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no data There were significant changes made to the body of Chancellor 414A as well. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. 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. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. 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 fuel system composed of a pair of main tanks and fuel selectors, emergency cross-feed shutoff valves, and other crucial parts to complete the system. Straight 414s with only 310-HP standard engines or even with a 325-HP RAM Series IV conversion will often have low useful loads. The Chancellor has a service ceiling of 30,800 feet and a maximum speed of 235 knots. What a difference! It can carry up to 8 passengers and baggage, or full fuel, but not both. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. Since 2017 he's been working as a content writer and loves that he can combine his love of aviation and writing here at Aviator Insider. The system left room for error, not only on the part of the pilot, but among line personnel. The engine is notorious for cracked cylinders and therefore requires periodic inspections. When discussing 414s and 414As, one must speak correctly. Stall mph 81. It is the flying carpet my wife always wanted, including a potty! ) Annual inspections, repairs and pre-buys must be conducted by specialists. 310, Range 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. Its the third model in the Chancellor line and the successor to the Cessna 414II. 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 longer fuselage now allowed for an eighth seat to be added as an option. (38.0 gallons/hr @ $5.40/gal), Misc: landing, parking, supplies,catering, etc, Typical Price: $307,752.00 }googletag.cmd.push(function() { googletag.display('inline'); });288All 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. NM, ROD 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. Checking the Cessna 152 POH it says to increase takeoff distance by 15% of ground roll (makes sense due to increased friction). To get at the fuel in the wing locker tanks, it must first be transferred to the mains. 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. STANDARD DATA: ( 411) Seats 6-8. Takeoff distance (50) 2,175. Operating Costs. 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. In 1979, the 402s received a new wing, with a 5 feet (1.5 m) greater span. Landing Weight - lbs. 3,865. 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. The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. fitness for any purpose is made or implied. - Aircraft specific reviews and articles. With the rise in FAA-PMA approved manufacturers, many have niched down to support a particular aircraft type and finding trim (knots2u, Texas Aeroplastics or AvFab), landing gear components (Robair Repair), or lighting (Whelen Aerospace Technologies or AeroLeds) for your 414 is not hard. kts, ROC Cessna Owner Organization. quantity indicators, both with three-position switches, to help the pilot keep track. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. Their parts may seem expensive, but they continue supporting us owners, and for that I am very willing to see them earn afair profit. In the years following its introduction, the airplane saw few major changes. 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. 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. 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. The 414A can be upgraded with the usual performance boosters such as vortex generators, which are highly recommended. The figures show that the demand for Dakotas has increased causing prices to rise by about 40 percent. 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. This can be remedied by fitting the aircraft with speed brakes/spoilers or installing a liquid cooling system to the engines. Of course, any airplanes safety depends a great deal on the proficiency of its pilots. The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. List price was $138,000 (thats over $740,000 in 2007 dollars)-$35,000 less than the Duke and some $50,000 less than both the 421 and Pipers P-Navajo. In my Cessna 152, a 20-knot headwind increases the glide angle from 5 degrees to 7.5 degrees, a 50-percent increase. 100 Ceiling 29,800. Fuel transferred too early is pumped overboard. Seating is spacious and available in a variety of arrangements. Find more About Us here! When discussing landing distance, two categories must be considered: Actual landing distance is the distance used in landing and braking to a complete stop (on a dry runway) after crossing the runway threshold at 50 feet; and, Required landing distance is the distance derived by applying a factor to the actual landing distance. The aircraft got heavier, with the MTOW and landing weight increasing by 400 lbs (181 kg) and 550 lbs (249 kg), respectively. Range 568-1,322. Cessna Country: United States Manufactured: 1972 to: 1984 ICAO: C340 Price: US$.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 The 375-HP 421Cs single engine ceiling is 14,900 feet. airplane 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. Its an $800 part.MODS, CLUBSAmong the most popular mods are the RAM Aircraft Corporation engine swaps. As has often been said, Cessna really got it right with the 414/414As. Among the most popular mods are the RAM Aircraft Corporation engine swaps. Most had the RAM VI engine conversion. The CESSNA 414A has a 2,530 runway length (or runway plus clearway and/or stopway) and 3,055 actual landing distance required. Takeoff distance (50) 2,220. Though its Continental engines could maintain their rated power at higher altitudes, Cessna implemented manifold pressure limitations above 20,000 ft (6,096 m) to prevent excessive engine temperatures. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. Most are the basic bucket.. (See www.ramaircraft.com.). It is a less powerful and lighter evolution of the Cessna 421. margin: 0 auto 0 0; Table of Contents Specifications Photo Gallery Description Manufacturer: Cessna Country: United States Manufactured: This can be a great aircraft and a good buy, but only for a pilot who doesnt need lots of payload. (2001, February 26). Insurance costs have equaled $7000 per year for the last couple of years for $1 million smooth with a hull value of $350,000. Range 489-1,242. The Chancellor 414A has an impeccable safety record. I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. 800 Each engine spun a constant speed, three-blade McCauley propeller. 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. 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. Oh, and the aft toilet. The original 414 was developed out of the fuselage of the Cessna 421 and of the wing of the Cessna 401. If an owner has taken a maintenance only as required approach to their aircraft, they can expect a far lower resale value. (n.d.). One of the biggest weak points of the 414A is the problematic Continental TSIO-520-NB engine. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. Would like to understand why. 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! Theres enough room in the aft cabin, the nose and wing lockers of a 414 to hold 930 pounds of baggage. The 421B tiptank twin Cessna has fuel carried in the mains (tips), auxiliary fuel cells in the wings and optional nacelle tanks. 6,165: 6,165: SOURCE: Sources. I own a 1978 Cessna 414A which I acquired in 1989. The Chancellors that cost close to $500,000 most often are pristine and like-new. By all accounts, vortex generators reduce Vmc and stall speeds. AOPA. 7,450. text-align: left; The new engine also has a TBO of 2,000 hours, which is a 600-hour increase from stock. 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. Cabin specifications: 04'03" cabin high, 04'07" cabin wide, and 11'03" cabin long. - Aircraft data that you believe is inaccurate or have specific experiences. Controls consisted of on/off/crossfeed valves and a fuel flow computer/indicator was added. Takeoff distance (50) 1,700. 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. kg, IAS Mysteries Of Flight: The Curious Case Of Pan Am Flight 914, Fond Farewell to a Titan: The Antonov An-225. Go figure. 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. Cruise mph 231. Range 1,284. The most significant and popular modifications that can be made to a 414A are the engine swaps by the RAM Aircraft Corporation. ft/min, TAS Finding replacement parts for a 414A is not as tough as one would think thanks to its shared parts with the 401 and 421. Continental also published overhaul procedures to enable -NB engines to get the TBO boost. Its an excellent idea, regardless of how much time you have. Flight planning or any other aircraft operations should only be done using official technical information provided The current concern is with wing spar cracking in high-time airplanes; with a series of ADs calling for inspections and modifications to the spar-compliance is expensive. 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. PERFORMANCE: Top mph 268. no data Ive previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); WORLD'S PREMIER INDEPENDENT AVIATION NEWS RESOURCE. The biggest club for owners and operators of a 414A or any large Cessna twin is the Twin Cessna Flyer club. It has an exterior length of 11.1 meters, a height of 3.5 meters, and a fuselage diameter of 1.5 meters. 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. Preferred Airparts, based in Ohio, provide worldwide customers with surplus new Cessna original components and used parts from dismantled aircraft. 414,Chancellor Over its production run the number of 414s and 414As were evenly split, with 516 and 554 built, respectively. Fuel capacity 202. (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35. 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. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. These aircraft were called the 414A Chancellor. It is a very stable instrument platform and I find it as easy to land as the T310 or any of the large singles Ive flown. With bigger turbochargers and intercoolers, much larger cowl flaps, new intake air scoops, and Scimitar props, the airplane becomes an entirely new animal within seconds of leaving the runway. The STANDARD DATA: Seats 6-8. The exhaust system sees a great deal of heat and vibration, thus components wear out. Four variations are available, all of which offer a boost in useful load, increased TBOs and new props. The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks. 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 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. Empty wt. 110 The new design used the same fuselage and tail as the 421 and the wing from the 402. This AD has a compliance time of 400 to 800 total time. [4] This involves the installation of FADEC-controlled aviation diesel piston engines that run on commonly available jet fuel. ft/min, IAS The pressurization and turbocharged nature of the aircraft mean it is complicated to work on, and specialization is needed. Gross wt. 6,500. Utility twin aircraft. Above this speed, turbulence or rapid control deflections increase the chance of structural damage. Ownership and operating costs. Rate of Climb: 1650 fpm; Climb Rate One Engine Inop: 315 fpm; Max Speed: 243 kts; Normal Cruise: 229 kts . Trevin is a licensed flight instructor and pilot with degrees in Commercial Aviation and Aviation Management. Answer: Gross Weight is the total aircraft weight, including pilots, passengers, fuel, oil, and cargo. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads. Power. Although you could fly for about 1,100 miles, you would be able to bring only two friends and a few bags. Already a member? Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. If followed carefully, a mechanic wont miss anything. Six seats were standard; a seventh was available as an option. Baggage capacity of the 414 is 930 pounds, and cabin seating is available with an array of executive options. However, a 414 RAM VI and VII can often have an excellent useful load with an impressive range/payload chart. No warranty of document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Your email address will not be published. Engines two 340-hp turbocharged Continentals. Takeoff distance (50) 2,010. text-align: center; 16 No warranty of }@media (max-width: 767px) { )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. 1100 One pilot and typical 6 passengers in main cabin. As we saw earlier, average prices sit between US$230,000 to US$280,000, yet highly modified and maintained aircraft command twice those figures. The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. The 1973 to 1977s are the long bodies. The main complaints seem to be an unnecessarily complicated fuel system requiring a distinct methodology for use. The takeoff distance is 408 meters while the landing distance is 365 meters. Crew-6 Launch Scrubbed For Ground Systems Issue, The Drip, Drip Of Bad Publicity About 100LL. The six- to seven-seat pressurized light transport is a step up for owners of the pressurized 340 and is fitted with the same 310-hp turbocharged engines. By. To keep CHTs below red line I had to fly at no more than 55 percent power and with the cowl flaps open at high altitudes. 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. While bad quality procedures in Wichita back in 1979 had probably caused my problem, the current staff at Cessna really impressed me with their efforts to help save this 27-year-old ship. Gross wt. They dedicated an engineer to my problem and working with my maintenance shop, they developed an approved repair for my wing, possibly saving the ship from the scrap yard! Maximal total range:705 NM / 811 SMCruise speed:203 knots / 234 MPHAverage price:$344,804.81Number of passengers:7 people, Your email address will not be published. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. In the early 414s, the main landing gear webbing is prone to cracking, requiring extensive rectification. 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. Bombardier Global 8000 Guide and Specs: Superior Sonic Transportation, Embraer Legacy 450 Guide and Specs: The Stepping Stone, Bombardier Challenger 300 Guide and Specs. Landing Distance: 3,170 ft (966 m) Maximum Operating Altitude 45,000 ft . In 1978, an enhanced version was launched, designated as the 414A Chancellor. 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. 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 aircraft is powered by two Continental TSIO-520-NB piston engines. The owners of Cessna 414As have mixed reviews. Specs, range, speed, operating weights and performance for the Cessna 340 here . 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. The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. Precise Flight and Spoilers, I. The crosswind characteristics are good, and its easy to make squeaker landings. 180 If you opt to go for a rebuilt engine from Continental will save you $6,000, for a total price of $54,000. The CESSNA 414A, production in 1978 1985, requires a one man crew and can be configured in 7 seats. 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. An STC is an approved modification to an aircraft, engine, or component. 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. Fuel capacity 102-207. 130 Required fields are marked *. The 414A has a combined 620 hp (456 kW), however, takeoff acceleration might not be as neck-snapping as one would assume. Copyright 2023 Aviator Insider | A Topsail Media Company | Powered by Astra WordPress Theme. The model 414, a 411 derivative introduced in 1970, utilized the 421s fuselage and tail unit with the 401s wings. 1000 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. EASY ACCESS Two large cabin doors allow for convenient entry and loading for student and instructor. Engines two 285-hp turbocharged Continentals. Engines two 375-hp turbocharged Continentals. Less powerful, light and low cost model of CESSNA 421 Golden Eagle. Approaching and landing with minimal power is a good habit. The Chancellor replaced the former 414 in 1978 and offered a new level of payload performance, range, and fuel efficiency. - Use this form or email to reach out to us: feedback@planephd.com. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). 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! He received his training at the University of North Dakota and has been in love with aviation for many years. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. 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. Please send us your experiences on your aircraft. In addition, the Chancellors wet wing has an increased fuel capacity of 106 gallons of usable fuel. The pressurized 414 was developed to appeal to owners of unpressurized, twin-engined aircraft, and was based on the fuselage of the Cessna 421 and used the wing design of the Cessna 401. When pilots are flying IFR, it means they are under the control of Air Traffic Control. ft/min, IAS The greater the experience of the owner/pilot, the lower the premiums. CESSNA 414A Ram V. Retrieved October 8, 2021, from https://www.aircraftcostcalculator.com/AircraftOperatingCosts/350/Cessna+414A+Ram+V, Continental 520 overhaul cost. The fuel economy of the 414A depends on the altitude, conditions, and power setting, but the general specific fuel consumption is approximately 0.44 lbs/hp/hr. Cabin specifications: 0403 cabin high, 0407 cabin wide, and 1103 cabin long. The engine is chock-full of new RAM components such as camshafts, cylinders, crankshaft, piston rods. 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. Specs, range, speed, operating weights and performance for the Cessna 340 here. Are COVID Vaccines Injuring Pilots? 2 x 310 HP Continental TSIO-520-NB turbocharged piston engines with 3 blade propellers. It featured major modifications, including a restructured and increased wingspan, incorporating integral fuel tanks, and a stretched nose to allow more space for baggage. Interested in buying this aircraft click here. Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. - Features that would be useful to you. Initial climb rate 1,900. 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. 414 chancellor. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. 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. 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. 520 Although the 414s have a huge cabin-class interior, the stock airplane has never been a tremendous load hauler. It has a range of 1,328 nautical miles and a climb rate of 1,520 feet per minute. The airplanes bonded wet wing is 4-1/2 feet longer than previous models and lifts an airframe that is 2 feet 8 inches longer from nose to tail. It is an approval granted to a parts manufacturer to manufacture specific aircraft components. 1000 Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. It is powered by two wing-mounted 310hp (231kW) Continental TSIO-520-J horizontally opposed, six-cylinder engines. 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. https://cessnaowner.org/414-chancellor/, estaff. CESSNA, V2 (IAS) They are the Cadillacs of the piston line, with attention having been paid to detail; even on an. Its an $800 part. Initial climb rate 1,610. Prices range from low-hour models of 2,750 hours TTAF, selling for just over US$575,000, while older aircraft from the late-1970s are selling for approximately US$230,000. Power was provided by twin 340-hp Continental engines, supercharged with AiResearch exhaust-driven compressors and turning full-feathering constant-speed propellers. Common are engine and aerodynamic modifications, including winglets. Engines two 340-hp turbocharged Continentals. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. 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. Interested in buying this aircraft click here. 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. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. Passengers love it for space, comfort, and low noise levels. 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.