Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. Would like to understand why. 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. Copyright permission must be sought from EUROCONTROL. (See page 25 for an abbreviated AD list.). 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. The Cessna 414 Chancellor was produced from 1968 to 1985. The engine is chock-full of new RAM components such as camshafts, cylinders, crankshaft, piston rods. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. Cessna Chancellor III (414A) Guide & Specs, Cessna Chancellor (414A) Performance and Handling, Piper Mirage Guide and Specs: All You Need To Know. Those owners who try to operate an aircraft like the Cessna 414 on a shoestring are pursuing false savings. Engines used were adaptations of the 300hp Continental TSIO-520s used on the 402. 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. 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. Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. Retrieved October 5, 2021, from https://www.aopa.org/go-fly/aircraft-and-ownership/aircraft-fact-sheets/cessna-414, Company, S. P. (n.d.). Continental also published overhaul procedures to enable -NB engines to get the TBO boost. The main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. 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. All told, Cessna built nearly 1000 of the airplanes-roughly a 50/50 split between early tip-tanked 414s and wet-wing 414A Chancellors-during 16 years of production. The Cessna 414 Chancellor is a light, pressurized, twin-engine transport aircraft with a pressurized cabin in service since 1969. RAM also makes winglets of their own design for the 414A to improve its aerodynamic performance. Empty wt. STANDARD DATA: (T310R) Seats 4-6. ) The V upgrade swaps out the Continental TSIO-520-NB for a more powerful big-bore, liquid-cooled Continental TSIOL-550A Voyager engine which produces 350 hp. 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. In my Cessna 152, a 20-knot headwind increases the glide angle from 5 degrees to 7.5 degrees, a 50-percent increase. Finally, the Riley Rocket 414 has two 400hp Lycoming IO-720 engines fitted. Fuel capacity 213-270. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. Landing distance (50) 1,790. 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. kts, ROC If you are looking for factory parts sites like CessnaParts, AircraftSpruce, and Knots2U have a large catalog of parts available for purchase.Cessna Chancellor (414A) Common Problems. A direct competitor of the 414A is the Beechcraft King Air. Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. 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: . Quality initial and recurrent training is critical. ( They are the Cadillacs of the piston line, with attention having been paid to detail; even on an288airplane of this vintage, only slight trim changes are needed when flaps or landing gear are reconfigured, although single-engine handling, as with any piston twin, is demanding and requires regular practice.The big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte. . 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 5,500. Cruise Speed: 224 kts: Fuel Capacity: 102 gal: Stall Speed (dirty): 70 kts: Range: 1090 nm: Takeoff: Landing: Ground Roll: 1695 ft: Ground Roll 805 ft: Over 50 ft obstacle . 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. Continental also published overhaul procedures to enable -NB engines to get the TBO boost.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). kt, MCS 720 Providing six seats as standard and an optional seventh, the aircraft appeared to private owners needing a comfortable long-range aircraft and corporate or charter organizations shifting people over short legs. Maximum operating altitude of 30,800, a optimal cruise speed of 203 knots/234 MPH, and a 705 NM/811 SM seats-full range. Thielert has offered engine conversions using their Centurion Engines. An engine rail replacement can cost an eye-watering $14,000. To better manage fuel, a fuel computer was added to the list of available options. MEL, in this case, refers to Multi-Engine Land. Description The engines were taken from the 402, with the only changes made to the setup were the inclusion of parts for bleed-air cabin pressurization, and different intercoolers. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. It is an approval granted to a parts manufacturer to manufacture specific aircraft components. 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. It also has a TBO of 1,400 hours which is low even for a turbocharged engine. Smart design means a better ride. 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. 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. Engine and aerodynamic modifications abound for the 414. For 1976 the airplane was equipped with a propeller synchrophaser to control propeller RPM and phase relationship of the blades, engine-to-engine. Ceiling 26,000. PERFORMANCE: Top mph 297. The 414A has an excellent safety record for good reason. On November 1, 1968, the prototype registered N7170C, conducted its maiden flight. There are only two fuel-288quantity indicators, both with three-position switches, to help the pilot keep track. The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. Landing distance (50) 1,815. 