Lightly loaded and at economic power settings, expect to get almost 1,300 nautical miles of range. kts, ROC 5 A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. In the years following its introduction, the airplane saw few major changes. Production aircraft were accessible in several optional seating configurations and avionics packages. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads. The Cessna 411, first delivered in 1965, was one of Wichitas first ventures into the airliner market. The fuselage and tail were essentially the same as the ones used on the 421B, while the wings were taken from the 401. Special Missions. The variable costs such as maintenance for the airframe, as well as other costs such as landing and parking fees totaling $206,550. Landing Distance: 3,170 ft (966 m) Maximum Operating Altitude 45,000 ft . The exhaust system sees a great deal of heat and vibration, thus components wear out. Ceiling 29,800. I have owned and flown a 1979 Cessna 414A for 14 months, accumulating 235 hours in all sorts of conditions. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. In 1978, an enhanced version was launched, designated as the 414A Chancellor. The Achilles heel of the airplane for me has been the cabin heater. }.tdi_115 .td-element-style{ Pilots with less experience can expect this range to rise to between 1,100 to 1,600 per year. Preferred Airparts, based in Ohio, provide worldwide customers with surplus new Cessna original components and used parts from dismantled aircraft. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. Owners recommend two groups. Performance specifications Horsepower: 2 x 375 HP Best Cruise Speed: 241 KIAS Best Range (i): 1,197 NM Fuel Burn @ 75%: 47.0 GPH Stall Speed: 74 KIAS Rate of climb: 1,940 FPM Rate of climb (1 engine out): 350 FPM Ceiling: 30,200 FT Ceiling (1 engine out): 14,900 FT Takeoff distance: 1,786 FT Landing distance: 720 FT The pressurized 414 was developed to appeal to owners of unpressurized, twin-engined aircraft, and was based on the fuselage of the Cessna 421 and used the wing design of the Cessna 401. Precise Flight and Spoilers, I. Cessna Country: United States Manufactured: 1961 to: 1985 ICAO: C185 Price: US$.32 million (2019) Performance Weights Dimensions Avionics: Engine: 1x Continental IO-520-D Piston Power: 300 horsepower Max Cruise Speed: 145 knots 269 Km/h Approach Speed (Vref): 49 knots Travel range: 720 Nautical Miles 1,333 Kilometers Fuel Economy: Service Ceiling: Average price for used aircraft CESSNA 414A is $344,804.81. Landing distance (50) 1,815. The 414 was meant to attract customers looking to upgrade from their unpressurized twin-engined aircraft and did so with limited success. Plane and Pilot expands upon the vast base of knowledge and experience from aviations most reputable influencers to inspire, educate, entertain and inform. 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. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor. 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 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. PERFORMANCE: Top mph 268. (n.d.). (See www.ramaircraft.com. no data ft/min, TAS Training is a must. 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. The Chancellors that cost close to $500,000 most often are pristine and like-new. - Send us pictures of your plane. 200 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. There are several problems that the 414A has. Landing Distance: 4000 ft; Performance. 7,450. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. 1100 The pressurized comfort of the 414A, which produces an 8000-foot cabin at 22,800 feet, cannot be overemphasized. The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. - Aircraft specific reviews and articles. The popularity of the aircraft ensures that there are enough aftermarket parts that can be bought if used parts are unavailable. The pressurization and turbocharged nature of the aircraft mean it is complicated to work on, and specialization is needed. 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. 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. 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. 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. One of the most important came in 1973, when cabin length was increased 16 inches and a fifth side window was installed. Cessna 120 Guide and Specs : Is It Powerful Enough? 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. The 401, introduced in 1966 and discontinued in 1972, was basically designed as a medium to . Stall mph cabin is separated from the passenger compartment by a divider. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); WORLD'S PREMIER INDEPENDENT AVIATION NEWS RESOURCE. The aircraft is powered by two Continental TSIO-520-NB piston engines. . 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. It's also a myth. It is our mission to be the go to leaders in the aviation industry. The landing gear track was also increased by 4 feet (1.2 m). It is powered by two wing-mounted 310hp (231kW) Continental TSIO-520-J horizontally opposed, six-cylinder engines. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Insurance costs have equaled $7000 per year for the last couple of years for $1 million smooth with a hull value of $350,000. For the 414, the engines chosen were the 310hp TSIO-520-Js, with intercoolers and takeoffs for cabin bleed air pressurization. PERFORMANCE: Top mph 268. A typically equipped 414A has a full-fuel payload of about 500 to 700 pounds, depending on equipment. Also says to increase landing distance by 45% (doesn't seem to make sense). I bought it to replace a nice Cessna T310R, which I flew for about a year. The first Cessna Chancellor - the 414 - took to the skies in 1968, and was produced from 1970 onwards. Membership in and attending the Twin Cessna Flyer Organizations Pilot Seminars should be required. B. C. (2015, July 13). 