Another area that needs to be checked for corrosion is the firewall. It has a service ceiling of 14,700 feet and a climb rate of 715 feet per minute. Fuel cost per hour: Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. When we're not in the air, we're here helping others how to join us here at Aviator Insider. These aircraft were called the 414 Chancellor. 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. RAM also makes winglets and vortex generators. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. Accident statistics suggest that no common threads are pointing to the system or design problems on the 414. No warranty of Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor. Once it reaches the cabin it is compressed enough to create an atmospheric pressure that mimics the desired altitude. 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. Chancellors are as roomy as 421B/Cs. The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. Cessna Country: United States Manufactured: 1978 to: 2006 ICAO: C550 Price: US$1.1 million (2019) Performance Weights Dimensions Avionics: Garmin 700 Engine: 2x Pratt & Whitney Canada JT15D-4B Turbofan Power: 2,500 pound-force Max Cruise Speed: 403 knots 746 Km/h Approach Speed (Vref): 82 knots Travel range: 2,000 Nautical Miles 3,704 Kilometers I bought it to replace a nice Cessna T310R, which I flew for about a year. Of course, any airplanes safety depends a great deal on the proficiency of its pilots. The 340 has a gross weight of 5,975 pounds, and an empty weight of 3,697 pounds. One former owner even stated that anyone who says the aircraft is reliable is delusional. Buyers should be looking carefully for compliance. One of the most important came in 1973, when cabin length was increased 16 inches and a fifth side window was installed. It is a less powerful and lighter evolution of the Cessna 421. If Cessna Kit SK414-19-1 is incorporated, the inspection is due every 9,600 hours. The main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. Eight aircraft factors influence 414 resale plus many other economic factors. They offer technical help and forums for members to discuss everything and anything about their aircraft. The Piper Seneca is also quite similar to the 414A, even though it is slightly smaller. 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. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. The 375-HP 421Cs single engine ceiling is 14,900 feet. Many of which have been addressed by ADs and service bulletins. Currently, David flies twin retractables, notably the Pa44 Seminole and Pa30 Twin Comanche. I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. To better manage fuel, a fuel computer was added to the list of available options. 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! There are several problems that the 414A has. While arguments rage today over whether the 414 or the 421 is the better aircraft, theres no doubt that with the 414, Cessna produced a comfortable, roomy, and stylish aircraft for personal and corporate travel. 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. Range 506- 1,325. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. Also worth joining is the Cessna Pilots Association (www.cessna.org and 805-934-0493). The standard aviation insurance all aircraft owners take is liability coverage, while hull coverage is optional. It is capable, comfortable, and performs well. Save my name, email, and website in this browser for the next time I comment. 2023 GlobalAir.com. (See www.ramaircraft.com.). Cruise mph 223. 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. It is our mission to be the go to leaders in the aviation industry. Loading must be watched carefully to avoid going out of the rear CG limit. Down low under 10,000 feet, things are much slower, more like 170 to 175 KTAS. Annual inspections, repairs and pre-buys must be conducted by specialists. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. PERFORMANCE: Top mph 268. 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. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. The STANDARD DATA: Seats 6-8. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. ( 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. With rare exception, all 414As have an aft potty. Come join us! The remedy for this was increased visual inspections and the strengthening of the wing spars by adding spar straps. Interested in buying this aircraft click here. 414 Chancellor | Cessna Owner Organization All rights reserved. Flight planning or any other aircraft operations should only be done using official technical information provided https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). If followed carefully, a mechanic wont miss anything. Total Cost of Ownership: $39,555.22 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. He received his training at the University of North Dakota and has been in love with aviation for many years. Some potties have a flushing feature. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. Stall mph 82. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. 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. (See page 25 for an abbreviated AD list. Take an early model 414 with -J engines and complete this upgrade to receive a 1600 hour TBO, up from the original 1400. The pressurization and turbocharged nature of the aircraft mean it is complicated to work on, and specialization is needed. The first Cessna Chancellor - the 414 - took to the skies in 1968, and was produced from 1970 onwards. By continuing to use this website, you are agreeing to our Cookie Policy. That resulted in cruise speeds of only about 180 to 185 KTAS up high. Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. The RAM IV struggled in the flight levels, especially in the summer. Finding replacement parts for a 414A is not as tough as one would think thanks to its shared parts with the 401 and 421. 3,865. Empty wt. Ball at 219-749-2520. 3060 A brand new engine exchange from Continental costs an average of $60,000. 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. