It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. Range 489-1,242. Come join us! Landing distance (50) 1,765. . Therefore, finding parts to support the aircraft is not difficult. When we look at the power loading of the aircraft, the why becomes obvious: weight. 6,165: 6,165: SOURCE: Sources. Interested in buying this aircraft click here. The 1970 to 1972 models are referred to as short-bodied 414s. Fuel capacity 202. 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. However, a 414 RAM VI and VII can often have an excellent useful load with an impressive range/payload chart. 3,467. 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 After the Chancellor debuted, there were few further refinements. The exhaust system sees a great deal of heat and vibration, thus components wear out. 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. STANDARD DATA: (T310R) Seats 4-6. Approaching and landing with minimal power is a good habit. As with all Twin Cessna's, the landing gear and exhaust systems must be maintained properly. PERFORMANCE: Top mph 297. 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. (RVSM rules have generally limited 414s to 28,000 feet.) The system left room for error, not only on the part of the pilot, but among line personnel. 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! 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. Cessna 414 chancellor. Ball at 219-749-2520. text-align: center; Derived from the Model 411, the Cessna 401 and 402 are essentially the same aircraft put to two different uses. 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. 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. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. The Chancellors that cost close to $500,000 most often are pristine and like-new. 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. Over its production run the number of 414s and 414As were evenly split, with 516 and 554 built, respectively. The maximum takeoff weight went up to 400 pounds to yield a higher useful load. The older 414s are known as the short-bodied models. Gross wt. kts, Distance Required fields are marked *. PERFORMANCE: Top mph 273. 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. [2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]. Of course, any airplanes safety depends a great deal on the proficiency of its pilots. Model 414 seats up to 7 passengers and 1 pilot. 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. Twin engine piston aircraft with retractable landing gear. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. Stall mph 81. The number of maintenance problems that can and do arise can cost a lot of money in a short time frame. ft/min, IAS Oh, and the aft toilet. Also, the big Cessnas have safety records that are unmatched by any other light twin. Down low under 10,000 feet, things are much slower, more like 170 to 175 KTAS. Balloons And Runway Calamities: Why Wait To Panic? 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. Pay attention to the fuel system in tip-tanked 414s. No warranty of All rights reserved. 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. 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. Purchasing a Cessna 414A is considered to be cheap for the number of airplanes you get. Seating is spacious and available in a variety of arrangements. Its the third model in the Chancellor line and the successor to the Cessna 414II. 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 Chancellor has a service ceiling of 30,800 feet and a maximum speed of 235 knots. One of our Planephd Experts will be in touch with you shortly. 2023 GlobalAir.com. An AD that requires the propeller hubs to be filled with red indicator oil to make cracks more visible was also released. The aircraft was labeled the Chancellor in 1976. By all accounts, vortex generators reduce Vmc and stall speeds. 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. Whats Going On with Cessna Denali Turboprop. Interested in buying this aircraft click here. 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. Plane and Pilot expands upon the vast base of knowledge and experience from aviations most reputable influencers to inspire, educate, entertain and inform. https://www.federalregister.gov/documents/2005/06/14/05-11613/airworthiness-directives-cessna-aircraft-company-models-402c-and-414a-airplanes, Cessna 414. }googletag.cmd.push(function() { googletag.display('inline'); });288All 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. Landing distance (50) 1,850. kg, IAS One of the most important came in 1973, when . (See page 25 for an abbreviated AD list. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. In the years following its introduction, the airplane saw few major changes. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. 230 FL Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. Answer: The process of delivering compressed, denser air to a combustion engine is referred to as forced induction. Eight aircraft factors influence 414 resale plus many other economic factors. Phone: (305) 342-0760. 16 Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. 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. For the 414, the engines chosen were the 310hp TSIO-520-Js, with intercoolers and takeoffs for cabin bleed air pressurization. However, it isnt just an engine swap. They can be purchased from Micro Aerodynamics and VG Systems. Empty wt. Description With its bigger nose and lockers, the 414A can carry 1500 pounds. The 414 and 414A truly provide a great family or business aircraft. . Takeoff distance (50) 2,010. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. (See www.ramaircraft.com. For example, the 414 may be powered by a standard 310-HP engine, a 325-HP RAM Series IV or a 335-HP RAM VI or VII. Most had the RAM VI engine conversion. by the manufacturer or FAA. The 414 was built using parts from other 400-series aircraft. However, some years, unexpected maintenance can eat your lunch. [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. The applications are smaller and they have maintenance issues, so the price does fall. According to Cessna, 4.2-psi cabin pressure differential could be maintained by either engine operating at 60 percent power. Fuel transferred too early is pumped overboard. Already a member? PERFORMANCE: Top mph 268. 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 Cessna 414 is an incredibly popular pressurized cabin-class twin, with almost 650 registered in the US alone. For the same liability coverage amount, pilots who dont meet the above criteria can expect to pay $1,100-$1,600 per year, and the cost increases to $5,700-$12,000 when hull coverage is brought in. 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 factory tends to be much pricier than third-party garages that overhaul your engine. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. This plane was. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). The same long-stroke, trailing-link landing gear common to all Citation jets allows the softest landings and smooth taxiing. I bought it to replace a nice Cessna T310R, which I flew for about a year. Ceiling 29,800. Passengers love it for space, comfort, and low noise levels. The Chancellor 414A has an impeccable safety record. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. Annual inspections, repairs and pre-buys must be conducted by specialists. 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. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. There are several problems that the 414A has. 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. The prices range from low-hour models with less than 4,000 hours TTAF, which are selling for just over US$385,000, while older aircraft from the early-1970s will sell for approximately US$150,000. Power. Straight 414s with only 310-HP standard engines or even with a 325-HP RAM Series IV conversion will often have low useful loads. 180 Total Cost of Ownership: $39,555.22 In a study of accident records some years ago, the 414 stood out as the safest light twin. Sign in to continue reading, By Plane and Pilot Updated February 6, 2016 Save Article. 5,500. fitness for any purpose is made or implied. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. Range 1,284. Cabin specifications: 04'03" cabin high, 04'07" cabin wide, and 11'03" cabin long. The aircraft has a remarkably high service ceiling of 30,800 ft (9387 m), but the normal operating range of a 414A is between 15,000 ft (4572 m) and FL250 (7,620 m). However, it takes a longer distance high wing loading aircraft to takeoff and land. The aircraft factors are: These terms are all within the control of the owner. Thielert claims increased power and improved fuel economy over other available conventional piston engines. I have owned and flown a 1979 Cessna 414A for 14 months, accumulating 235 hours in all sorts of conditions. The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. The pressurized comfort of the 414A, which produces an 8000-foot cabin at 22,800 feet, cannot be overemphasized. Home > Aircraft Specs > Manufacturers > Cessna Aircraft > 414 pressurized-turbocharged Performance Information. 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. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. The calculation is made by assuming the aircraft is operated for 450 hours annually, during which fuel costs $5 a gallon bringing total fuel costs to $2,250 a year. The landing gear is the standard electromechanical system that is on all tiptank twin Cessnas. kt, Distance Stall mph 82. Ceiling 26,180. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. 2023 GlobalAir.com. 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. I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. 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. Average price for used aircraft CESSNA 414A is $344,804.81. 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. 110 All data presented is for entertainment purposes and should not be used operationally. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. The fuselage and tail were essentially the same as the ones used on the 421B, while the wings were taken from the 401. Liability coverage covers damage caused by the aircraft, including passengers, while hull coverage covers damage to the aircraft itself. It can carry up to 8 passengers and baggage, or full fuel, but not both. Landing distance (50) 1,790. Mandatory power reductions during the climb above FL220 meant long climb times and getting above FL250 seemed to take forever at the 200 FPM climb rate that could be achieved up there. 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. ( 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 Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. fitness for any purpose is made or implied. The pressurization and turbocharged nature of the aircraft mean it is complicated to work on, and specialization is needed. 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. Cessna 182 vs 185 Compared: Which Is Better? One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. Send feedback comments to the EUROCONTROL Training Institute. Bringing the grand annual total to $240,785. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. 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. 