The Cessna 404 was a development of the Cessna 402 with an enlarged vertical tail and other changes. 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. Cessna initially offered two models of what was at the time its largest piston twin: the 10-passenger Titan Ambassador, and a cargo/passenger version called … The pressure differential - five pounds per square inch - is greater so that the airplane can cruise at higher altitudes. It is powered by two 375 hp/280 kW turbocharged Continental Motors GTSIO-520 piston engines. Maximum useful load: 2417 lbs. Duration at max cruise: 5.67 hrs. 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.Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. Duration at econ cruise: 7.14 hrs. In addition, there is an AD (2005-12-13) on the 414 wing that requires a spar strap at 9,000 hours TT for aircraft with serial # 200 and lower. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. 288 The range numbers I derived from the average GS obtained from the GNS 530. Kudos go to Cessna for rising to the occasion. ROC: 1580 fpm. I sometimes carried a 50 pound bag of sand in the nose if I was flying single pilot with two people in the back and no baggage. I have had my share of problems with turbos, turbo controllers, cylinders and cracked cases. CE-414 Engine: 2 x Continental TSIO-520-N, 310 hp. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. Design and development. 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. I think if you don't need the extra space the operating costs between a 340 and a 414 would be fairly close the 340 is faster and smaller. With 1000 pounds of fuel, the payload may be 400 to 600 pounds. The Twin Cessna Flyer (www.twincessna.org) is headed by Larry A. Engines two 310-hp turbocharged Continentals. 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. Once again, SIDs are completely optional in piston Part 91 operations. Do you have any perspective on the significance of the differences of the 4141A over the 414 ? 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. 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! 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. Thanks, Mark (All the best for a good holiday weekend. Down low under 10,000 feet, things are much slower, more like 170 to 175 KTAS. Max range cruise: 209 kt. Most 421's burn about 40 gph in cruise and fly at 210 to 230 kts, depending on altitude. The Commander will do the same trip nonstop in 4 to 4.5 hours. The process from testing to certification was relatively quick. Equipped useful load: 2492 lb. The crosswind characteristics are good, and its easy to make squeaker landings. Membership in and attending the Twin Cessna Flyer Organizations Pilot Seminars should be required. 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. SE ROC: 510 fpm @ 86 kt. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. Cessna 414 Series Aircraft Information. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. Horsepower: 2 x 300 HP. CONCERNS: Payload: The 421 can be CG sensitive. On the old 414, fuel was carried in as many as six tanks, only two of which were standard equipment. Single-engine service ceiling: 19850 ft. 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. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. Service ceilings are above 30,000 feet, but few owners fly that high. Stalling speed clean: 82 kts. Climb gradient: 853 ft/nm. Gross wt. Thanks, Mark (All the … Seats: 7 / 8 CIDC Turbo Star 414 / Cessna 414 Engines: 2 x Allison 250-B17B, 420 hp. 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. Turbulent-air penetration speed: 144 kts. Some low-time pilots might be approved for 340 insurance, but rejected for a 414/414A. And I burn less fuel in the Beech 18! 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! 2. The Cessna 414 … 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. Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. Fuel Burn @ 75%: 32.0 GPH So, if its just pressurization youre looking for and youre going to be flying with only another person or two aboard, you might want to look at the 340 for a personal hot rod. The prototype Cessna 404, N5404J, began flight testing in early 1975 and Type Certificate A25CE was issued in July of the following year. A ramp weight of 6785 pounds was approved to allow for the consumption of six gallons of fuel during start, taxi and runup. Most are the basic “bucket.”. The prototype first flew on 26 February 1975. It’s a combination of the airstair door, large cabin, air conditioning, abundant baggage space, large picture windows, pressurization and -not to be discounted-the potty! RAM also makes winglets and vortex generators. 2. In many other countries, all Service Bulletins and SIDs are required. 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. The last of Cessnas cabin-class piston twins, used 414s and Chancellors are much in demand as owner-flown business and personal aircraft. It had basically the same tail and “wide-oval” fuselage as the 421B, and the 401s wing. 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. SE ROC: 240 fpm @ 105 kt. In real terms, a 34-gph burn in the 414 will cost you about $220/hr, a 42-gallon consumption would be $273/hr in the 421. Fuel, Known Ice, Heated Glass Windshield, Av... See More Details Horsepower for takeoff: 310 TBO hrs. Much has been written about the 414s, but its no big deal. (RVSM rules have generally limited 414s to 28,000 feet.) Fuel Burn @ 75%: 38.0 GPH. Scenic Air Lines, in 1977, acquired from American Jet Industries engineering and manufacturing rights for turboprop conversions of Cessna Models 402 and 414, now known as Turbo Star 402 and Turbo Star Pressurised 414. Modification of the Cessna 421C for installation of a Space Imaging System. Continental also published overhaul procedures to enable -NB engines to get the TBO boost. Fuel tanks The complexity of the fuel … Zero-fuel weight: 6515 lbs. Empty wt. Fuel Burn: 181 gph; Get a Jet Management Proposal for a Citation II How much does it cost to buy a Cessna Citation II 550? Once above 12,000 feet, the 414's turbocharging begins to ratchet up the speed, and at FL 250, Cessna … The engines were adapted from those used on the 401 and 402 models-the differences were intercoolers and provisions for bleed-air cabin pressurization. Equipped useful load: 2492 lb. Of course, any airplanes safety depends a great deal on the proficiency of its pilots. Also, I know more people who have lost an engine on a 421 than any other twin. 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. Equipped useful load: 1889 lb. 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. Props: McCauley 3-blade, 76.5-in. The 414 has the capacity for 1-2 crew members and up to 8 passengers. I have owned a 1979 C414AW (a 414A with RAM winglets) for five years and about 2400 flight hours. With GAMIjectors and lean-of-peak operation owners report a reduction of about 3 gph per engine at all power settings as well as cooler operating temperatures.Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. We typically have to stop for fuel every 2 hours when hauling an appreciable pax load. There are only two fuel-. : 1400 Fuel Type: … Read More "Cessna 340" We lost another Twin Cessna 414 (not A) today. 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. 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. Compared to its biggest competitors-the 421 and Duke-a 414 provides a more room than the Duke, as much as the 421, travels a little slower, but does so more economically.MAINTENANCE 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 1973 to 1977s are the long bodies. RAM also makes winglets and vortex generators. 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. Controls consisted of on/off/crossfeed valves and a fuel flow computer/indicator was added.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. View Cessna … "Never put your family in a cabin class Cessna unless you intend on buying one" A 340 is a bit small for my needs, the whole family is full size. The empty weight is 4365 lb (1980 kg) and the gross weight is 6750 lb (3062 kg). 414A - Two 230kW (310hp) TSIO-520-NBs. 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 nose baggage compartment of the 414A made CG juggling easier. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor. According to Cessna, 4.2-psi cabin pressure differential could be maintained by either engine operating at 60 percent power. Issued : 5/21/1999: SA00404WI : Installation of a starter engagement indication system. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. 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. A 414A RAM Series VII with Winglets (AW) will compete in many ways with a 421C. Once in service the airplanes became popular as workhorses for small charter and corporate flight departments, as well as comfortable transports for private owners.Today, prices range from around $160,000 to over $400,000 for typically-equipped 414s with mid-time engines. I have owned and flown a 1979 Cessna 414A for 14 months, accumulating 235 hours in all sorts of conditions. Mike Buschs Savvy Owners seminar is valuable. Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads. Production of the 414 ended in 1985 with almost … Horsepower: 310 Gross Weight: 6350 lbs Top Speed: 239 kts Empty Weight: 4039 lbs 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: 2350 ft Over 50 ft obstacle: 1865 ft Rate Of Climb: 1580 fpm Rate of Climb (One Engine): 240 fpm Ceiling: 30100 ft Ceiling (One Engine): 11350 ft At 21:04Z C-GTRK executed an overshoot. Best Cruise Speed: 224 KIAS. That way, “I … Cabin pressure: 4.2 psi. 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. The pressurized 414 was developed to appeal to owners of un-pressurised twin-engined aircraft and was based on the fuselage of the Cessna … To utilize the 414 to its potential, it needs to be flown high. Copyright © 2020 all-aero. 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. One of the most important came in 1973, when cabin length was increased 16 inches and a fifth side window was installed. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds.In the years following its introduction, the airplane saw few major changes. Horsepower: 2 x 310 HP. Certificated ceiling with oxygen equipment: 30,000 ft. Certificated ceiling without oxygen equipment: 25,000 ft. 8000ft cabin alt @: 21700 ft. 10,000ft cabin alt at: 26,500 ft. Dougherty is a pilot but not yet checked out on the 414. 1.3 Vso: 96 kt. It occurred as it approached John Wayne Airport. Our 414 holds 203 gallons of fuel, which I consider to be essential if you want to make long trips non … Insurance costs have equaled $7000 per year for the last couple of years for $1 million smooth with a hull value of $350,000. Fuel burn is the same, 34 GPH in cruise at all altitudes, with the RAM VII at 69 percent. If followed carefully, a mechanic wont miss anything. Controls consisted of on/off/crossfeed valves and a fuel flow computer/indicator was added. I travel for work and go off line for days at a time so please excuse me if I don't respond quickly to this thread). .td_uid_104_5fde785d95b38_rand.td-a-rec-img {
The gross weight and useful load of the new airplane both are substantially greater than those of the old 414, which gives it much better payload and endurance numbers and makes it a more viable corporate transport. 288 Of course, any airplanes safety depends a great deal on the proficiency of its pilots. Fuel burn: 35.8GPH @ 185-195K @ 16000 – 17000 Ft. The FSS noticed that the flight's left wing dipped unusually low at the time of the overshoot. The system left room for error, not only on the part of the pilot, but among line personnel. Reissued : 12/31/2002: SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. quantity indicators, both with three-position switches, to help the pilot keep track. 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. 1980 Cessna 414AEngines: RAM Overhauled TSIO-520-B, 335 hpTBO: 1600 hour Propellers: McCauley Series Saber Tip C500, Model 3AF32CC515, 3 Bladed Prop TBO: 2000Gross Ramp Weight: 7140 lbMax Gross Takeoff Weight: 7105 lbEmpty Weight: 5120.72 lbUseful Load: 1979.28 lbUseful load W/full main tanks (206USG): 743.28 lb Nose Baggage capacity: 332 lb Fuel burn: 35.8GPH @ 185-195K @ 16000 – 17000 Ft.Range with 206USG: 800 miles w/ 1 hr reserve.Seats: 7 / 8CIDC Turbo Star 414 / Cessna 414 Engines: 2 x Allison 250-B17B, 420 hp. The 340 carries less than the 414, but its faster on the same fuel burn. Beautiful, Low Time, Well-Maintained RAM VII Cessna 414A, 5030TTSN, 1636SRAM, 222STOH, Winglets, GARMIN 530/430 NAV/Com GPS, Dual Garmin Xdprs, 206 Gal. quantity indicators, both with three-position switches, to help the pilot keep track. Built by Cessna, the Cessna 414 is an American light, pressurized, twin-engine transport aircraft. SIDs are Cessna's means to address aging aircraft. A batch of World War II letters offers a glimpse of the high personal cost of flying bombers and fighters in their intended use. Seats: 6/8. Also, the big Cessnas have safety records that are unmatched by any other light twin. The 414 has the capacity for 1-2 crew members and … Each model has different after-market engine/prop conversions and when other performance-enhancing modifications are factored in, weights and other performance criteria vary. 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. Seats: 6/8. Major changes included a redesigned and increased-span wing incorporating integral fuel tanks and more baggage capacity in an extended nose. The 340, 340A, and 414 (non A) are basically the same operating cost per hour having basically the same systems and engines. Versions available between 1978 and 1986, were the standard Model 414A Chancellor, the Chancellor II and later the Chancellor III, all with differing factory installed avionic/equipment packages. It is the flying carpet my wife always wanted, including a potty! Wing loading: 29.9 lbs/sq.ft. The system left room for error, not only on the part of the pilot, but among line personnel. So, if its just pressurization youre looking for and youre going to be flying with only another person or two aboard, you might want to look at the 340 for a personal hot rod.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 Achilles heel of the airplane for me has been the cabin heater. Wing loading: 33.5 lb/sq.ft. It had a rate of 0.8 fatal accidents for each 100,000 … Best Range (i): 833 NM. 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. Standard empty weight: 4368 lbs. Call Listing Broker Scott MacDonald 772-781-5900 or … Issued : 5/21/1999: SA00404WI : Installation of a starter engagement indication system. margin: 0 auto 0 0;
The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks. After 513 of the original Model 414s had been built, Cessna combined the air-frame that was developed for the Golden Eagle in 1978 with the 310-hp engines of the 414 to produce the 414A Chancellor. (See page 25 for an abbreviated AD list.). 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. 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. We highly recommend them. 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