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); WORLD'S PREMIER INDEPENDENT AVIATION NEWS RESOURCE. Smart design means a better ride. no data 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. However, owners should expect depreciation, and the price to decrease over time. Bombardier Challenger 350 Guide and Specs: Is It Up to the Challenge? 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 system left room for error, not only on the part of the pilot, but among line personnel. . It did away with the extremely complicated and troublesome fuel system of the previous generations and replaced it with wet-wing fuel tanks that were 4.50 ft (1.37 m) longer and held 213 gal (968 l) total. 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. The aircraft was labeled the Chancellor in 1976. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. The 414A has a combined 620 hp (456 kW), however, takeoff acceleration might not be as neck-snapping as one would assume. The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks. Go figure. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. The 401, introduced in 1966 and discontinued in 1972, was basically designed as a medium to . 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. }@media (max-width: 767px) { Would like to understand why. Handling, range, speed and fuel economy, and hourly costs are often considered to be at or exceeding the industry standard. Developed from the 310, it utilizes a similar landing gear and tail unit. Required fields are marked *. Takeoff distance (50) 2,175. STANDARD DATA: (T310R) Seats 4-6. Aerodynamic mods include vortex generators to increase aileron and rudder control authority at low speeds. 6,200: 6,430: Zero Fuel Weight - lbs. On November 1, 1968, the prototype registered N7170C, conducted its maiden flight. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. The 421B tiptank twin Cessna has fuel carried in the mains (tips), auxiliary fuel cells in the wings and optional nacelle tanks. They can be purchased from Micro Aerodynamics and VG Systems. Pay attention to the fuel system in tip-tanked 414s. Answer: TBO means Time Between Overhaul, which is the manufacturers recommended running time, in hours or calendar time, before overhaul. 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. And $34,235 for fixed costs such as insurance. In 1973 Cessna stretched the fuselage by 16 inches and added a fifth side window. 110 Heres an even more interesting thing-normally, the RAM engines want to gulp down 19 to 22 GPH a side at higher power settings. 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. Another point of consideration for a 414 buyer is the SB/AD on the wing spar. - Features that would be useful to you. 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. ) kts, ROC (n.d.). Maximum operating altitude of 30,800, a optimal cruise speed of 203 knots/234 MPH, and a 705 NM/811 SM seats-full range. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. I use SimCom. As we saw earlier, average prices sit between US$230,000 to US$280,000, yet highly modified and maintained aircraft command twice those figures. With the RAM IV, useful load is over 2100 pounds, which enables one to carry full fuel plus 900 pounds. }.tdi_115.td-a-rec-img{ [4] This involves the installation of FADEC-controlled aviation diesel piston engines that run on commonly available jet fuel. As far as handling goes, owners have reported that it is a stable aircraft that behaves in a very neutral manner and reacts to control inputs predictably. kts, ROC 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. PDF Flight Safety Foundation The resale value increases greatly if a RAM conversion has been done and additional performance modifications have been fitted. Derived from the Model 411, the Cessna 401 and 402 are essentially the same aircraft put to two different uses. PERFORMANCE: Top mph 297. Cessna 340 - Price, Specs, Photo Gallery, History - Aero Corner Cessna 340 Specifications, Cabin Dimensions, Performance - GlobalAir.com Ceiling 29,800. When pilots are flying IFR, it means they are under the control of Air Traffic Control. ft/min, TAS When discussing 414s and 414As, one must speak correctly. 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. 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. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). 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. 16 200 Cessna 414 Specifications, Cabin Dimensions, Performance - GlobalAir.com fitness for any purpose is made or implied. Pricing Fuel capacity 213-270. The fuel economy of the 414A depends on the altitude, conditions, and power setting, but the general specific fuel consumption is approximately 0.44 lbs/hp/hr. 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. Landing Distance: 4000 ft; Performance. 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. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. The air is run through a compressor connected to the intake manifold of the engine to create a more efficient fuel burn which will eventually produce more power. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. Cessna Citation II (550) - Price, Specs, Photo Gallery, History - Aero . 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. One pilot and typical 6 passengers in main cabin. The figures show that the demand for Dakotas has increased causing prices to rise by about 40 percent. 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). So before buying one, you should ensure that there is an AMT with experience on pressurized Cessna twins in your area. 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. 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. Based on 450 hours a year and fuel cost at $5.00 per-gallon, the CESSNA 414A has total variable costs of $233,550.00, total fixed costs of $73,885.00, and hypothetical summary cost of $307,435.00. Continental also published overhaul procedures to enable -NB engines to get the TBO boost.