Finally, spoiler mods aid faster descents while avoiding engine shock cooling. The 414 is a low-wing cantilever monoplane with a conventional tail section and a retractable tricycle undercarriage. Data from Jane's All The World's Aircraft 198283[8], Last edited on 27 February 2023, at 22:02, "RAM Altitude Performance Enhancing Winglets", "CENTURION ENGINES - Cessna 340, 414 & 421", "National Transportation Safety Board Aviation Accident Final Report Accident Number: FTW82AA299", https://en.wikipedia.org/w/index.php?title=Cessna_414&oldid=1141981287, This page was last edited on 27 February 2023, at 22:02. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. The gear system of the 414A is easy to maintain, with one spot to watch: When assembling the center bolt on the main landing gear scissors, the correct washers must be installed in the correct sequence or the bolt can pull out, allowing the main gear wheel to turn sideways.Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. 5,500. Those owners who try to operate an aircraft like the Cessna 414 on a shoestring are pursuing false savings. The Cessna 340 produced by Cessna. } Crew-6 Launch Scrubbed For Ground Systems Issue, The Drip, Drip Of Bad Publicity About 100LL. Utility twin aircraft. ft/min, ROC Reaching fever pitch in the 1980s, Cessna had positioned itself well for the demand, offering light twins for almost every conceivable subsection of the market. All rights reserved. Range 506- 1,325. It featured major modifications, including a restructured and increased wingspan, incorporating integral fuel tanks, and a stretched nose to allow more space for baggage. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. 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 (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. 4,640. The Cessna 414 Chancellor was produced from 1968 to 1985. Distances Balanced Field Length: 1780 ft Landing Distance: 2358 ft Performance Rate of Climb: 920 fpm Max Speed: 156 kts Normal Cruise: 147 kts Economy Cruise: 117 kts Cost per Hour: $ 220.95 Power Plant Engines: 1 Engine Mfg: Continental Engine Model: IO-520-F Marketplace Information Interested in buying this aircraft click here! Takeoff distance (50) 1,700. 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. In addition to 335-HP engines, new props and intercooler scoops, it includes a set of vortex generators and gives an increase in useful load of 415 pounds. 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. Plane and Pilot builds on more than 50 years of serving pilots and owners of aircraft with the goal of empowering our readers to improve their knowledge and enthusiasm for aviation. ( 3,467. These aircraft were called the 414A Chancellor. 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. [4] This involves the installation of FADEC-controlled aviation diesel piston engines that run on commonly available jet fuel. 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. With the same fuselage as the 421, the 414 was roomy with huge baggage space. Bringing the grand annual total to $240,785. It is powered by two wing-mounted 310hp (231kW) Continental TSIO-520-J horizontally opposed, six-cylinder engines. In addition to 335-HP engines, new props and intercooler scoops, it includes a set of vortex generators and gives an increase in useful load of 415 pounds. The 16 inches of extra length and the added side window do not directly mean much, but short-bodied 414s rarely have the typical cabin-class size refreshment center nor a potty. Always remember where the wind is coming from and adjust the pattern accordingly. Ceiling 26,000. 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.Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. 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 In service since 1969. 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. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. Operating and maintenance costs are attractive when compared with those of competing airplanes, such as the big-brother 421 and Beech Aircrafts Duke.In a study of accident records some years ago, the 414 stood out as the safest light twin. Another area that needs to be checked for corrosion is the firewall. A qualified pilot is considered to be one with a PPL license with IFR and MEL ratings, who have 1,500 total hours, 500 MEL hours, and 25 hours on type. Each of its 620 hp has to carry 10.8 lbs, which is quite poor. 16 Soaring Good Looks. EASY ACCESS Two large cabin doors allow for convenient entry and loading for student and instructor. BUILT FOR TRAINING Ideal for entry-level landings, the Skyhawk piston features a sturdy tricycle landing system and a resilient airframe. Cessna made the most significant changes to the Chancellor when it introduced the 414A. Real world speeds depend on engine configuration, but owners typically report 200 kts at about 38 gph in the upper teens. 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. kg, IAS Takeoff distance (50) 2,175. 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. 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. (n.d.). 2023 GlobalAir.com. Service ceilings are above 30,000 feet, but few owners fly that high. According to the president of the Twin Cessna Flyer a society for owners of Cessna Twin aircraft Larry Ball, there are a few more problem areas of the 414A that have not been published but are common enough to talk about. PERFORMANCE: Top mph 273. According to Aircraftcostoperator.com, the average total hourly cost of operating a Cessna 414A is roughly $535. (See page 25 for an abbreviated AD list.). This means the aircraft will burn around 17 gph (64 lph) per engine at 65% power and FL250, which is enough to get you cruising at around 202 KTAS (232 mph / 374 kmph). 