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. Range 489-1,242. Pay attention to the fuel system in tip-tanked 414s. The Chancellor has a service ceiling of 30,800 feet and a maximum speed of 235 knots. kt, ROD 1200 Model 414 seats up to 7 passengers and 1 pilot. The AD 2005-05-52 was put in place to counteract this issue by using eddy currents to inspect the said struts and visually inspect the auxiliary and rearward struts. Some potties have a flushing feature. MEL, in this case, refers to Multi-Engine Land. Each engine spun a constant speed, three-blade McCauley propeller. Range 506- 1,325. kt, MCS 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. Continental also published overhaul procedures to enable -NB engines to get the TBO boost. 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 two main tanks were essential sections of the sealed wet wing. 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. (Beginning in 1957, horsepower was modestly increased to 230.) Fuel capacity varies. I cannot count the number of heater failures Ive suffered over the years and the number of maintenance folks who have done their best to help me. An improved variant the Cessna 414A Chancellor was introduced in 1978 with the major change being a redesigned and increased-span wing with integral fuel tanks and an extended nose to give more baggage space. Fuel capacity 202. We use cookies to help you get the best experience when using our website. Beginning in 1978, Cessna offered three basic equipment packages. He's worked on various aircraft from small two-seaters like Tomahawks or Boeing 767s. Even with the company is getting its feet wet in piston products again, there are no immediate plans to make any cabin-class piston twins to replace those being retired. Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. Six seats were standard; a seventh was available as an option. . Operating and maintenance costs are attractive when compared with those of competing airplanes, such as the big-brother 421 and Beech Aircrafts Duke. No warranty of 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. ( 2023 GlobalAir.com. Once it reaches the cabin it is compressed enough to create an atmospheric pressure that mimics the desired altitude. 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. 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. The takeoff distance is 408 meters while the landing distance is 365 meters. Many of which have been addressed by ADs and service bulletins. David is a seasoned pilot and aviation expert. 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. https://www.aviationconsumer.com/aircraftreviews/cessna-414-chancellor/(N.d.). 3060 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 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. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. By continuing to use this website, you are agreeing to our Cookie Policy. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. The pressure of the cabin is usually around 8,000 ft but can be less according to how the system is set up. Soaring Good Looks. One club offers extensive support for the 414, in addition to all other twin Cessnas. Most had the RAM VI engine conversion. Takeoff distance (50) 1,662. 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. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. When discussing 414s and 414As, one must speak correctly. The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg. Also, the big Cessnas have safety records that are unmatched by any other light twin. 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. Top mentions include the true cabin class, reasonable cruise speed, and maintenance of sea-level pressure to 10,000 feet. When we look at the power loading of the aircraft, the why becomes obvious: weight. 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 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. 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. Come join us! Mike Buschs Savvy Owners seminar is valuable. The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. Refreshment centers can be aft or a vertical unit positioned behind the pilot or copilot seat. Overall, the 414A is a capable aircraft. With the rise in FAA-PMA approved manufacturers, many have niched down to support a particular aircraft type and finding trim (knots2u, Texas Aeroplastics or AvFab), landing gear components (Robair Repair), or lighting (Whelen Aerospace Technologies or AeroLeds) for your 414 is not hard. 1000 )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. Cruise mph 223. Initial climb rate 1,610. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. This can be remedied by fitting the aircraft with speed brakes/spoilers or installing a liquid cooling system to the engines. If youre one of the lucky owners who have to overhaul their engine without replacing the cylinder heads, a shop will only charge an average of $33,000 nearly half of what the factory charges. 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 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. (See www.ramaircraft.com.). Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. 3,865. Range 568-1,322. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. The Cessna 414A is an improved 414 with narrower vertical tail, longer span bonded wet wing without tip tanks, a lengthened nose, re-designed landing gear and powered by two 310hp (231kW) TSIO-520-N engines. Each of its 620 hp has to carry 10.8 lbs, which is quite poor. The 340 has a gross weight of 5,975 pounds, and an empty weight of 3,697 pounds. 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. Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. 150 Cessna 414 Guide and Specs : Is It High Performance? Save my name, email, and website in this browser for the next time I comment. Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners. The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. Landing distance (50) 1,790. Email Seller Video Chat. 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 Aviation Consumer. Another point of consideration for a 414 buyer is the SB/AD on the wing spar. 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. Gross wt. 180 Are COVID Vaccines Injuring Pilots? These aircraft were called the 414A Chancellor. Fuelburn: 34.0 GPH Specs, range, speed, operating weights and performance for the Cessna 340 here. 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 1973 to 1977s are the long bodies. In my Cessna 152, a 20-knot headwind increases the glide angle from 5 degrees to 7.5 degrees, a 50-percent increase. It has a range of 1,328 nautical miles and a climb rate of 1,520 feet per minute. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. However, there seem to be plenty that are not. As has often been said, Cessna really got it right with the 414/414As. According to Cessna, 4.2-psi cabin pressure differential could be maintained by either engine operating at 60 percent power. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). The applications are smaller and they have maintenance issues, so the price does fall. 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. Gross wt. Features wing of CESSNA 402 and fuselage of CESSNA 421. We are a collective group of airline instructors, and pilots dedicated to all things aviation. (38.0 gallons/hr @ $5.40/gal), Misc: landing, parking, supplies,catering, etc, Typical Price: $307,752.00 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. When it comes time to overhaul the engine, the cylinders might have to be replaced, and a new set of Continental brand cylinders cost roughly $5,000 depending on the supplier, whereas an off-brand set costs around $2,000. 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. Electronic prop synchrophasers became standard equipment in 1976, when two versions of the airplane were put on the market: a bare-bones 414 and a 414II, which came with an assortment of ARC 400-series avionics equipment.That year, most limiting and recommended airspeeds were boosted a few knots (except Vmc, which was lowered from 84 to 82 knots), and the -J engines were replaced with TSIO-520-Ns. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. Its wings are borrowed from the Model 414. Also worth joining is the Cessna Pilots Association (www.cessna.org and 805-934-0493). He was a glider pilot for several years before obtaining his private license in taildraggers. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. 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. The change allowed the engine to produce 310 hp (228 kW) at 2700 RPM from sea level to 20,000 ft (6,096 m). Give me one three-hour cross country with any new owner and hell be able to teach the system. An engine rail replacement can cost an eye-watering $14,000. Cessna Caravan Maximum Range: 1,070 nm Maximum Occupants: 10 - 14 Cessna SkyCourier (Freighter) Maximum Range: 940 nm Payload: 6,000 lb Cessna SkyCourier (Passenger) Maximum Range: 920 nm Maximum Passengers: 19 Single Engine Aircraft The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. Answer: TBO means Time Between Overhaul, which is the manufacturers recommended running time, in hours or calendar time, before overhaul. The original 414 aircraft retailed at US$138,000 in 1970. On November 1, 1968, the prototype registered N7170C, conducted its maiden flight. Empty wt. 520 Cessna 414 pressurized-turbocharged - Performance Data . However, most owners report that after a few hours of flying, it requires little thought. The Cessna Pilots Association, located at www.cessna.org, and the Twin Cessna Flyer, at www.twincessna.org. With the O&N tanks in both nacelles, I can carry up to 260 gallons of fuel, good for over seven hours of endurance. The older 414s are known as the short-bodied models. The Cessna 180 Skywagon is not a beautiful airplane, but it is a classic-looking taildragger that became an . Send feedback comments to the EUROCONTROL Training Institute. The 414A has an issue with shock cooling of the engine that occurs during rapid descents. 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. 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. 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. For the Cessna 414A Chancellor, average pricing was US$280,000, having approximately 7,500 hours total time airframe (TTAF) and mid-life engines. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. 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. My flights range from an hour to four hours and while I have flown the airplane from coast to coast, I find trips of three hours or less are well suited for the airplane.

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