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). As has often been said, Cessna really got it right with the 414/414As. The 414 was meant to attract customers looking to upgrade from their unpressurized twin-engined aircraft and did so with limited success. CESSNA 310 - Plane & Pilot Magazine The exhaust system sees a great deal of heat and vibration, thus components wear out. . }.tdi_115 .td-element-style{ 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. The package that gives the 414A the most significant boost in performance is the series V upgrade. For 1981, Chancellor refinements included a heated fuel manifold, frost panes for cockpit side windows, and threadless-blade propellers. If an owner has taken a maintenance only as required approach to their aircraft, they can expect a far lower resale value. Answer: IFR means Instrument Flight Rules. The 1970 to 1972 models are referred to as short-bodied 414s. As with all Twin Cessna's, the landing gear and exhaust systems must be maintained properly. Cessna 120 Guide and Specs : Is It Powerful Enough? 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! I own a 1978 Cessna 414A which I acquired in 1989. All rights reserved. I have had my share of problems with turbos, turbo controllers, cylinders and cracked cases. Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: To get at the fuel in the wing locker tanks, it must first be transferred to the mains. Stall mph cabin is separated from the passenger compartment by a divider. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. As an Amazon Associate I earn from qualifying purchases. 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. ft/min, IAS Cessna 414 Guide and Specs : Is It High Performance? The Chancellor replaced the former 414 in 1978 and offered a new level of payload performance, range, and fuel efficiency. 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. Distinguishing features are: retractable landing gear and three-bladed, constant speed, fully feathering propellers. 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. The new engine also has a TBO of 2,000 hours, which is a 600-hour increase from stock. When we look at the power loading of the aircraft, the why becomes obvious: weight. Given the popularity of the 414 series, its fair to say that if you need a modification, you can find it. Coupled with smaller engines than the 421, you had an economical transport that could carry a couple of passengers and baggage over 1000 miles or six executives to a day meeting two hours away. The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg. 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. We use cookies to help you get the best experience when using our website. Plane and Pilot expands upon the vast base of knowledge and experience from aviations most reputable influencers to inspire, educate, entertain and inform. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. (See www.ramaircraft.com. Improved version CESSNA 414A Chancellor (appeared in 1978) with bonded wet wing, without tip tanks. The piping which directs the exhaust from the manifold to the turbo is also susceptible to cracking. The factory tends to be much pricier than third-party garages that overhaul your engine. 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. - Send us pictures of your plane. There are four options, all of which provide a sizable increase in horsepower, increase the TBO, and newer, more powerful propellers. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. The pressurized comfort of the 414A, which produces an 8000-foot cabin at 22,800 feet, cannot be overemphasized. 150 The 411A, produced from 1967-68, featured a redesigned nose and more baggage space. 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. In the early 414s, the main landing gear webbing is prone to cracking, requiring extensive rectification. 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. Technique: Landing like a pro - AOPA The landing gear is the standard electromechanical system that is on all tiptank twin Cessnas. VGs are also available from Micro Aerodynamics (www.microaero.com) and V/G Systems, phone 800-328-4629. CESSNA 340 - Plane & Pilot Magazine Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. Its an $800 part.MODS, CLUBSAmong the most popular mods are the RAM Aircraft Corporation engine swaps. Thus, it is an indication of age and use. ft/min, ROC Become a member and get exclusive access to articles, contests and more! Pilots with less experience can expect this range to rise to between 1,100 to 1,600 per year. 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. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). Range 568-1,322. Range 489-1,242. Ceiling 27,400. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. Faster aircraft generally have a higher wing loading as less area is required to carry the same mass. Cessna 182 vs 185 Compared: Which Is Better? Replacing the cylinder heads requires money and time, which will increase your engine overhaul costs by $6,000 bringing your grand total to $39,000. 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. Passengers love it for space, comfort, and low noise levels. Specs, range, speed, operating weights and performance for the Cessna 340 here. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. Twin engine piston aircraft with retractable landing gear. 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). kg, IAS The Cessna 414 was given a clean wing in 1978. Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. Winglets aid climb and cruise speeds. Operating Costs. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. ( FL Range 1,284. GlobalAir.com is your partner in connecting you with relevant information and resources. No warranty of 414 chancellor. The Chancellor 414A has an impeccable safety record. It was developed to bridge the gap between the unpressurized Cessna 401 and the pressurized, more powerful Cessna 421. The 414 does have AD97-26-16 requiring consideration, and those aircraft requiring regular x-ray and ultimate installation of the service kit will necessarily command a lower price. 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. A simpler fuel system was among a host of improvements unveiled in 1978 with introduction of the Model 414A Chancellor. 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
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