7,450. 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 Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads. Cessna 414 - AOPA - Aircraft Owners and Pilots Association 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. 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 bigger turbochargers and intercoolers, much larger cowl flaps, new intake air scoops, and Scimitar props, the airplane becomes an entirely new animal within seconds of leaving the runway. (2005, June 14). 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. He received his training at the University of North Dakota and has been in love with aviation for many years. 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. They dedicated an engineer to my problem and working with my maintenance shop, they developed an approved repair for my wing, possibly saving the ship from the scrap yard! With a range of approximately 2,200 nautical miles and a relative low cost, the Conquest II was an unparalleled aircraft in its time. Americas owner-flown aircraft enthusiasts and active-pilot resource, delivered to your inbox! - Aircraft data that you believe is inaccurate or have specific experiences. 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. With the RAM IV, useful load is over 2100 pounds, which enables one to carry full fuel plus 900 pounds. text-align: center; Citation CJ4 Gen2 - Cessna We use cookies to help you get the best experience when using our website. 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). Handling is good, too. Engines two 285-hp turbocharged Continentals. So newer, more powerful engines with stronger components and increased aerodynamics all of which boost performance greatly and increase the value. The 414A, aka Chancellor, was introduced in model year 1978 with the last built in 1985. ft/min, IAS For the 414, the engines chosen were the 310hp TSIO-520-Js, with intercoolers and takeoffs for cabin bleed air pressurization. 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. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. One of the most important came in 1973, when cabin length was increased 16 inches and a fifth side window was installed. Why is the landing distance increased on grass runways? 3,467. The RAM VII changed all that. The mod is expensive, but in my case we found serious factory mis-drilled wing spar attachment holes that could have caused a spar failure at any time! 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. An AD that requires the propeller hubs to be filled with red indicator oil to make cracks more visible was also released. Empty wt. Give me one three-hour cross country with any new owner and hell be able to teach the system. Specs, range, speed, operating weights and performance for the Cessna 340 here. RAM also makes winglets and vortex generators. Range 568-1,322. The landing gear track was also increased by 4 feet (1.2 m). Buyers should be looking carefully for compliance. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. No warranty of Cruise Speed: 224 kts: Fuel Capacity: 102 gal: Stall Speed (dirty): 70 kts: Range: 1090 nm: Takeoff: Landing: Ground Roll: 1695 ft: Ground Roll 805 ft: Over 50 ft obstacle . 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. This AD has a compliance time of 400 to 800 total time. ( Gross wt. I have had my share of problems with turbos, turbo controllers, cylinders and cracked cases. During that period, I have exchanged two sets of engines (RAM IV), two props (one new set), two paint jobs, an interior and updated the avionics. According to Cessna, 4.2-psi cabin pressure differential could be maintained by either engine operating at 60 percent power. 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. Home > Aircraft Specs > Manufacturers > Cessna Aircraft > 414 pressurized-turbocharged Performance Information. Airworthiness Directives; Cessna Aircraft Company models 402C and 414A airplanes. 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. 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! This has made insuring a 414 tougher. The other category that brings the price up to the same number are the aircraft that have undergone a RAM conversion. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. This can be remedied by fitting the aircraft with speed brakes/spoilers or installing a liquid cooling system to the engines. Cessna 120 Guide and Specs : Is It Powerful Enough? 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. ft/min, IAS 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. The package that gives the 414A the most significant boost in performance is the series V upgrade. Also worth joining is the Cessna Pilots Association (www.cessna.org and 805-934-0493). It uses spent exhaust gases to run the compressor, which draws in and compresses clean air to deliver to the engine. 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. Are COVID Vaccines Injuring Pilots? By all accounts, vortex generators reduce Vmc and stall speeds. Stall mph 82. Range 489-1,242. Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. Each model has different after-market engine/prop conversions and when other performance-enhancing modifications are factored in, weights and other performance criteria vary. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. 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. Its a combination of the airstair door, large cabin, air conditioning, abundant baggage space, large picture windows, pressurization and -not to be discounted-the potty! All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. 