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 before buying one, you should ensure that there is an AMT with experience on pressurized Cessna twins in your area. With a range of approximately 2,200 nautical miles and a relative low cost, the Conquest II was an unparalleled aircraft in its time. Operating Costs. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Your email address will not be published. The Chancellor utilizes the hydraulic components of the Golden Eagle gear and features a five-second retraction time. Fuselage strakes improve yaw control, performance in turbulence, and a higher cruise speed. STOL kits can also be purchased to help reduce the field length of the aircraft. Fuel capacity 202. Other engine mods include a turboprop-powered conversion of the Cessna 414, named the Turbo Star Pressurized 414, using Allison 250-B17B engines, and the Thielert FADEC-controlled diesel Centurion piston engines that run on commonly available jet fuel. 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. Stall mph 79. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. The efficiency of the 414As long high-aspect ratio wing is highlighted by noting the 414As single-engine service ceiling is 19,850 feet. .tdi_115.td-a-rec-img { Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. Answer: An STC refers to a Supplemental Type Certificate. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. 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. RAM also makes winglets and vortex generators. I have split my time about equally between the RAM IV 325-HP engines and the RAM VII 335-HP engines and Scimitar props that I had installed when the RAM IVs hit their TBO. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. Cited as an excellent IFR platform, youll 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. Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: }.tdi_115 .td-element-style{ 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. Passengers love it for space, comfort, and low noise levels. LED landing and recognition lights offer enhanced visibility and strong illumination for night flying. Phone: (305) 342-0760. PERFORMANCE: Top mph 297. FL Retrieved October 5, 2021, from https://www.globalair.com/aircraft-for-sale/Specifications?specid=971. 6,200: 6,430: Zero Fuel Weight - lbs. ) Developed from the 310, it utilizes a similar landing gear and tail unit. 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. The two main tanks were essential sections of the sealed wet wing. All rights reserved. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. Derived from the Model 411, the Cessna 401 and 402 are essentially the same aircraft put to two different uses. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Operating and maintenance costs are attractive when compared with those of competing airplanes, such as the big-brother 421 and Beech Aircrafts Duke. The design of the Cessna 414 was to bridge the gap between their unpressurized twin, the Cessna 402, and their pressurized flagship, the Cessna 421. It is capable, comfortable, and performs well. 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. Other modifications in 1978 included a longer nosecone, a redesigned undercarriage system, and an extended wing without the earlier tip tanks. https://www.federalregister.gov/documents/2005/06/14/05-11613/airworthiness-directives-cessna-aircraft-company-models-402c-and-414a-airplanes, Cessna 414. The Chancellor replaced the former 414 in 1978 and offered a new level of payload performance, range, and fuel efficiency. 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. Flight planning or any other aircraft operations should only be done using official technical information provided However, the eddy current method did not effectively identify the cracks until it was to the point where a load much lower than the published maximum load can cause catastrophic structural damage. As with all Twin Cessna's, the landing gear and exhaust systems must be maintained properly. No warranty of 6,165: 6,165: SOURCE: Sources. The Cessna 414 is a high-performance aircraft requiring regular and comprehensive maintenance, and if looked after and regularly updated, the aircraft will hold its own on resale. Also says to increase landing distance by 45% (doesn't seem to make sense). The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. no data I have had my share of problems with turbos, turbo controllers, cylinders and cracked cases. If you opt to go for a rebuilt engine from Continental will save you $6,000, for a total price of $54,000. Cruise mph 231. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. Cessna 195 Guide and Specs : All About The 195 Businessliner, Bombardier Challenger 300 Guide and Specs, Installed equipment, specially avionic fit-out. 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 top of the line for the 414 is the series VI. Six seats were standard; a seventh was available as an option. 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. However, there seem to be plenty that are not. Aerodynamic mods include vortex generators to increase aileron and rudder control authority at low speeds. Engines two 375-hp turbocharged Continentals. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. 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. Would like to understand why. Faster aircraft generally have a higher wing loading as less area is required to carry the same mass.
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