text-align: center; The Cessna Pilots Association, located at www.cessna.org, and the Twin Cessna Flyer, at www.twincessna.org. Fuel burn is the same, 34 GPH in cruise at all altitudes, with the RAM VII at 69 percent. However, only upon acquiring the 414 did I finally attain my goal-virtually complete independence from the airlines for domestic travel. The 414 was meant to attract customers looking to upgrade from their unpressurized twin-engined aircraft and did so with limited success. Those owners who try to operate an aircraft like the Cessna 414 on a shoestring are pursuing false savings. 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. 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 Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. It featured major modifications, including a restructured and increased wingspan, incorporating integral fuel tanks, and a stretched nose to allow more space for baggage. Empty wt. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. I own a 1978 Cessna 414A which I acquired in 1989. - Aircraft specific reviews and articles. Although you could fly for about 1,100 miles, you would be able to bring only two friends and a few bags. Initial climb rate 1,610. 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. [4] This involves the installation of FADEC-controlled aviation diesel piston engines that run on commonly available jet fuel. I sell 25 Twin Cessnas a year, which usually includes six to eight 414s and 414As. STANDARD DATA: ( 411) Seats 6-8. Specs, range, speed, operating weights and performance for the Cessna 340 here . Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. Landing Distance: 4000 ft; Performance. LED landing and recognition lights offer enhanced visibility and strong illumination for night flying. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. 230
Answer: An STC refers to a Supplemental Type Certificate. Many supplemental type certificates exist for the aircraft that allow upgrades to improve performance. 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. It is our mission to be the go to leaders in the aviation industry. One pilot and typical 6 passengers in main cabin. } 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 I have had my share of problems with turbos, turbo controllers, cylinders and cracked cases. Soaring Good Looks. 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. 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. PERFORMANCE: Top mph 273. Cruise mph 277. We use cookies to help you get the best experience when using our website. Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. 800
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. If an owner has taken a maintenance only as required approach to their aircraft, they can expect a far lower resale value. 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. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. It can carry up to 8 passengers and baggage, or full fuel, but not both. NM, ROD
Passengers love it for space, comfort, and low noise levels. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor. CESSNA 414A Ram V. Retrieved October 8, 2021, from https://www.aircraftcostcalculator.com/AircraftOperatingCosts/350/Cessna+414A+Ram+V, Continental 520 overhaul cost. Some ADs have called for replacing faulty parts such as a set of vacuum pumps, and bolts on the fork of the main landing gear. Phone: (305) 342-0760. kt, ROD
The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. It uses spent exhaust gases to run the compressor, which draws in and compresses clean air to deliver to the engine. The resale value increases greatly if a RAM conversion has been done and additional performance modifications have been fitted. Answer: An aircrafts service ceiling is defined as the height at which the aircraft cannot climb at a rate greater than 100 feet per minute. One of the most important came in 1973, when cabin length was increased 16 inches and a fifth side window was installed. 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. Sure, many have been plowed up for houses or 2023 Aviation Publishing Group. Range 1,284. However, there are a number of airworthiness directives (AD) and service bulletins that have been published over the years. )A potential buyer should carefully investigate the compliance status of the airplane by flight time and serial number, especially if the airplane is high time. Cessna 414 Stock Airplane vs. RAM Series IV; Primary Specifications Cessna 414 RAM 325 hp Series IV; Engine Model: Continental - TSIO-520-J-NB: Horsepower: 310: 325: . 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. According to Cessna, 4.2-psi cabin pressure differential could be maintained by either engine operating at 60 percent power. . Features wing of CESSNA 402 and fuselage of CESSNA 421. Although the 414s have a huge cabin-class interior, the stock airplane has never been a tremendous load hauler. The Chancellor utilizes the hydraulic components of the Golden Eagle gear and features a five-second retraction time. Thus, it is an indication of age and use. 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. Please send us your experiences on your aircraft. Landing distance (50) 1,815. The engine is notorious for cracked cylinders and therefore requires periodic inspections. 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. Pressurization happens in the engine, where hot air is compressed and then directed to the cabin. https://cessnaowner.org/414-chancellor/, estaff. Best Range: 1106 NM Its a combination of the airstair door, large cabin, air conditioning, abundant baggage space, large picture windows, pressurization and -not to be discounted-the potty! 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. It is a less powerful and lighter evolution of the Cessna 421. 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. 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: - Already a member? The Cessna 414 Chancellor was produced from 1968 to 1985. 1100
RAM also makes winglets and vortex generators. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. [2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]. (2001, February 26). Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. (n.d.). Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds.In the years following its introduction, the airplane saw few major changes. Empty wt. 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. 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. I bought it to replace a nice Cessna T310R, which I flew for about a year. 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. Fuel capacity varies. It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. 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. . )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. 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. With rare exception, all 414As have an aft potty. 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. Lightly loaded and at economic power settings, expect to get almost 1,300 nautical miles of range. 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. He was a glider pilot for several years before obtaining his private license in taildraggers. The applications are smaller and they have maintenance issues, so the price does fall. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. 310, Range
kts, Distance
There are only two fuel-. Six seats were standard; a seventh was available as an option. All speak highly of the 414 as a dependable aircraft offering a lot, including pressurization, for the price. Answer: Wing loading is the total aircraft mass divided by its wing area. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. 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. 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. Rate of Climb: 1650 fpm; Climb Rate One Engine Inop: 315 fpm; Max Speed: 243 kts; Normal Cruise: 229 kts . Range 568-1,322. The greater the experience of the owner/pilot, the lower the premiums. (See page 25 for an abbreviated AD list.). 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. David has licenses as an aircraft maintenance engineer in New Zealand and Australia. (See page 25 for an abbreviated AD list. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). This piston engine is a six-cylinder, horizontally-opposed, direct drive, turbocharge, air-cooled, and fuel-injected type that produces a maximum thrust of 310 horsepower each. Its an $800 part. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. 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. The model 414, a 411 derivative introduced in 1970, utilized the 421s fuselage and tail unit with the 401s wings. That resulted in cruise speeds of only about 180 to 185 KTAS up high. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. Come join us! In general, all owners praise the performance and capability of the aircraft, especially ones that have a RAM conversion and STOL kit, because it makes the aircraft much more versatile. Stall mph 81. As has often been said, Cessna really got it right with the 414/414As. The aircraft factors are: These terms are all within the control of the owner. Purchasing a Cessna 414A is considered to be cheap for the number of airplanes you get. Frequently, a a buyer makes assumptions that arent correct. After the Chancellor debuted, there were few further refinements. Each model has different after-market engine/prop conversions and when other performance-enhancing modifications are factored in, weights and other performance criteria vary. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. The aircraft got heavier, with the MTOW and landing weight increasing by 400 lbs (181 kg) and 550 lbs (249 kg), respectively. Ceiling: 30,800 FT Ceiling (1 engine out): 19,850 FT Takeoff distance: 2,185 FT Landing distance: 1,013 FT Takeoff distance over 50ft obstacle: 2,595 FT Landing distance over 50ft obstacle: 2,393 FT Weights Gross Weight: 6,750 LBS Empty Weight: 4,543 LBS Maximum Payload: 1,769 LBS Fuel capacity: 213 GAL Ownership Costs 1978 Total Cost of Ownership: However, there seem to be plenty that are not. The RAM IV struggled in the flight levels, especially in the summer. 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. text-align: center;