Best Range: 1106 NM 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. 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. So before buying one, you should ensure that there is an AMT with experience on pressurized Cessna twins in your area. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. Developed from the 310, it utilizes a similar landing gear and tail unit. The change allowed the engine to produce 310 hp (228 kW) at 2700 RPM from sea level to 20,000 ft (6,096 m). ( Chancellors are as roomy as 421B/Cs. The landing gear was replaced, using the simpler system from the Cessna 414. 16 Eight aircraft factors influence 414 resale plus many other economic factors. Among the most popular mods are the RAM Aircraft Corporation engine swaps. The exhaust system sees a great deal of heat and vibration, thus components wear out. B. C. (2015, July 13). Thielert has offered engine conversions using their Centurion Engines. The RAM IV struggled in the flight levels, especially in the summer. Im required to attend an approved school for recurrent training. 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). The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. 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. 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. by the manufacturer or FAA. Even with aging aircraft and occasional engine-related issues, the 414A offers a large cabin, the comfort and convenience of pressurization and the performance and safety of turbo charging. 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. Common are engine and aerodynamic modifications, including winglets. Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. The new engine also has a TBO of 2,000 hours, which is a 600-hour increase from stock. 2023 Madavor Media, LLC. The piping which directs the exhaust from the manifold to the turbo is also susceptible to cracking. Annual inspections, repairs and pre-buys must be conducted by specialists. 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. 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. The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks. Loading must be watched carefully to avoid going out of the rear CG limit. That resulted in cruise speeds of only about 180 to 185 KTAS up high. Propeller- to-fuselage clearance is more than 31 inches for a very quiet cabin. One of the most important came in 1973, when cabin length was increased 16 inches and a fifth side window was installed. Lightly loaded and at economic power settings, expect to get almost 1,300 nautical miles of range. However, there are a number of airworthiness directives (AD) and service bulletins that have been published over the years. 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. 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. The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. 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. Soaring Good Looks. 200 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. The longer fuselage now allowed for an eighth seat to be added as an option. Stall mph 82. Optional auxiliary and locker tanks were available to boost usable capacity to 180 gallons, then to 203 gallons in 1973.The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. Each engine spun a constant speed, three-blade McCauley propeller. They are the Cadillacs of the piston line, with attention having been paid to detail; even on an288airplane 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 big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte. However, a 414 RAM VI and VII can often have an excellent useful load with an impressive range/payload chart. 150 The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Answer: An aircrafts service ceiling is defined as the height at which the aircraft cannot climb at a rate greater than 100 feet per minute. With rare exception, all 414As have an aft potty. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. Its an $800 part.MODS, CLUBSAmong the most popular mods are the RAM Aircraft Corporation engine swaps. quantity indicators, both with three-position switches, to help the pilot keep track. Distances Balanced Field Length: 1780 ft Landing Distance: 2358 ft Performance Rate of Climb: 920 fpm Max Speed: 156 kts Normal Cruise: 147 kts Economy Cruise: 117 kts Cost per Hour: $ 220.95 Power Plant Engines: 1 Engine Mfg: Continental Engine Model: IO-520-F Marketplace Information Interested in buying this aircraft click here! Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. Given the age and systems on the 414, plenty of airworthiness directives need reviewing for compliance. Liability coverage covers damage caused by the aircraft, including passengers, while hull coverage covers damage to the aircraft itself. ( Cessna Chancellor III (414A) Guide & Specs, Cessna Chancellor (414A) Performance and Handling, Piper Mirage Guide and Specs: All You Need To Know. One pilot and typical 6 passengers in main cabin. 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. The Cessna 414 is an incredibly popular pressurized cabin-class twin, with almost 650 registered in the US alone. That is why an approval to modify them is classed as supplemental. The cabin length is 3.5 meters, height is 1.3 meters, and width is 1.4 meters. 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. 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. However, some years, unexpected maintenance can eat your lunch. kt, ROD 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. The Chancellor has a service ceiling of 30,800 feet and a maximum speed of 235 knots. In service since 1969. margin: 0 auto 0 0; 3,467. Average price for used aircraft CESSNA 414A is $344,804.81. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg. Distances Balanced Field Length: 2595 ft Landing Distance: 4000 ft Performance Rate of Climb: 1520 fpm Climb Rate One Engine Inop: 290 fpm Max Speed: 235 kts Normal Cruise: 203 kts Power Plant Engines: 2 Engine Mfg: Continental Engine Model: TSIO-520-NB Marketplace Information Interested in buying this aircraft click here! }@media (max-width: 767px) { All rights reserved. The 414 seats up to 6 passengers plus 1 pilot. Cessna's 414 is among a large group of aircraft headed for extinction. 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: The displacement and power output remained the same, but the manifold pressure was increased from 36 hPa to 38 hPa. Pay attention to the fuel system in tip-tanked 414s. VGs are also available from Micro Aerodynamics (www.microaero.com) and V/G Systems, phone 800-328-4629. Fuel transferred too early is pumped overboard. If followed carefully, a mechanic wont miss anything. Takeoff distance (50) 1,700. Model 414 seats up to 7 passengers and 1 pilot. It is powered by two wing-mounted 310hp (231kW) Continental TSIO-520-J horizontally opposed, six-cylinder engines. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. Engines two 375-hp turbocharged Continentals. Currently, David flies twin retractables, notably the Pa44 Seminole and Pa30 Twin Comanche. The greater the experience of the owner/pilot, the lower the premiums. And $34,235 for fixed costs such as insurance. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. Its an $800 part. 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 same long-stroke, trailing-link landing gear common to all Citation jets allows the softest landings and smooth taxiing. Stall mph 82. 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. Come join us! In 1979, the 402s received a new wing, with a 5 feet (1.5 m) greater span. Whats Going On with Cessna Denali Turboprop. ft/min, IAS The upgrade from the T310R came about because my family, including a dog, cannot all be wearing nosebags. Engines two 285-hp turbocharged Continentals. 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. With a range of approximately 2,200 nautical miles and a relative low cost, the Conquest II was an unparalleled aircraft in its time. The older 414s are known as the short-bodied models. Over its production run the number of 414s and 414As were evenly split, with 516 and 554 built, respectively. As has often been said, Cessna really got it right with the 414/414As. 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. 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. Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. It has a range of 1,328 nautical miles and a climb rate of 1,520 feet per minute. Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. Cessna Owner Organization. The length of the cabin was increased by 16 inches (40.64 cm), an extra window was installed, electronic propeller synchrophasing was made standard, and various ARC 400-series avionics equipment was included. 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. 310, Range Are COVID Vaccines Injuring Pilots? Landing distance (50) 1,790. Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. The remedy for this was increased visual inspections and the strengthening of the wing spars by adding spar straps. Engines two 340-hp turbocharged Continentals. It also has a TBO of 1,400 hours which is low even for a turbocharged engine. The Cessna Pilots Association, located at www.cessna.org, and the Twin Cessna Flyer, at www.twincessna.org. The engine is chock-full of new RAM components such as camshafts, cylinders, crankshaft, piston rods. Cessna 414A Ram V - TAKEOFF and LANDING (Short Flight) Evan Luft 29.3K subscribers Description 92K views 6 years ago Flying a Cessna 414A with Ram V liquid cooled engines! The more generic components such as filters, wheels, tires, and brakes are off the shelf and stocked by large aviation suppliers like Aircraft Spruce & Specialty or Wag Aero. The 414A has an excellent safety record for good reason. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. Cessna borrowed components from existing 400-series airplanes to come out in 1970 with a model to bridge the price gap between unpressurized and pressurized twins. Find more About Us here! Gross wt. Ceiling 27,400. 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.MAINTENANCEEnsuring 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.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. He received his training at the University of North Dakota and has been in love with aviation for many years. Operating Costs. With its bigger nose and lockers, the 414A can carry 1500 pounds. Winglets aid climb and cruise speeds. 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. 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. fitness for any purpose is made or implied. Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. 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. 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. Its wings are borrowed from the Model 414. The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. Takeoff distance (50) 2,175. Send feedback comments to the EUROCONTROL Training Institute. The gear system of the 414A is easy to maintain, with one spot to watch: When assembling the center bolt on the main landing gear scissors, the correct washers must be installed in the correct sequence or the bolt can pull out, allowing the main gear wheel to turn sideways. Pay attention to the fuel system in tip-tanked 414s.A simpler fuel system was among a host of improvements unveiled in 1978 with introduction of the Model 414A Chancellor. Ram also claims youll see an extra 5 takeoff manifold pressure, a 1900 fpm climb, 13 knots extra cruise speed, and a 415lb increase in useful load. Their parts may seem expensive, but they continue supporting us owners, and for that I am very willing to see them earn afair profit. A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. Answer: Maximum structural cruise, or Vno, refers to the airspeed above which the aircraft should be flown only in smooth air. One former owner even stated that anyone who says the aircraft is reliable is delusional. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. Takeoff distance (50) 2,010. (RVSM rules have generally limited 414s to 28,000 feet.) Production aircraft were accessible in several optional seating configurations and avionics packages. 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. 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. If Cessna Kit SK414-19-1 is incorporated, the inspection is due every 9,600 hours. Above this speed, turbulence or rapid control deflections increase the chance of structural damage. BUILT FOR TRAINING Ideal for entry-level landings, the Skyhawk piston features a sturdy tricycle landing system and a resilient airframe. 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. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. These aircraft were called the 414A Chancellor. 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. Crew-6 Launch Scrubbed For Ground Systems Issue, The Drip, Drip Of Bad Publicity About 100LL. https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). Distances Takeoff Distance: 2185 ft Balanced Field Length: 2595 ft Landing Distance: 4000 ft Performance Rate of Climb: 1900 fpm Climb Rate One Engine Inop: 325 fpm Max Speed: 240 kts Normal Cruise: 230 kts Economy Cruise: 210 kts Cost per Hour: $ 522.43 Power Plant Engines: 2 Engine Mfg: Continental Engine Model: TSIOL-550A The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. 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.Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. 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. When discussing 414s and 414As, one must speak correctly. (See page 25 for an abbreviated AD list.). Range 489-1,242. Total Cost of Ownership: $39,555.22 The Cessna 414 is a high-performance aircraft requiring regular and comprehensive maintenance, and if looked after and regularly updated, the aircraft will hold its own on resale. While bad quality procedures in Wichita back in 1979 had probably caused my problem, the current staff at Cessna really impressed me with their efforts to help save this 27-year-old ship. } ft/min, IAS )We spoke with Michael Cook and Todd Voshell who direct maintenance at Rapid Air, in Grand Rapids, Michigan, which has been operating 300 and 400 series Cessna twins for over 25 years. PERFORMANCE: Top mph 273. [1], In 1974, American Jet Industries built a turboprop-powered conversion of the Cessna 414, named the Turbo Star Pressurized 414, using Allison 250-B17B engines. kg, IAS Fuel capacity 102-207. Also says to increase landing distance by 45% (doesn't seem to make sense). 2023 GlobalAir.com. Another point of consideration for a 414 buyer is the SB/AD on the wing spar. RAM also makes winglets and vortex generators. These aircraft arent like the 172s. The Cessna 411, first delivered in 1965, was one of Wichitas first ventures into the airliner market. Absolutely the Right 414A RAM IV, This Aircraft is Impeccable and reflects the condition and attention to details that this owner has given N414EM with Only 20 Hours on each RAM Engine and 20 Hours.See More Details. 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. There are several good training programs available to help keep 414 pilots in top form, something we feel to be quite important as, while the accident rate is low, the accidents seem primarily to occur on amateur flown airplanes and involve judgment errors on the part of the pilot rather than anything wrong with the airplane.HISTORYCessna borrowed components from existing 400-series airplanes to come out in 1970 with a model to bridge the price gap between unpressurized and pressurized twins. The first Cessna Chancellor the 414 took to the skies in 1968, and was produced from 1970 onwards. The main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. Ive previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. Pressurization differential was increased to 5.0 PSI to enable the airplane to maintain cabin altitudes of 10,000 and 11,950 feet at cruising altitudes of 26,500 and 30,000 feet, respectively. Other modifications in 1978 included a longer nosecone, a redesigned undercarriage system, and an extended wing without the earlier tip tanks. The 414A, aka Chancellor, was introduced in model year 1978 with the last built in 1985. Ceiling 26,000. Straight 414s with only 310-HP standard engines or even with a 325-HP RAM Series IV conversion will often have low useful loads. 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: - Ball reports that the pressurization controller diaphragms only last for about five years and the cabin pressure dump switch on the right landing gear should be checked often as well. 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. The pressurized 414 was developed to appeal to owners of unpressurized, twin-engined aircraft, and was based on the fuselage of the Cessna 421 and used the wing design of the Cessna 401. The crosswind characteristics are good, and its easy to make squeaker landings. The 414A has a combined 620 hp (456 kW), however, takeoff acceleration might not be as neck-snapping as one would assume. 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. 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. PERFORMANCE: Top mph 268. 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 updated Chancellor abolished the original tip tanks in favor of a longer wet wing, benefitted from a lengthened fuselage, mounted an improved 5.0 psi pressurization system, and enjoyed a 400-pound heavier gross weight. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. Ceiling 26,000. Cessna 414 pressurized-turbocharged - Performance Data . 7,450. In airplane engines, turbochargers are popularly used to achieve forced induction.
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