All rights reserved. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Chancellors are as roomy as 421B/Cs. 4,640. ( We use cookies to help you get the best experience when using our website. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. Engine and aerodynamic modifications abound for the 414. Fuel capacity varies. By continuing to use this website, you are agreeing to our Cookie Policy. Landing distance (50) 2,393. 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. 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. Any part that isnt new is all overhauled from the turbocharger to the fuel pressure regulator. With its bigger nose and lockers, the 414A can carry 1500 pounds. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. 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 However, as aircraft age, they dont get cheaper to own or operate, which the price will reflect. Soaring Good Looks. 180 However, there are a number of airworthiness directives (AD) and service bulletins that have been published over the years. 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. Ownership and operating costs. So before buying one, you should ensure that there is an AMT with experience on pressurized Cessna twins in your area. 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. Stall mph 82. Takeoff distance (50) 2,220. That resulted in cruise speeds of only about 180 to 185 KTAS up high. GlobalAir.com is your partner in connecting you with relevant information and resources. kt, Distance In airplane engines, turbochargers are popularly used to achieve forced induction. no data The exact specifications of the Cessna Chancellor 414A are: A hotch-potch of the Cessna 401 and 421, the Chancellor easily stole the limelight as the best of the 400-series, even though it was meant to simply fill the gap between the two, and became a hit among pilots everywhere, and in recent years has gained popularity with charter operators. So, if its just pressurization youre looking for and youre going to be flying with only another person or two aboard, you might want to look at the 340 for a personal hot rod. The remedy for this was increased visual inspections and the strengthening of the wing spars by adding spar straps. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. 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. It is an approval granted to a parts manufacturer to manufacture specific aircraft components. Cessna Owner Organization. A typically equipped 414A has a full-fuel payload of about 500 to 700 pounds, depending on equipment. The first Cessna Chancellor the 414 took to the skies in 1968, and was produced from 1970 onwards. 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. 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. 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. They can be purchased from Micro Aerodynamics and VG Systems. 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 1976 the airplane was equipped with a propeller synchrophaser to control propeller RPM and phase relationship of the blades, engine-to-engine. A 414A RAM Series VII with Winglets (AW) will compete in many ways with a 421C. Fuel transferred too early is pumped overboard. 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. The Piper Seneca is also quite similar to the 414A, even though it is slightly smaller. Pilots with less experience can expect this range to rise to between 1,100 to 1,600 per year. The 411A, produced from 1967-68, featured a redesigned nose and more baggage space. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. Save my name, email, and website in this browser for the next time I comment. . Answer: The process of delivering compressed, denser air to a combustion engine is referred to as forced induction. This can be remedied by fitting the aircraft with speed brakes/spoilers or installing a liquid cooling system to the engines. (38.0 gallons/hr @ $5.40/gal), Misc: landing, parking, supplies,catering, etc, Typical Price: $307,752.00 (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. 5 Landing Distance: 3,170 ft (966 m) Maximum Operating Altitude 45,000 ft . (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. }.tdi_115.td-a-rec-img{ 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. 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. 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. The Chancellor 414A has an impeccable safety record. (2001, February 26). kt, ROD Ball at 219-749-2520. 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). This is when Cessna decided to take advantage of Continental Motor's then-new, 225-horsepower O-470-A engine and develop the robust Cessna 180, which first flew in May 1952. 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. A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. Aviation Consumer. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. Derived from the Model 411, the Cessna 401 and 402 are essentially the same aircraft put to two different uses. According to Aircraftcostoperator.com, the average total hourly cost of operating a Cessna 414A is roughly $535. In the early 414s, the main landing gear webbing is prone to cracking, requiring extensive rectification. Take an early model 414 with -J engines and complete this upgrade to receive a 1600 hour TBO, up from the original 1400. The greater the experience of the owner/pilot, the lower the premiums. Gross wt. With rare exception, all 414As have an aft potty. When pilots are flying IFR, it means they are under the control of Air Traffic Control. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. Mike Buschs Savvy Owners seminar is valuable. Cessna Country: United States Manufactured: 1972 to: 1984 ICAO: C340 Price: US$.36 million (1982) Performance Weights Dimensions Avionics: Garmin G500 PFD Engine: 2x Continental TSIO-520-NB Piston Power: 310 horsepower Max Cruise Speed: 244 knots 452 Km/h Approach Speed (Vref): 71 knots Travel range: 1,406 Nautical Miles 2,604 Kilometers I bought it to replace a nice Cessna T310R, which I flew for about a year. It can carry up to 8 passengers and baggage, or full fuel, but not both. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). The aircraft can seat up to eight passengers and one or two crew. Other modifications in 1978 included a longer nosecone, a redesigned undercarriage system, and an extended wing without the earlier tip tanks. All rights reserved. Quality initial and recurrent training is critical. Specs, range, speed, operating weights and performance for the Cessna 340 here. He was a glider pilot for several years before obtaining his private license in taildraggers. 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. The 414A has an excellent safety record for good reason. The more the industry drags out phasing out 100LL, the more susceptible it is to looking unconcerned about public health risks. Send feedback comments to the EUROCONTROL Training Institute. The STANDARD DATA: Seats 6-8. 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. m. All data presented is only indicative and should not be used operationally. 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. Total Cost of Ownership: $39,555.22 Service ceilings are above 30,000 feet, but few owners fly that high. Pay attention to the fuel system in tip-tanked 414s. Answer: Maximum structural cruise, or Vno, refers to the airspeed above which the aircraft should be flown only in smooth air. The turbocharger is connected to both the exhaust and intake manifolds of the engine. 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. Range 568-1,322. The 414A has a combined 620 hp (456 kW), however, takeoff acceleration might not be as neck-snapping as one would assume. 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. The 414 and 414A are popular aircraft with considerable numbers worldwide, and unless some economic or aircraft supply-side variable changes, you can expect your 414 to command a reasonable resale price from someone needing a serious, cabin-class, high-performance twin. kts, ROC This AD has a compliance time of 400 to 800 total time. However, it takes a longer distance high wing loading aircraft to takeoff and land. Cruise mph 223. One of the most distressing issues the Cessna 414A has is cracking along the forward wing spars. In 1979, the 402s received a new wing, with a 5 feet (1.5 m) greater span. 110 Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. 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. 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. I use SimCom. The average price for a used Cessna 414 at the time of print was US$230,000, having approximately 6,000 hours total time airframe (TTAF) and engine times of around 800 hours. Most had the RAM VI engine conversion. 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. Membership in and attending the Twin Cessna Flyer Organizations Pilot Seminars should be required. .tdi_115.td-a-rec-img { Continental also published overhaul procedures to enable -NB engines to get the TBO boost. The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. 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. 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.