5 .tdi_115.td-a-rec{ STANDARD DATA: ( 411) Seats 6-8. STANDARD DATA: (411) Seats 6-8. Many supplemental type certificates exist for the aircraft that allow upgrades to improve performance. Some low-time pilots might be approved for 340 insurance, but rejected for a 414/414A. The standard aviation insurance all aircraft owners take is liability coverage, while hull coverage is optional. Are COVID Vaccines Injuring Pilots? If an owner has taken a maintenance only as required approach to their aircraft, they can expect a far lower resale value. A direct competitor of the 414A is the Beechcraft King Air. To better manage fuel, a fuel computer was added to the list of available options. 3060 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. text-align: center; }.tdi_115 .td-element-style{ According to Hangar 67, a very high-time 1979 model year 414A was recently sold at $129,900, which is the lowest price we have found. margin: 0 auto 0 0; Pilots with less experience can expect this range to rise to between 1,100 to 1,600 per year. Fuel cost per hour: 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. In addition, the Chancellors wet wing has an increased fuel capacity of 106 gallons of usable fuel. 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. Landing Distance: 3,170 ft (966 m) Maximum Operating Altitude 45,000 ft . Above this speed, turbulence or rapid control deflections increase the chance of structural damage. Remained in production until 1985. The Cessna 414 Chancellor was produced from 1968 to 1985. Gross wt. Fuel transferred too early is pumped overboard. 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. 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. There were significant changes made to the body of Chancellor 414A as well. Arguably the most popular engine mod youll see on used aircraft is the engine upgrade to 335 hp offered by Ram Aircraft atwww.ramaircraft.com. Please send us your experiences on your aircraft. With its bigger nose and lockers, the 414A can carry 1500 pounds. Copyright permission must be sought from EUROCONTROL. In 1978, an enhanced version was launched, designated as the 414A Chancellor. Initial climb rate 1,900. Engines two 340-hp turbocharged Continentals. The engine is notorious for cracked cylinders and therefore requires periodic inspections. 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. Kudos go to Cessna for rising to the occasion. Airworthiness Directives; Cessna Aircraft Company models 402C and 414A airplanes. The Chancellor replaced the former 414 in 1978 and offered a new level of payload performance, range, and fuel efficiency. Six seats were standard; a seventh was available as an option. Other modifications in 1978 included a longer nosecone, a redesigned undercarriage system, and an extended wing without the earlier tip tanks. 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. So, if its just pressurization youre looking for and youre going to be flying with only another person or two aboard, you might want to look at the 340 for a personal hot rod.A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). Range 1,284. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. 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. }.tdi_115.td-a-rec-img{ m, MTOW There are four options, all of which provide a sizable increase in horsepower, increase the TBO, and newer, more powerful propellers. 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. BUILT FOR TRAINING Ideal for entry-level landings, the Skyhawk piston features a sturdy tricycle landing system and a resilient airframe. 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. Training is a must. The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. Stall mph 82. 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. 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.Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. As has often been said, Cessna really got it right with the 414/414As. The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. Currently, David flies twin retractables, notably the Pa44 Seminole and Pa30 Twin Comanche. Maximum operating altitude of 30,800, a optimal cruise speed of 203 knots/234 MPH, and a 705 NM/811 SM seats-full range. Accident statistics suggest that no common threads are pointing to the system or design problems on the 414. Top mentions include the true cabin class, reasonable cruise speed, and maintenance of sea-level pressure to 10,000 feet. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. 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! According to Aircraftcostoperator.com, the average total hourly cost of operating a Cessna 414A is roughly $535. It is a less powerful and lighter evolution of the Cessna 421. 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. Cruise mph 231. Thus, it is an indication of age and use. 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. If followed carefully, a mechanic wont miss anything. Owners recommend two groups. 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 . 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. Four variations are available, all of which offer a boost in useful load, increased TBOs and new props. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. The 414A, aka Chancellor, was introduced in model year 1978 with the last built in 1985. (See www.ramaircraft.com.). Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. 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. 1000 We highly recommend them. 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 414 is a low-wing cantilever monoplane with a conventional tail section and a retractable tricycle undercarriage. Its an excellent idea, regardless of how much time you have.
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