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. VGs are also available from Micro Aerodynamics (www.microaero.com) and V/G Systems, phone 800-328-4629. Checking the Cessna 152 POH it says to increase takeoff distance by 15% of ground roll (makes sense due to increased friction). ) 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! The package that gives the 414A the most significant boost in performance is the series V upgrade. Cessna 182 vs 185 Compared: Which Is Better? 6,500. 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. The Cessna 414 was given a clean wing in 1978. Answer: TBO means Time Between Overhaul, which is the manufacturers recommended running time, in hours or calendar time, before overhaul. The exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. Less powerful, light and low cost model of CESSNA 421 Golden Eagle. 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. With a range of approximately 2,200 nautical miles and a relative low cost, the Conquest II was an unparalleled aircraft in its time. .tdi_115.td-a-rec{ 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. Americas owner-flown aircraft enthusiasts and active-pilot resource, delivered to your inbox! } 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. no data For a private pilot with 1,500 hours total time, an IFR/MEL rating, 500 hours on multi-engined aircraft, and 25 hours on type, the 2021 cost per year for US$1,000,000 liability coverage is in the range of US$850 to US$1,400 per year. The top of the line for the 414 is the series VI. Stall mph 82. }.tdi_115.td-a-rec-img img{ The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. On the flip side, when fully loaded with eight passengers and baggage, there will be enough space for barely two hours of fuel. The RAM IV struggled in the flight levels, especially in the summer. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds.In the years following its introduction, the airplane saw few major changes. The system left room for error, not only on the part of the pilot, but among line personnel. Given the age and systems on the 414, plenty of airworthiness directives need reviewing for compliance. Bombardier Challenger 350 Guide and Specs: Is It Up to the Challenge? The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. The Chancellor replaced the former 414 in 1978 and offered a new level of payload performance, range, and fuel efficiency. Please send us your experiences on your aircraft. 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. The 414 is a low-wing cantilever monoplane with a conventional tail section and a retractable tricycle undercarriage. The Cessna 340 produced by Cessna. They can be purchased from Micro Aerodynamics and VG Systems. Come join us! The switch for that light is on the underside of a Tee fitting in the pressure line to the tail and thus fills with water, rust and crud and should be pulled and cleaned periodically, or it will fail. Landing Distance: 3,170 ft (966 m) Maximum Operating Altitude 45,000 ft . The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. The greater the experience of the owner/pilot, the lower the premiums. Ceiling 26,180. Kudos go to Cessna for rising to the occasion. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. The applications are smaller and they have maintenance issues, so the price does fall. 1000 The aircraft can seat up to eight passengers and one or two crew. Owners of 414As can opt for the series V conversion, which includes Continentals 350-HP liquid cooled Voyager engines, which have a TBO of 2000 hours. 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. Fuel cost per hour: Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. MicroAerodynamics VGs provide a 350-pound gross-weight increase. In 1979, the 402s received a new wing, with a 5 feet (1.5 m) greater span. 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 It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. Power was supplied by two horizontally opposed, six-cylinder, direct-drive, turbocharged, air-cooled, fuel-injected Continental TSIO-520-Js which produced 310 hp (228 kW). LED landing and recognition lights offer enhanced visibility and strong illumination for night flying. The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg. All data presented is for entertainment purposes and should not be used operationally. The wingspan is 13.46 meters, the wing area is 20.97 square meters, and the wheelbase is 3.3 meters. Finding replacement parts for a 414A is not as tough as one would think thanks to its shared parts with the 401 and 421. It did away with the extremely complicated and troublesome fuel system of the previous generations and replaced it with wet-wing fuel tanks that were 4.50 ft (1.37 m) longer and held 213 gal (968 l) total. Cessna 414 Stock Airplane vs. RAM Series VII; Primary Specifications Cessna 414 The aircraft has a remarkably high service ceiling of 30,800 ft (9387 m), but the normal operating range of a 414A is between 15,000 ft (4572 m) and FL250 (7,620 m). 520 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. Range 489-1,242. Six seats were standard; a seventh was available as an option. 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: Landing Weight - lbs. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. 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. 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. 