The 1970 to 1972 models are referred to as short-bodied 414s. 16 (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. 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 That is why an approval to modify them is classed as supplemental. When we're not in the air, we're here helping others how to join us here at Aviator Insider. 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). By all accounts, vortex generators reduce Vmc and stall speeds. Gross wt. MicroAerodynamics VGs provide a 350-pound gross-weight increase. Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. Bombardier Global 8000 Guide and Specs: Superior Sonic Transportation, Embraer Legacy 450 Guide and Specs: The Stepping Stone, Bombardier Challenger 300 Guide and Specs. Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. Then in 1976, Cessna upgraded the engines to the newer -N series TSIO-520 offering a higher manifold pressure at 2700rpm, allowing the engines to maintain rated horsepower to 20,000 feet. 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. 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. The Cessna 414 is an incredibly popular pressurized cabin-class twin, with almost 650 registered in the US alone. I have put in three different heaters over the past several years and changed out all the blower motors, ductwork, fuel pump, fuel pressure regulator, igniter, air flow sensor and thermostat at least once and I still plan for failure in flight. The difference is that an -N engine uses 38 inches of manifold pressure, rather than 36 inches, and 2700 RPM to produce its rated 310 horsepower. Power. Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. } Fuel burn is the same, 34 GPH in cruise at all altitudes, with the RAM VII at 69 percent. The cabin length is 3.5 meters, height is 1.3 meters, and width is 1.4 meters. STOL kits can also be purchased to help reduce the field length of the aircraft. 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. The new design used the same fuselage and tail as the 421 and the wing from the 402. Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: Takeoff distance (50) 1,662. Required fields are marked *. Thielert has offered engine conversions using their Centurion Engines. Landing distance (50) 1,790. One of the most important came in 1973, when cabin length was increased 16 inches and a fifth side window was installed. In a study of accident records some years ago, the 414 stood out as the safest light twin. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. ) The difference is that an -N engine uses 38 inches of manifold pressure, rather than 36 inches, and 2700 RPM to produce its rated 310 horsepower. Preferred Airparts, based in Ohio, provide worldwide customers with surplus new Cessna original components and used parts from dismantled aircraft. ft/min, IAS The 1973 to 1977s are the long bodies. The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. Seating is spacious and available in a variety of arrangements. (n.d.). Although you could fly for about 1,100 miles, you would be able to bring only two friends and a few bags. Takeoff distance (50) 2,175. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. The exhaust system sees a great deal of heat and vibration, thus components wear out. Range 568-1,322. Cessna 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. Its an excellent idea, regardless of how much time you have. Empty wt. 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, the big Cessnas have safety records that are unmatched by any other light twin. By continuing to use this website, you are agreeing to our Cookie Policy. Overall, the 414A is a capable aircraft. 6,200: 6,430: Zero Fuel Weight - lbs. Answer: IFR means Instrument Flight Rules. 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. . (38.0 gallons/hr @ $5.40/gal), Misc: landing, parking, supplies,catering, etc, Typical Price: $307,752.00 Landing Weight - lbs. 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. 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. ft/min, IAS 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. Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. The landing gear track was also increased by 4 feet (1.2 m). The Cessna 340 is a pressurized six-place twin featuring center-aisle seating, an air-stair door, and top cruise performance. 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. A 414A RAM Series VII with Winglets (AW) will compete in many ways with a 421C. Baggage capacity of the 414 is 930 pounds, and cabin seating is available with an array of executive options. 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. Twin engine piston aircraft with retractable landing gear. The 414A, aka Chancellor, was introduced in model year 1978 with the last built in 1985. Description Four variations are available, all of which offer a boost in useful load, increased TBOs and new props. This has made insuring a 414 tougher. Absolutely the Right 414A RAM IV, This Aircraft is Impeccable and reflects the condition and attention to details that this owner has given N414EM with Only 20 Hours on each RAM Engine and 20 Hours.See More Details. These aircraft were called the 414A Chancellor. The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. 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. With 1000 pounds of fuel, the payload may be 400 to 600 pounds. The pressure of the cabin is usually around 8,000 ft but can be less according to how the system is set up. Although not required on my serial number for many thousands of more hours, I had the spar strap mod installed and I cant emphasize enough how happy I am that I did it. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Cessna 182 vs 185 Compared: Which Is Better? They offer technical help and forums for members to discuss everything and anything about their aircraft. The package that gives the 414A the most significant boost in performance is the series V upgrade. The landing gear is the same as the 414, but the horizontal and vertical stabilizer, elevator and rudder are the same as the 310; minor changes in the 310 tail make it interchangeable with the 340. General characteristics Crew: one or two Capacity: four to six Length: 36 ft 4 12 in (11.09 m) Wingspan: 44 ft 1 12 in (13.45 m) Height: 11 ft 5 12 in (3.49 m) Wing area: 225.8 sq ft (20.98 m 2) Empty weight: 4,368 lb (1,981 kg) Max takeoff weight: 6,750 lb (3,062 kg) Fuel capacity: 213 US gal (177 imp gal; 810 L) usable An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. 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. Thus, it is an indication of age and use. Finally, in 1979 the -NB series TSIO-520 engines were installed, providing an improved crankshaft, and in time, an increased engine TBO of 1600 hours against the -Ns 1400. 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. Liability coverage covers damage caused by the aircraft, including passengers, while hull coverage covers damage to the aircraft itself. 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. Otherwise, the periodicity is 1,600, or 200 hours depending on the mod state. It was developed to bridge the gap between the unpressurized Cessna 401 and the pressurized, more powerful Cessna 421. The aircraft was labeled the Chancellor in 1976. However, it takes a longer distance high wing loading aircraft to takeoff and land. Landing distance over 50-ft obstacle: 2,393 ft: Landing distance, ground roll: 1,013 ft: Limiting and . 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. Fuel cost per hour: Speed brakes/spoilers are available from PowerPac Spoilers (www.powerpacspoilers.com) and more advanced intercoolers come from American Aviation (www.americanaviationinc.com). When we look at the power loading of the aircraft, the why becomes obvious: weight. no data Distinguishing features are: retractable landing gear and three-bladed, constant speed, fully feathering propellers. Take an early model 414 with -J engines and complete this upgrade to receive a 1600 hour TBO, up from the original 1400. The mod is expensive, but in my case we found serious factory mis-drilled wing spar attachment holes that could have caused a spar failure at any time! Some potties have a flushing feature. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. 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. According to BWI Fly, for liability coverage of $1,000,000, a qualified pilot of a 414A who aims to use the aircraft for private use can expect to pay around $840 $1,400 per year and $4,400 $5,800 per year for a combination of the liability and hull coverage of $225,000. Phone: (305) 342-0760. 414 chancellor. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. Thielert claims increased power and improved fuel economy over other available conventional piston engines. Its wings are borrowed from the Model 414. Also says to increase landing distance by 45% (doesn't seem to make sense). 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 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. Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. 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. Cessna made more room for roughly 410 lbs (185 kg) baggage and equipment such as avionics by fitting on the nose of the 421 onto the 414A to which made the aircraft longer. Down low under 10,000 feet, things are much slower, more like 170 to 175 KTAS. 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 of their own design for the 414A to improve its aerodynamic performance. Operating and maintenance costs are attractive when compared with those of competing airplanes, such as the big-brother 421 and Beech Aircrafts Duke. )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. Landing Distance: 2393 ft: 729 m: Max Takeoff Weight: 6751 lbs: 3062 kg: Max Landing Weight: 6750 lbs: 3062 kg: Useful Weight: 2417 . Plane and Pilot expands upon the vast base of knowledge and experience from aviations most reputable influencers to inspire, educate, entertain and inform. 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. Engines two 285-hp turbocharged Continentals. 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. 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.The exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. RAM also makes winglets and vortex generators. Passengers love it for space, comfort, and low noise levels. One of the most important came in 1973, when cabin length was increased 16 inches and a fifth side window was installed. Six seats were standard; a seventh was available as an option. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. If the insurance includes additional hull cover for US$225,000, the annual premium for the experienced pilot will be between US$4,400 to US$5,800 per year, while the lesser experienced pilot can expect US$5,700 to US$12,000 per year. He received his training at the University of North Dakota and has been in love with aviation for many years. 1200 You Tell Us, EAA To Host Webinar Event For Aspiring Aviators, National Museum Of The U.S. Air Force Celebrates 100 Years, FAA IACRA System Hit With Database Issues, FAA Nominee Quizzed On Aviation Knowledge, General Aviation Accident Bulletin, February 27, 2023, Pratt & Whitney Canada Passes One Billion Flight-Hour Milestone, AeroLEDs Introduces New Landing Light Series, Universal Avionics Receives TSO Approval For Aperture, MyGoFlights Head-Up Display Division Sold To Partner, AeroBrigham. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. In 1973, an updated 414 was released with major changes, this model was named the 414II. The crosswind characteristics are good, and its easy to make squeaker landings. Engine and aerodynamic modifications abound for the 414. Mike Buschs Savvy Owners seminar is valuable. - Aircraft data that you believe is inaccurate or have specific experiences. kt, ROD ft/min, TAS Other modifications in 1978 included a longer nosecone, a redesigned undercarriage system, and an extended wing without the earlier tip tanks. Pricing Cessna 414 Stock Airplane vs. RAM Series VII; Primary Specifications Cessna 414 GlobalAir.com is your partner in connecting you with relevant information and resources. Straight 414s with only 310-HP standard engines or even with a 325-HP RAM Series IV conversion will often have low useful loads. 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: - 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. The engine is notorious for cracked cylinders and therefore requires periodic inspections. Landing Distance: 3,170 ft (966 m) Maximum Operating Altitude 45,000 ft . A direct competitor of the 414A is the Beechcraft King Air. The Chancellor utilizes the hydraulic components of the Golden Eagle gear and features a five-second retraction time. Cruise mph 277. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. The nose baggage compartment of the 414A made CG juggling easier. The aircraft also featured a 28V, negative ground, direct current electrical system charged by an alternator on each engine, and a 24V battery. The 414A has an excellent safety record for good reason. The 414A has an issue with shock cooling of the engine that occurs during rapid descents. It featured major modifications, including a restructured and increased wingspan, incorporating integral fuel tanks, and a stretched nose to allow more space for baggage. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads.The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. Annual inspections, repairs and pre-buys must be conducted by specialists. ), 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. The maximum takeoff weight went up to 400 pounds to yield a higher useful load. That resulted in cruise speeds of only about 180 to 185 KTAS up high. Cessna 195 Guide and Specs : All About The 195 Businessliner, Bombardier Challenger 300 Guide and Specs, Installed equipment, specially avionic fit-out. 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. fitness for any purpose is made or implied. Engines two 375-hp turbocharged Continentals. 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 Ceiling 29,800. With rare exception, all 414As have an aft potty. VGs are also available from Micro Aerodynamics (www.microaero.com) and V/G Systems, phone 800-328-4629. 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.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. ( 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 414A has a single-engine ceiling of 19,850 ft (6,050 m) which is the best among all its peers. Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. 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. Cruise mph 223. Even though Cessna Chancellor 414A has a good safety record, the earlier 414s and their complicated fuel system have caused a few scares, the most recent one in 2018. Once it reaches the cabin it is compressed enough to create an atmospheric pressure that mimics the desired altitude. These aircraft were called the 414 Chancellor. Copyright permission must be sought from EUROCONTROL. They can be purchased from Micro Aerodynamics and VG Systems. Ive previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. Specs, range, speed, operating weights and performance for the Cessna 340 here. Each engine spun a constant speed, three-blade McCauley propeller. Improved version CESSNA 414A Chancellor (appeared in 1978) with bonded wet wing, without tip tanks. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). No warranty of Balloons And Runway Calamities: Why Wait To Panic? - Aircraft specific reviews and articles. 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. (2005, June 14). However, a 414 RAM VI and VII can often have an excellent useful load with an impressive range/payload chart. With a range of approximately 2,200 nautical miles and a relative low cost, the Conquest II was an unparalleled aircraft in its time. However, it isnt just an engine swap. 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.