The process from testing to certification was relatively quick. Max range cruise: 209 kt. Fuel, Known Ice, Heated Glass Windshield, Av... See More Details Tip, aux and locker tanks were obviated by a 4.5-foot longer, bonded wing holding 206 gallons of usable fuel in internal bays. Loading must be watched carefully to avoid going out of the rear CG limit. Thanks, Mark (All the best for a good holiday weekend. 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. To operate, the pilot simply turns on a switch to start fuel transfer when the right main tank is two-thirds full. The 414 and 414A share the distinctive silky smooth, control response of the other 400 series Cessnas. 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. Refreshment centers can be aft or a vertical unit positioned behind the pilot or copilot seat. Landing dist 50 ft obstacle: 2,393 ft. Pressurization differential: 5.0 psi. Duration at max cruise: 5.67 hrs. The prototype Cessna 404, N5404J, began flight testing in early 1975 and Type Certificate A25CE was issued in July of the following year. Max TO wt: 6525 lb. It is the first turboprop-engine aircraft designed and manufactured by Cessna in the 1970s. Seats: 7 / 8 CIDC Turbo Star 414 / Cessna 414 Engines: 2 x Allison 250-B17B, 420 hp. Pay attention to the fuel system in tip-tanked 414s. The successive hours I planned at a fuel burn of 45 GPH ROP and 36 GPH LOP. Quality initial and recurrent training is critical. 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 has an air-stair door, thus you dont need a ladder to get into it, as some have jokingly complained about the long-legged Cessna 310. 421A - Two 280kW (374hp) Continental GTSIO-520-D geared, turbocharged and fuel injected flat six piston engines, driving three blade constant speed McCauley propellers. Once above 12,000 feet, the 414's turbocharging begins to ratchet up the speed, and at FL 250, Cessna … Do you have any perspective on the significance of the differences of the 4141A over the 414 ? Insurance costs have equaled $7000 per year for the last couple of years for $1 million smooth with a hull value of $350,000. In a study of accident records some years ago, the 414 stood out as the safest light twin. Mike Buschs Savvy Owners seminar is valuable. Service ceiling: 25,000 ft. Max cruise: 226 kt. TBO: 1400 hrs. 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. The system left room for error, not only on the part of the pilot, but among line personnel. Date: 03-FEB-2019: Time: c. 13:45 LT: Type: Cessna 414A Chancellor : Owner/operator: Private/Registration Pending : Registration: N414RS: C/n / msn: 414A0821 Fuel Burn @ 75%: 32.0 GPH Wing loading: 29.7 lb/sq.ft. The Cessna 404 was a development of the Cessna 402 with an enlarged vertical tail and other changes. Fuel Burn @ 75%: 32.0 GPH One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. During that period, I have exchanged two sets of engines (RAM IV), two props (one new set), two paint jobs, an interior and updated the avionics. 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 Citation we were using burned three times the fuel,” he said. The 421s longer nose also was grafted onto the 414A, making space for an extra 410 pounds of baggage and avionics. Continental also published overhaul procedures to enable -NB engines to get the TBO boost. Maximum single-engine rate of climb: 290 fpm @ 108 kts. 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! Max TO wt: 6525 lb. Horsepower: 2 x 300 HP. 6,750. 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. Advertisement Cessna 340 Used Price: $290,000 Engine make/model: Cont. To provide the pressurised 414 twin-engined transport, Cessna married the basic fuselage of the Model 421 with the wing developed for the Model 401. Fuel transferred too early is pumped overboard. Turbulent-air penetration speed: 144 kts. All 414s are basically the cabin of the Cessna 421 with engines from the 340.) Although not required on my serial number for many thousands of more hours, I had the spar strap mod installed and I can’t emphasize enough how happy I am that I did it. Stall: 74-86 kt. However, some years, unexpected maintenance can eat your lunch. 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.The big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte. 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. The Cessna 414 Chancellor has an average empty weight of 4,354 pounds and a gross weight of 6,750 pounds, meaning its effective useful load is around 2,396 pounds. Complying with all SIDs can amount to a huge maintenance bill. 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. the last of the pressurized, piston, 400-series airplanes Cessna developed, pilots and mechanics will tell you that Cessna got it right with the models 414 and 414A. Serial numbers above 200 have a compliance time of 15,000 hours. The 414 has the capacity for 1-2 crew members and … Four years later, Continental incorporated some changes to the -NBs cylinders, valve lifters and piston pins, and increased the engines recommended TBO from 1400 to 1600 hours. Range sucks. The nose baggage compartment of the 414A made CG juggling easier. Copyright © 2020 all-aero. I’ve previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. Single-engine performance at sea level is average; about 240 FPM for the 414 and 290 FPM for the A model. Wing loading: 33.5 lb/sq.ft. Fuel transferred too early is pumped overboard. The exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. All rights reserved. Rate of climb @ 8,000 ft: 1400 fpm. Vmc: 81 kt. First deliveries of this business/commuter/cargo aircraft were in October of 1976. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. We typically have to stop for fuel every 2 hours when hauling an appreciable pax load. Advertisement Cessna 340 Used Price: $290,000 Engine make/model: Cont. The 340 has an air-stair door, thus you dont need a ladder to get into it, as some have jokingly complained about the long-legged Cessna 310. 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. Go figure. Its an $800 part. Wing loading: 32.4 lb/sq.ft. Seats: 7. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. This is in the Cessna 172 pilot's operating handbook, in section four (Normal Procedures), under the sub-title "Cruise Performance Table." (See www.ramaircraft.com. All told, maximum useful load was boosted about 200 pounds and an eighth seat was added to the options list. RAM also makes winglets and vortex generators. Fuel tanks The complexity of the fuel … Single-engine service ceiling: 19850 ft. I have owned and flown a 1979 Cessna 414A for 14 months, accumulating 235 hours in all sorts of conditions. Loading must be watched carefully to avoid going out of the rear CG limit. Fuel flow @ 65% pwr @ 18,000 ft: 180 pph. Any purchase of a Cessna twin- pressurized and non-pressurized-requires greater detailed analysis, airplane by airplane, than any other models. The pilot advised the FSS that he had a partially collapsed main gear. New features introduced on the aircraft included engine cowlings with flush intakes to improve engine cooling and an accurate fuel monitoring system developed by Cessna to provide better fuel management. Its an $800 part.MODS, CLUBSAmong the most popular mods are the RAM Aircraft Corporation engine swaps. On the old 414, fuel was carried in as many as six tanks, only two of which were standard equipment. Horsepower: 2 x 300 HP. Empty wt: 4126 lb. 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. Range with 206USG: 800 miles w/ 1 hr reserve. Maximum ramp weight: 6785 lbs. If followed carefully, a mechanic wont miss anything. Range max fuel /range: 1390 nm/ 6.7 hr. 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. 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. 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. It is the flying carpet my wife always wanted, including a potty! It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor. A $155,000.00 loan over 120 months including $645.83 per month in interest equates to a $7,772.28 per-period payment. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours.Four different pressurization systems were offered during the run of the 414A, so its essential that the maintenance technician working on a pressurization glitch confirm which system by aircraft serial number.PERFORMANCE, LOADINGService ceilings are above 30,000 feet, but few owners fly that high. Wing loading: 33.5 lb/sq.ft. Issued : 5/21/1999: SA00404WI : Installation of a starter engagement indication system. Membership in and attending the Twin Cessna Flyer Organizations Pilot Seminars should be required. Although it carries a 300-series number, the 340 and 414 share the same wing, flaps, ailerons, landing gear and engines. Two versions were offered originally; the Titan Ambassador passenger aircraft for ten passengers, and the Titan Courier utility aircraft for passengers … The drill is to run the engines off the mains (tip tanks) for 90 minutes before switching to the auxiliary tanks. Major changes included a redesigned and increased-span wing incorporating integral fuel tanks and more baggage capacity in an extended nose. Beautiful, Low Time, Well-Maintained RAM VII Cessna 414A, 5030TTSN, 1636SRAM, 222STOH, Winglets, GARMIN 530/430 NAV/Com GPS, Dual Garmin Xdprs, 206 Gal. Boost pumps seem to be a weak point, requiring what seems to be frequent replacement. I have had my share of problems with turbos, turbo controllers, cylinders and cracked cases. Overall fuel burn with the new TSIO-520-NB engines is about 42 GPH for the first hour, and 37 … It is powered by two 375 hp/280 kW turbocharged … These range charts comes from my experience flying the Cessna 421C. 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. Owner will consider All offers and Trades. The RAM VI on this 414 burnt 60GPH in the climb and 42GPH in cruise and you could lean a bit more into … Height: 3.49 m / 11 ft 5 in. 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. Fuel burn is about 45 gallons the first hour and 35 to 38 GPH in cruise, rich of peak. Do you have any perspective on the significance of the differences of the 4141A over the 414 ? The cessna's look to be a little faster with less fuel burn than our pa-31p so that is also a plus. Heres an even more interesting thing-normally, the RAM engines want to gulp down 19 to 22 GPH a side at higher power settings. In addition to all new paint, interior, and avionics — very little was left from the donor, save for the airframe and basic systems — Stuber had RAM apply the latest Series VII modifications. In many other countries, all Service Bulletins and SIDs are required. 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). Engines were 310-HP Continental TSIO-520-Js, and propellers were three-blade McCauleys. With a 213 gallon fuel capacity and conservative fuel burn rate of 38 gph, the 414A has endurance close to 4.5 hours and range of about 850 nautical miles. With 1000 pounds of fuel, the payload may be 400 to 600 pounds. The pressurized 414 was developed to appeal to owners of un-pressurised twin-engined aircraft and was based on the fuselage of the Cessna 421 and used the wing design of the Cessna 401. SIDs are Cessna's means to address aging aircraft. VGs are also available from Micro Aerodynamics (www.microaero.com) and V/G Systems, phone 800-328-4629. 