1100 Landing Distance: 4000 ft; Performance. 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. Owners speak of the 414s smoothness, stability, and ease with which you can trim the aircraft out. Owners of 414As can opt for the series V conversion, which includes Continentals 350-HP liquid cooled Voyager engines, which have a TBO of 2000 hours. Answer: Wing loading is the total aircraft mass divided by its wing area. He's worked on various aircraft from small two-seaters like Tomahawks or Boeing 767s. They are the Cadillacs of the piston line, with attention having been paid to detail; even on an. The 414 and 414A truly provide a great family or business aircraft. The aircraft also featured a 28V, negative ground, direct current electrical system charged by an alternator on each engine, and a 24V battery. 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 Interested in buying this aircraft click here. 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. Top mentions include the true cabin class, reasonable cruise speed, and maintenance of sea-level pressure to 10,000 feet. Passengers love it for space, comfort, and low noise levels. Aerodynamic mods include vortex generators to increase aileron and rudder control authority at low speeds. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Real world speeds depend on engine configuration, but owners typically report 200 kts at about 38 gph in the upper teens. Above this speed, turbulence or rapid control deflections increase the chance of structural damage. It is the first GA airplane Ive ever owned or flown that treats passengers as comfort-seeking humans and not adventurous sardines. Landing distance (50) 1,765. . Flight planning cruise speeds appear to be between 190 to 200 knots with 37 to 38 mph fuel consumption while operating cost per hour for most owners is sub-$400. GlobalAir.com is your partner in connecting you with relevant information and resources. Takeoff distance (50) 1,662. Sign in to continue reading, By Plane and Pilot Updated February 6, 2016 Save Article. .tdi_115.td-a-rec-img { m. All data presented is only indicative and should not be used operationally. 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. And $34,235 for fixed costs such as insurance. At 11,350 feet, the 414's single-engine service ceiling is below average, but, at 19,850, the 414A is tops in its class. Speed brakes/spoilers are available from PowerPac Spoilers (www.powerpacspoilers.com) and more advanced intercoolers come from American Aviation (www.americanaviationinc.com). kt, Distance Also, the big Cessnas have safety records that are unmatched by any other light twin. This AD has a compliance time of 400 to 800 total time. No warranty of )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. It is our mission to be the go to leaders in the aviation industry. 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. We use cookies to help you get the best experience when using our website. 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. 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 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. 2023 GlobalAir.com. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. Landing distance (50) 1,815. 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 By all accounts, vortex generators reduce Vmc and stall speeds. There are four options, all of which provide a sizable increase in horsepower, increase the TBO, and newer, more powerful propellers. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. That resulted in cruise speeds of only about 180 to 185 KTAS up high. text-align: center; Fuel capacity 202. Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. Another great resource is the Cessna Pilots Association, it offers a monthly magazine, forums, technical information, and even training. Propeller- to-fuselage clearance is more than 31 inches for a very quiet cabin. Lots of external baggage in the nose and wing lockers, a pressurized aft cabin baggage area for desired in-flight items, like food, toys/games, cosmetics and a roomy pressurized 6000-foot cabin at 20,000 feet. Stall mph 82. 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. Takeoff distance (50) 1,700. 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. Takeoff distance (50) 2,220. Utility twin aircraft. 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. Send feedback comments to the EUROCONTROL Training Institute. If Cessna Kit SK414-19-1 is incorporated, the inspection is due every 9,600 hours. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. The piping which directs the exhaust from the manifold to the turbo is also susceptible to cracking. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. 7,450. The first Cessna Chancellor the 414 took to the skies in 1968, and was produced from 1970 onwards. Developed from the 310, it utilizes a similar landing gear and tail unit. Cessna made the most significant changes to the Chancellor when it introduced the 414A. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. They were the last of the pressurized, piston, 400-series airplanes Cessna developed, and pilots and mechanics will tell you that Cessna got it right with the Models 414 and 414A. Cessna 120 Guide and Specs : Is It Powerful Enough? The big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte.