will be between US$4,400 to US$5,800 per year, while the lesser experienced pilot can expect US$5,700 to US$12,000 per year. 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. Crew-6 Launch Scrubbed For Ground Systems Issue, The Drip, Drip Of Bad Publicity About 100LL. Although the 414s have a huge cabin-class interior, the stock airplane has never been a tremendous load hauler. m, MTOW 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: - STOL kits can also be purchased to help reduce the field length of the aircraft. Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. 2023 Madavor Media, LLC. The cabin length is 3.5 meters, height is 1.3 meters, and width is 1.4 meters. text-align: center; Maintenance costs vary from year to year, but $300 to $350 direct per hour is a good estimate for the 125 to 150 hours per year I fly. The engines on the 414II were upgraded to the newer Continental TSIO-520-Ns. However, single-engine performance at sea level is lower than the competition, with the aircraft only being able to climb 290 ft (88 m) per minute. This has made insuring a 414 tougher. Flight planning or any other aircraft operations should only be done using official technical information provided (2001, February 26). The figures show that the demand for Dakotas has increased causing prices to rise by about 40 percent. For 1981, Chancellor refinements included a heated fuel manifold, frost panes for cockpit side windows, and threadless-blade propellers. Though its Continental engines could maintain their rated power at higher altitudes, Cessna implemented manifold pressure limitations above 20,000 ft (6,096 m) to prevent excessive engine temperatures. With the O&N tanks in both nacelles, I can carry up to 260 gallons of fuel, good for over seven hours of endurance. Both were quick to praise the 414 and especially the 414A as the best of the Cessna piston twins, with good systems, particularly the hydraulic gear on the 414A. PERFORMANCE: Top mph 268. Owners of 414As can opt for the series V conversion, which includes Continentals 350-HP liquid cooled Voyager engines, which have a TBO of 2000 hours. BUILT FOR TRAINING Ideal for entry-level landings, the Skyhawk piston features a sturdy tricycle landing system and a resilient airframe. Answer: Pressurization is the creation of a false atmosphere in the cabin of the aircraft in order to allow us to breathe at higher altitudes without pure oxygen. The maximum takeoff weight went up to 400 pounds to yield a higher useful load. Cessna Country: United States Manufactured: 1972 to: 1984 ICAO: C340 Price: US$.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 Cessna 414 - AOPA - Aircraft Owners and Pilots Association 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. A direct competitor of the 414A is the Beechcraft King Air. The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. He received his training at the University of North Dakota and has been in love with aviation for many years. AOPA. The 414 and 414A truly provide a great family or business aircraft. 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. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Your email address will not be published. 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. 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. Cessna Skylane Loading must be watched carefully to avoid going out of the rear CG limit. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. We highly recommend them. Empty wt. The prototype, registered N7170C, first flew on 1 November 1968, and production aircraft were available in a number of optional seating arrangements and avionics packages. 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. The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. by the manufacturer or FAA. Take an early model 414 with -J engines and complete this upgrade to receive a 1600 hour TBO, up from the original 1400. Its wings are borrowed from the Model 414. 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 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: 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. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. To ensure the aircraft you are buying is airworthy and will be reliable in the future, spend a bit more on an in-depth inspection. [4] This involves the installation of FADEC-controlled aviation diesel piston engines that run on commonly available jet fuel. Copyright permission must be sought from EUROCONTROL. Answer: TBO means Time Between Overhaul, which is the manufacturers recommended running time, in hours or calendar time, before overhaul. Cruise mph 231. (2005, June 14). Takeoff distance (50) 2,220. Liability coverage covers damage caused by the aircraft, including passengers, while hull coverage covers damage to the aircraft itself. 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. NM, ROD The system left room for error, not only on the part of the pilot, but among line personnel. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. With 1000 pounds of fuel, the payload may be 400 to 600 pounds. In the early 414s, the main landing gear webbing is prone to cracking, requiring extensive rectification. Owners speak of the 414s smoothness, stability, and ease with which you can trim the aircraft out. Initial climbout increased by at least 200 FPM to more than 1000 FPM. The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. Kudos go to Cessna for rising to the occasion. With the first flight in 1968 and production in 1970, Cessna manufactured the 414 for 17 years, with almost 1100 shipped. I own a 1978 Cessna 414A which I acquired in 1989. Rate of Climb: 1650 fpm; Climb Rate One Engine Inop: 315 fpm; Max Speed: 243 kts; Normal Cruise: 229 kts . m. All data presented is only indicative and should not be used operationally. Description There are only two fuel-288quantity indicators, both with three-position switches, to help the pilot keep track. 110 Any part that isnt new is all overhauled from the turbocharger to the fuel pressure regulator. So before buying one, you should ensure that there is an AMT with experience on pressurized Cessna twins in your area. Less powerful, light and low cost model of CESSNA 421 Golden Eagle. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. However, there are a number of airworthiness directives (AD) and service bulletins that have been published over the years. Landing Distance: 3,170 ft (966 m) Maximum Operating Altitude 45,000 ft . Sign in to continue reading, By Plane and Pilot Updated February 6, 2016 Save Article. 414 Chancellor | Cessna Owner Organization Cessna 414 pressurized-turbocharged - Performance Data . - Send us pictures of your plane. Full fuel allows the Chancellor 414A to fly for roughly four and a half hours, IFR reserves included, and has enough load leftover to carry six standard passengers, and not a pound more. The aircraft also featured a 28V, negative ground, direct current electrical system charged by an alternator on each engine, and a 24V battery. According to Aircraftcostoperator.com, the average total hourly cost of operating a Cessna 414A is roughly $535. CESSNA 310 - Plane & Pilot Magazine They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. kt, Vat (IAS) 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 compressed air is then cooled down, which makes it denser, on its way to the cabin. 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. Membership in and attending the Twin Cessna Flyer Organizations Pilot Seminars should be required. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. Cessna 182 vs 185 Compared: Which Is Better? 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. The aircraft was labeled the Chancellor in 1976. Citation Longitude - Cessna 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. (n.d.). How much does it cost to fly: $683.19 per hour. Cessna 340 Specifications, Cabin Dimensions, Performance - GlobalAir.com Fuel capacity 202. FL Cessna 414 for sale - Specs and History - ADN - FindAircraft.com Go figure. ( When discussing 414s and 414As, one must speak correctly.

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