Power. Each model has different after-market engine/prop conversions and when other performance-enhancing modifications are factored in, weights and other performance criteria vary. Mike Buschs Savvy Owners seminar is valuable. The 414 was meant to attract customers looking to upgrade from their unpressurized twin-engined aircraft and did so with limited success. }.tdi_115.td-a-rec-img{ The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. 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. 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. The Cessna 340 produced by Cessna. The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. No warranty of 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. kg, IAS 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. 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. 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. Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. 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. It is a less powerful and lighter evolution of the Cessna 421. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. Aircraft of similar configuration, age, and role include the Beechcraft Queen Air, AeroCommander 690, Piper Cheyenne, Beechcraft Duke, and the Piper Pa-31 Navajo. They can be purchased from Micro Aerodynamics and VG Systems. The exhaust system sees a great deal of heat and vibration, thus components wear out. Come join us! The other category that brings the price up to the same number are the aircraft that have undergone a RAM conversion. The factory tends to be much pricier than third-party garages that overhaul your engine. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. Takeoff distance (50) 1,700. Landing distance (50) 1,850. }.tdi_115.td-a-rec-img img{ The basic 414 was born in 1970 with a 4.2 psi pressurization differential and ascended to become the Chancellor in 1978. Operating Costs. RAM also makes winglets and vortex generators. Four years later, Continental incorporated some changes to the -NBs cylinders, valve lifters and piston pins, and increased the engines recommended TBO from 1400 to 1600 hours. Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. 100 kts, ROC All rights reserved. no data All rights reserved. Any part that isnt new is all overhauled from the turbocharger to the fuel pressure regulator. Like most all twin Cessnas, we give the 414 high marks for cockpit ergos, and the logical layout of systems and controls makes the flight deck a comfortable place to chew up the miles. Cessna 414 Stock Airplane vs. RAM Series VII; Primary Specifications Cessna 414 One of the most distressing issues the Cessna 414A has is cracking along the forward wing spars. One former owner even stated that anyone who says the aircraft is reliable is delusional. I am a professional aircraft broker who specializes in Twin Cessnas. Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. 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. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds.In the years following its introduction, the airplane saw few major changes. Retrieved October 5, 2021, from https://www.globalair.com/aircraft-for-sale/Specifications?specid=971. 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. Introduced in 1978, the Cessna 414A or more commonly known as the Cessna Chancellor III, is a pressurized, twin-engined aircraft, with retractable landing gear. quantity indicators, both with three-position switches, to help the pilot keep track. This plane was. Passengers love it for space, comfort, and low noise levels. 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. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. An engine rail replacement can cost an eye-watering $14,000. The most significant and popular modifications that can be made to a 414A are the engine swaps by the RAM Aircraft Corporation. 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. There are several good training programs available to help keep 414 pilots in top form, something we feel to be quite important as, while the accident rate is low, the accidents seem primarily to occur on amateur flown airplanes and involve judgment errors on the part of the pilot rather than anything wrong with the airplane.HISTORYCessna borrowed components from existing 400-series airplanes to come out in 1970 with a model to bridge the price gap between unpressurized and pressurized twins. The engine is notorious for cracked cylinders and therefore requires periodic inspections. The applications are smaller and they have maintenance issues, so the price does fall. 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. All rights reserved. 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. Fuel capacity 213-270. However, it isnt just an engine swap. Initial climb rate 1,700. When we look at the power loading of the aircraft, the why becomes obvious: weight. ) 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. We use cookies to help you get the best experience when using our website. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. 720 Rate of Climb: 1650 fpm; Climb Rate One Engine Inop: 315 fpm; Max Speed: 243 kts; Normal Cruise: 229 kts . Answer: TBO means Time Between Overhaul, which is the manufacturers recommended running time, in hours or calendar time, before overhaul. 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.After the Chancellor debuted, there were few further refinements. 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. Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. The 1970 to 1972 models are referred to as short-bodied 414s. Range 489-1,242. Cessna 414 Performance & Handling Cited as an excellent IFR platform, you'll guess the control forces on the 414 are heavy and stable, yet a great design means only minor trim changes are needed when extending landing gear or flaps. Landing distance (50) 2,393. The Chancellors that cost close to $500,000 most often are pristine and like-new. 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. Email Seller Video Chat. 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. Training is a must. The aircraft got heavier, with the MTOW and landing weight increasing by 400 lbs (181 kg) and 550 lbs (249 kg), respectively. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. In my Cessna 152, a 20-knot headwind increases the glide angle from 5 degrees to 7.5 degrees, a 50-percent increase. Fuel transferred too early is pumped overboard. Landing distance (50) 1,815. The aircraft is powered by two Continental TSIO-520-NB piston engines. Landing distance (50) 1,815. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. 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. 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. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. One of our Planephd Experts will be in touch with you shortly. It's also a myth. Landing distance over 50-ft obstacle: 2,393 ft: Landing distance, ground roll: 1,013 ft: Limiting and . All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. Owners speak of the 414s smoothness, stability, and ease with which you can trim the aircraft out. Cessna Owner Organization. Stall mph 82. STANDARD DATA: ( 411) Seats 6-8. by the manufacturer or FAA. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. The figures show that the demand for Dakotas has increased causing prices to rise by about 40 percent. 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. 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. In 1973 Cessna stretched the fuselage by 16 inches and added a fifth side window. TAKE-OFF MTOW: WTC: RECAT-EU: Light Distance: V2 (IAS): 520 m 100 kts INITIAL CLIMB (to 5000 ft) IAS: ROC: 130 kts 1200 ft/min CLIMB (to FL 240) IAS: ROC: 150 kts 800 ft/min CLIMB (to FL 150) IAS: ROC: 150 kts 1000 ft/min MACH CLIMB MACH: ROC: - - CRUISE MACH: Ceiling: - 310 FL TAS: 230 kt Range: 1100 NM INITIAL DESCENT (to FL 240) MACH: - ROD: - 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. Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. Flight planning or any other aircraft operations should only be done using official technical information provided no data But the average price of a 414A is around $300,000, while the price range is between $200,00 $500,000. 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. 16 Gross wt. Please send us your experiences on your aircraft. The system left room for error, not only on the part of the pilot, but among line personnel. How much does it cost to fly: $683.19 per hour. Many supplemental type certificates exist for the aircraft that allow upgrades to improve performance. On the flip side, when fully loaded with eight passengers and baggage, there will be enough space for barely two hours of fuel. The top of the line for the 414 is the series VI. Seating is spacious and available in a variety of arrangements. 180 The deice light on the panel illuminates only very briefly when the pneumatic deicing system is activated and only indicates that theres pressure to the tail boots. The 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 414A has a single-engine ceiling of 19,850 ft (6,050 m) which is the best among all its peers. Developed from the 310, it utilizes a similar landing gear and tail unit. 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. Fuel capacity 102-207. Total Cost of Ownership: $39,555.22 4,640. The 375-HP 421Cs single engine ceiling is 14,900 feet. 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. Range 506- 1,325. The Cessna 414 Chancellor was produced from 1968 to 1985. I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. Empty wt. Cruise mph 223. 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 Answer: An STC refers to a Supplemental Type Certificate.
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