Soaring Good Looks. Please send us your experiences on your aircraft. I am a professional aircraft broker who specializes in Twin Cessnas. 720 The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. Gross wt. 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 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.Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. 16 Otherwise, the periodicity is 1,600, or 200 hours depending on the mod state. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. 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. 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. Top mentions include the true cabin class, reasonable cruise speed, and maintenance of sea-level pressure to 10,000 feet. 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. Ceiling 29,800. (See www.ramaircraft.com. Even with aging aircraft and occasional engine-related issues, the 414A offers a large cabin, the comfort and convenience of pressurization and the performance and safety of turbo charging. 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. When pilots are flying IFR, it means they are under the control of Air Traffic Control. Optional auxiliary and locker tanks were available to boost usable capacity to 180 gallons, then to 203 gallons in 1973. They offer technical help and forums for members to discuss everything and anything about their aircraft. The Cessna 414 Chancellor was produced from 1968 to 1985. It was developed to bridge the gap between the unpressurized Cessna 401 and the pressurized, more powerful Cessna 421. Pay attention to the fuel system in tip-tanked 414s.A simpler fuel system was among a host of improvements unveiled in 1978 with introduction of the Model 414A Chancellor. Some potties have a flushing feature. 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. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. 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. Some low-time pilots might be approved for 340 insurance, but rejected for a 414/414A. 3,865. 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. It also has a TBO of 1,400 hours which is low even for a turbocharged engine. Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. The aircraft has a maximum takeoff weight of 3,061 kg and a maximum landing weight of 2,697 kg. Power. The 375-HP 421Cs single engine ceiling is 14,900 feet. 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. (Beginning in 1957, horsepower was modestly increased to 230.) They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. Speed brakes/spoilers are available from PowerPac Spoilers (www.powerpacspoilers.com) and more advanced intercoolers come from American Aviation (www.americanaviationinc.com). Its the third model in the Chancellor line and the successor to the Cessna 414II. An STC is an approved modification to an aircraft, engine, or component. Pilots love the 414 for the roomy cockpit, thoughtful systems layout, and good visibility. The compressed air is then cooled down, which makes it denser, on its way to the cabin. Although the 414s have a huge cabin-class interior, the stock airplane has never been a tremendous load hauler. 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. - Features that would be useful to you. Passengers love it for space, comfort, and low noise levels. If followed carefully, a mechanic wont miss anything. Full fuel allows the Chancellor 414A to fly for roughly four and a half hours, IFR reserves included, and has enough load leftover to carry six standard passengers, and not a pound more. The pressure of the cabin is usually around 8,000 ft but can be less according to how the system is set up. Come join us! The engine is notorious for cracked cylinders and therefore requires periodic inspections. 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. Fuel transferred too early is pumped overboard. 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. 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. However, it takes a longer distance high wing loading aircraft to takeoff and land. 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. 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. 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). The efficiency of the 414As long high-aspect ratio wing is highlighted by noting the 414As single-engine service ceiling is 19,850 feet. 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. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads. Accident statistics suggest that no common threads are pointing to the system or design problems on the 414. Answer: FAA refers to the Federal Aviation Administration, and PMA means Parts Manufacturer Approval. 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. Handling is good, too. Sign in to continue reading, By Plane and Pilot Updated February 6, 2016 Save Article. Stall mph 79. Phone: (305) 342-0760. 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. GlobalAir.com is your partner in connecting you with relevant information and resources. Balloons And Runway Calamities: Why Wait To Panic? Areas that require increased scrutiny and service are the exhaust system, crankcase, engine mounts, and magneto blocks. https://www.federalregister.gov/documents/2005/06/14/05-11613/airworthiness-directives-cessna-aircraft-company-models-402c-and-414a-airplanes, Cessna 414. . The more generic components such as filters, wheels, tires, and brakes are off the shelf and stocked by large aviation suppliers like Aircraft Spruce & Specialty or Wag Aero. By. Features wing of CESSNA 402 and fuselage of CESSNA 421. Best Cruise: 229 KIAS (See page 25 for an abbreviated AD list.). - Aircraft data that you believe is inaccurate or have specific experiences. Ball also says that heated windshields should be checked often to ensure there are no cracks. 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. Optional auxiliary and locker tanks were available to boost usable capacity to 180 gallons, then to 203 gallons in 1973.The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. Replacing the cylinder heads requires money and time, which will increase your engine overhaul costs by $6,000 bringing your grand total to $39,000. One former owner even stated that anyone who says the aircraft is reliable is delusional. A brand new engine exchange from Continental costs an average of $60,000. Landing distance (50) 1,790. kt, MCS The aircraft factors are: These terms are all within the control of the owner. Therefore, finding parts to support the aircraft is not difficult. 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. The same long-stroke, trailing-link landing gear common to all Citation jets allows the softest landings and smooth taxiing. Once it reaches the cabin it is compressed enough to create an atmospheric pressure that mimics the desired altitude. B. C. (2015, July 13). The Cessna 340 is a pressurized six-place twin featuring center-aisle seating, an air-stair door, and top cruise performance. 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. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). 230 The 414 is a reasonably sophisticated, older, twin-engined aircraft, and if not managed and maintained appropriately, maintenance costs can spiral. It has a take-off distance of 665 meters and a landing distance of 718 meters. Bombardier Challenger 350 Guide and Specs: Is It Up to the Challenge? The Achilles heel of the airplane for me has been the cabin heater. 5 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. Always remember where the wind is coming from and adjust the pattern accordingly. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. Answer:The flaps extend to 45 degreesThe TSIO-520-NBs red-line is 2700 RPM. What a difference! 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 number of maintenance problems that can and do arise can cost a lot of money in a short time frame. Owners speak of the 414s smoothness, stability, and ease with which you can trim the aircraft out. Takeoff distance (50) 2,220. Initial climb rate 1,900. Each of its 620 hp has to carry 10.8 lbs, which is quite poor. Stall mph 81. 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. Finding replacement parts for a 414A is not as tough as one would think thanks to its shared parts with the 401 and 421. } Chancellors are as roomy as 421B/Cs. Buyers should be looking carefully for compliance. (2005, June 14). margin: 0 auto 0 0; ft/min, TAS 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. A cabin differential of 5.0 psi allows a 10,000-foot cabin at 26,500 feet. Cruise mph 277. 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 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. Heres an even more interesting thing-normally, the RAM engines want to gulp down 19 to 22 GPH a side at higher power settings. He received his training at the University of North Dakota and has been in love with aviation for many years. Description Four variations are available, all of which offer a boost in useful load, increased TBOs and new props. kts, ROC 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. Ownership and operating costs. Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Your email address will not be published. In 1973, an updated 414 was released with major changes, this model was named the 414II. Utility twin aircraft. 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. https://cessnaowner.org/414-chancellor/, estaff. We are a collective group of airline instructors, and pilots dedicated to all things aviation. Aviation Consumer. Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. The Chancellor replaced the former 414 in 1978 and offered a new level of payload performance, range, and fuel efficiency. Six seats were standard; a seventh was available as an option. Based on 450 hours a year and fuel cost at $5.00 per-gallon, the CESSNA 414A has total variable costs of $233,550.00, total fixed costs of $73,885.00, and hypothetical summary cost of $307,435.00. Description Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. Maximum operating altitude of 30,800, a optimal cruise speed of 203 knots/234 MPH, and a 705 NM/811 SM seats-full range. Of note is AD97-26-16 requiring an X-ray inspection of the engine mount beams for fatigue cracking. 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 . A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. 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. Propeller- to-fuselage clearance is more than 31 inches for a very quiet cabin. Find more About Us here! For 1976 the airplane was equipped with a propeller synchrophaser to control propeller RPM and phase relationship of the blades, engine-to-engine. Answer: The process of delivering compressed, denser air to a combustion engine is referred to as forced induction. Range 568-1,322. (See www.ramaircraft.com.). Controls consisted of on/off/crossfeed valves and a fuel flow computer/indicator was added. One of the biggest weak points of the 414A is the problematic Continental TSIO-520-NB engine. 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 The Cessna 414 is a low-wing, twin piston engine, pressurized-turbocharged aircraft produced by Cessna from 1970 until 1985. When we look at the power loading of the aircraft, the why becomes obvious: weight. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor. 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 Interested in buying this aircraft click here. [1], In 1974, American Jet Industries built a turboprop-powered conversion of the Cessna 414, named the Turbo Star Pressurized 414, using Allison 250-B17B engines. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. It's the third model in the Chancellor line and the successor to the Cessna 414II. Before doing so, however, the pilot has to ensure there are fewer than 20 gallons in each main (tip) tank. Copyright permission must be sought from EUROCONTROL. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. The most significant and popular modifications that can be made to a 414A are the engine swaps by the RAM Aircraft Corporation. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. The landing gear was replaced, using the simpler system from the Cessna 414. Ball at 219-749-2520. 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. ft/min, IAS The model 414, a 411 derivative introduced in 1970, utilized the 421s fuselage and tail unit with the 401s wings. Like most all twin Cessnas, we give the 414 high marks for cockpit ergos, and the logical layout of systems and controls makes the flight deck a comfortable place to chew up the miles. Although you could fly for about 1,100 miles, you would be able to bring only two friends and a few bags. To offset the reduction of performance because of the weight increase, the wing area was increased by 30 ft (2.78 m). It had basically the same tail and wide-oval fuselage as the 421B, and the 401s wing. The basic 414 was born in 1970 with a 4.2 psi pressurization differential and ascended to become the Chancellor in 1978. However, as aircraft age, they dont get cheaper to own or operate, which the price will reflect. The top of the line for the 414 is the series VI. 3,467. A typically equipped 414A has a full-fuel payload of about 500 to 700 pounds, depending on equipment. kts, ROC Cessna's 414 is among a large group of aircraft headed for extinction. That resulted in cruise speeds of only about 180 to 185 KTAS up high. 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. 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! no data Empty wt. Fuselage strakes improve yaw control, performance in turbulence, and a higher cruise speed. Ceiling 26,000. fitness for any purpose is made or implied. An AD that requires the propeller hubs to be filled with red indicator oil to make cracks more visible was also released. Maximum luggage capacity of 85.00 ft^3; 31.00 ft^3 being internal and 54.00 ft^3 being external. Go figure. by Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. Distinguishing features are: retractable landing gear and three-bladed, constant speed, fully feathering propellers. However, only upon acquiring the 414 did I finally attain my goal-virtually complete independence from the airlines for domestic travel. Annual inspections, repairs and pre-buys must be conducted by specialists. [2] Scenic Airlines of Las Vegas purchased the rights to the design in 1977.[3]. Each engine spun a constant speed, three-blade McCauley propeller. LED landing and recognition lights offer enhanced visibility and strong illumination for night flying. Answer: TTAF stands for Total Time Airframe, which refers to the number of flying hours the airframe has accumulated since new. 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. I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. Gross wt. Bringing the grand annual total to $240,785. (RVSM rules have generally limited 414s to 28,000 feet.) 4.0 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. It has a range of 1,328 nautical miles and a climb rate of 1,520 feet per minute. The top of the line for the 414 is the series VI. The change allowed the engine to produce 310 hp (228 kW) at 2700 RPM from sea level to 20,000 ft (6,096 m). 2023 Madavor Media, LLC. In service since 1969. On a standard day, when loaded to MTOW, it needs 4,000 ft (1,219 m) to hit Vr and then come to a complete stop. 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. 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. Takeoff distance (50) 2,010. Ceiling 26,180. Both refer to ratings or approvals that a pilot must achieve to enable the operation of a multi-engined aircraft or flight under instrument flight rules. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. no data The 414A, aka Chancellor, was introduced in model year 1978 with the last built in 1985. 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.Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. However, most owners report that after a few hours of flying, it requires little thought. )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. text-align: left; 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. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. I have split my time about equally between the RAM IV 325-HP engines and the RAM VII 335-HP engines and Scimitar props that I had installed when the RAM IVs hit their TBO. The 414 seats up to 6 passengers plus 1 pilot. All rights reserved. No warranty of Cessna 414As that comply with all their service bulletins and airworthiness directives, have been maintained well, and dont have too much time can fetch a good price. The STANDARD DATA: Seats 6-8. The resale value increases greatly if a RAM conversion has been done and additional performance modifications have been fitted. The prices range from low-hour models with less than 4,000 hours TTAF, which are selling for just over US$385,000, while older aircraft from the early-1970s will sell for approximately US$150,000. Cessna 414 chancellor. Average price for used aircraft CESSNA 414A is $344,804.81. 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 main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. But the average price of a 414A is around $300,000, while the price range is between $200,00 $500,000.
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