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. Baggage capacity of the 414 is 930 pounds, and cabin seating is available with an array of executive options. Answer: TBO means Time Between Overhaul, which is the manufacturers recommended running time, in hours or calendar time, before overhaul. Range 506- 1,325. Special Missions. Loading must be watched carefully to avoid going out of the rear CG limit. 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. 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. kts, ROC Cessna 180 Skywagon: Legendary popularity - AOPA 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. With the same fuselage as the 421, the 414 was roomy with huge baggage space. 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. However, most owners report that after a few hours of flying, it requires little thought. Pricing ( Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. Would like to understand why. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. Thus, it is an indication of age and use. 800 2023 Madavor Media, LLC. 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.Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. Insurance costs have equaled $7000 per year for the last couple of years for $1 million smooth with a hull value of $350,000. (See www.ramaircraft.com.). 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. Interested in buying this aircraft click here. Precise Flight and Spoilers, I. Auxiliary fuel pumps were placed outside the tanks, while the fuel flow gauge together with the fuel quantity gauge and the fuel low-level warning light is in the cockpit. . 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. 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. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. It's the third model in the Chancellor line and the successor to the Cessna 414II. kts, ROC Faster aircraft generally have a higher wing loading as less area is required to carry the same mass. With rare exception, all 414As have an aft potty. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. Bombardier Global 8000 Guide and Specs: Superior Sonic Transportation, Embraer Legacy 450 Guide and Specs: The Stepping Stone, Bombardier Challenger 300 Guide and Specs. These can be purchased by Sierra Industries. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. The Cessna 340 produced by Cessna. no data The pressurization and turbocharged nature of the aircraft mean it is complicated to work on, and specialization is needed. 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. A typically equipped 414A has a full-fuel payload of about 500 to 700 pounds, depending on equipment. The first Cessna Chancellor the 414 took to the skies in 1968, and was produced from 1970 onwards. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. 1200 Lots of external baggage in the nose and wing lockers, a pressurized aft cabin baggage area for desired in-flight items, like food, toys/games, cosmetics and a roomy pressurized 6000-foot cabin at 20,000 feet. 100 PERFORMANCE: Top mph 273. 6,200: 6,430: Zero Fuel Weight - lbs. Answer: Wing loading is the total aircraft mass divided by its wing area. 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. Liability coverage covers damage caused by the aircraft, including passengers, while hull coverage covers damage to the aircraft itself. Plane and Pilot expands upon the vast base of knowledge and experience from aviations most reputable influencers to inspire, educate, entertain and inform. Quality initial and recurrent training is critical. . CESSNA 414 Aircraft For Sale - 33 Listings | Controller.com 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. 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. I use SimCom. }.tdi_115.td-a-rec-img{ The 414 was meant to attract customers looking to upgrade from their unpressurized twin-engined aircraft and did so with limited success. 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. - Aircraft specific reviews and articles. Fuel transferred too early is pumped overboard. Even though Cessna Chancellor 414A has a good safety record, the earlier 414s and their complicated fuel system have caused a few scares, the most recent one in 2018. With the O&N tanks in both nacelles, I can carry up to 260 gallons of fuel, good for over seven hours of endurance. Cessna 414A RAM Specifications, Cabin Dimensions, Performance All aircraft, engines, and components have type certificates that approve their use. The aircraft is powered by two Continental TSIO-520-NB piston engines. 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. Fuselage strakes improve yaw control, performance in turbulence, and a higher cruise speed. 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. 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. Landing Distance: 2393 ft: 729 m: Max Takeoff Weight: 6751 lbs: 3062 kg: Max Landing Weight: 6750 lbs: 3062 kg: Useful Weight: 2417 . 180 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. It has a range of 1,328 nautical miles and a climb rate of 1,520 feet per minute. The 414 was built using parts from other 400-series aircraft. Ceiling 26,180. As has often been said, Cessna really got it right with the 414/414As. With its bigger nose and lockers, the 414A can carry 1500 pounds. Take an early model 414 with -J engines and complete this upgrade to receive a 1600 hour TBO, up from the original 1400. Bombardier Challenger 350 Guide and Specs: Is It Up to the Challenge? Continental also published overhaul procedures to enable -NB engines to get the TBO boost. Also says to increase landing distance by 45% (doesn't seem to make sense). Its an $800 part.MODS, CLUBSAmong the most popular mods are the RAM Aircraft Corporation engine swaps. 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. FL The Achilles heel of the airplane for me has been the cabin heater. (RVSM rules have generally limited 414s to 28,000 feet.) Best Range: 1106 NM 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. Description However, only upon acquiring the 414 did I finally attain my goal-virtually complete independence from the airlines for domestic travel. Cessna 414/414A Speed, Style, Class - AVweb A 414A RAM Series VII with Winglets (AW) will compete in many ways with a 421C. Initial climb rate 1,900. no data If Cessna Kit SK414-19-1 is incorporated, the inspection is due every 9,600 hours. Find more About Us here! Landing distance (50) 1,815. Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners.Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. Takeoff distance (50) 2,010. EASY ACCESS Two large cabin doors allow for convenient entry and loading for student and instructor. Overall, the 414A is a capable aircraft. At 11,350 feet, the 414s single-engine service ceiling was a bit below average; but, at 19,850, the 414A is tops in its class.Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. Pilots with less experience can expect this range to rise to between 1,100 to 1,600 per year. Landing distance (50) 1,790. The Cessna 414 Chancellor series gets high marks for its spacious dwelling, generous baggage space and favorable control response. It can carry up to 8 passengers and baggage, or full fuel, but not both. The aircraft also featured a 28V, negative ground, direct current electrical system charged by an alternator on each engine, and a 24V battery. However, there seem to be plenty that are not. Seating is spacious and available in a variety of arrangements. Cessna 340 - AOPA - Aircraft Owners and Pilots Association 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. No warranty of Cessna 414 Specifications, Cabin Dimensions, Performance - GlobalAir.com The switch for that light is on the underside of a Tee fitting in the pressure line to the tail and thus fills with water, rust and crud and should be pulled and cleaned periodically, or it will fail. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. kts, Distance I bought it to replace a nice Cessna T310R, which I flew for about a year. The 1973 to 1977s are the long bodies. Loading must be watched carefully to avoid going out of the rear CG limit. (Beginning in 1957, horsepower was modestly increased to 230.) margin: 0 auto 0 0; Fuel cost per hour: Optional auxiliary and locker tanks were available to boost usable capacity to 180 gallons, then to 203 gallons in 1973. 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). 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. That said, the aircraft is not a great load lifter, stack in the people, and theyd better have no baggage and be wishing to travel only short hops. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. Common are engine and aerodynamic modifications, including winglets. In my Cessna 152, a 20-knot headwind increases the glide angle from 5 degrees to 7.5 degrees, a 50-percent increase. In a study of accident records some years ago, the 414 stood out as the safest light twin. 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.Beginning in 1978, Cessna offered three basic equipment packages. Given the popularity of the 414 series, its fair to say that if you need a modification, you can find it. The system left room for error, not only on the part of the pilot, but among line personnel. According to Cessna, 4.2-psi cabin pressure differential could be maintained by either engine operating at 60 percent power. The engine is chock-full of new RAM components such as camshafts, cylinders, crankshaft, piston rods. The remedy for this was increased visual inspections and the strengthening of the wing spars by adding spar straps. Cruise mph 277. Total Cost of Ownership: $39,555.22 The 16 inches of extra length and the added side window do not directly mean much, but short-bodied 414s rarely have the typical cabin-class size refreshment center nor a potty. Cessna 402 - Wikipedia Therefore, finding parts to support the aircraft is not difficult. RAM also makes winglets of their own design for the 414A to improve its aerodynamic performance. Controls consisted of on/off/crossfeed valves and a fuel flow computer/indicator was added. Fuel capacity 213-270. It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. [2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]. However, almost all owners complain about the maintenance, and most say that the low acquisition cost of the aircraft will be offset by the cost of maintenance a few years down the line. 5 Ceiling 27,400. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. The Chancellor utilizes the hydraulic components of the Golden Eagle gear and features a five-second retraction time. Passengers love it for space, comfort, and low noise levels. AOPA. Checking the Cessna 152 POH it says to increase takeoff distance by 15% of ground roll (makes sense due to increased friction). Landing distance over 50-ft obstacle: 2,393 ft: Landing distance, ground roll: 1,013 ft: Limiting and . 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. Engines two 340-hp turbocharged Continentals. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. Approaching and landing with minimal power is a good habit. Many of which have been addressed by ADs and service bulletins. When we look at the power loading of the aircraft, the why becomes obvious: weight. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. However, it takes a longer distance high wing loading aircraft to takeoff and land. 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.
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