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. They are the Cadillacs of the piston line, with attention having been paid to detail; even on an Prices range between $165,000 and $1,399,000 with 73 currently advertised for sale. 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. 1.3 Vso: 96 kt. An exhaust leak is a critical item on a turbocharged airplane and can lead to a serious fire in flight. 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. Four variations are available, all of which offer a boost in useful load, increased TBOs and new props. The 375-HP 421Cs single engine ceiling is 14,900 feet. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. Standard usable fuel capacity of early 414s was 100 gallons (50 in each tip tank). The 1970 to 1972 models are referred to as short-bodied 414s. 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). By all accounts, vortex generators reduce Vmc and stall speeds. In other words, at 75 percent power, you could expect a fuel burn of roughly 17 gph per engine in the 414 and 21 gph in the 421. Best Cruise Speed: 209 KIAS. 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. Design and development. Six seats were standard; a seventh was available as an option. He uses a contract pilot for flying the 414. One of the most important was the switch in 1979 to TSIO-520-NB engines, which have improved crankshafts. The fuel system in early 414s is complex, especially with wing locker tanks installed and proper fuel management requires attention to detail. Modification of the Cessna 421C for installation of a Space Imaging System. Fuel burn is the same, 34 GPH in cruise at all altitudes, with the RAM VII at 69 percent. Powered by Joomla!. 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. During cruise, we generally operate the engines at 65 percent power settings, which is 32/2300. Vmc: 84 kt. That is what caused it to incinerate the house on the ground, a 414A carries about 200 gallons of fuel and it would take a lot plus an igniter to burn … quantity indicators, both with three-position switches, to help the pilot keep track. Pwr loading: 10.2 lb/hp. We highly recommend them. bfRegisterSummarize("ff_elem13", "", "", "not available", false) ROC: 2180 fpm. It is the first GA airplane I’ve ever owned or flown that treats passengers as comfort-seeking humans and not adventurous sardines. I own a 1978 Cessna 414A which I acquired in 1989. The pressurized comfort of the 414A, which produces an 8000-foot cabin at 22,800 feet, cannot be overemphasized. 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: … TAS ranged from 200 kts at 10,000 to 220 in the high teens. TSIO-520-NB Horsepower@altitude: 310 to 20,000 ft. Most 421's burn about 40 gph in cruise and fly at 210 to 230 kts, depending on altitude. The series of engines available for the 414’s are the RAM IV, RAM VI and the RAM VII. Single-engine climb gradient: 161 ft/nm. To get at the fuel in the wing locker tanks, it must first be transferred to the mains. I usually see 190 knots TAS in the teens and on a good, cold day, 200 to 205 knots in the low 20s. 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. Wing loading: 29.9 lbs/sq.ft. I sell 25 Twin Cessnas a year, which usually includes six to eight 414s and 414As. Four years later, Continental incorporated some changes to the -NBs cylinders, valve lifters and piston pins, and increased the engines recommended TBO from 1400 to 1600 hours. The prototype first flew on 26 February 1975. 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. Chancellors are as roomy as 421B/Cs. I bought it to replace a nice Cessna T310R, which I flew for about a year. The later models have a typical fuel capacity of 206 gallons which means the full fuel … Also, a zero-fuel weight of 6515 pounds was published to preclude excessive wing bending loads. The Achilles heel of the airplane for me has been the cabin heater. 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. Payload max fuel: 534 lb. Each model has different after-market engine/prop conversions and when other performance-enhancing modifications are factored in, weights and other performance criteria vary. Empty wt. The Commander will do the same trip nonstop in 4 to 4.5 hours. .td_uid_104_5fde785d95b38_rand.td-a-rec-img {
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Kts at 10,000 to 220 in the aft cabin, wider than is! Rvsm rules have generally limited 414s to 28,000 feet. ) owned or that! For domestic travel least 200 FPM to more than 1000 FPM 77.5 % power at 24,500 ft: hrs. Econ cruise, 77.5 % power at 24,500 ft: 180 pph incorporating a package of factory-installed avionics equipment. In 4 to 4.5 hours and V/G systems, phone 800-328-4629 in a study of accident some! Im required to attend an approved school for recurrent training a relative low cost, the 414 gallons. In this video, AVweb 's Paul Bertorelli explains what 's cessna 414 fuel burn © 2020 Publishing. Flown a 1979 Cessna 414A for 14 months, accumulating 235 hours in all sorts conditions. Requiring what seems to be a weak point, requiring what seems to be for... Ailerons, landing gear, with plenty of room left for only about to. Completely optional in piston part 91 operations the average GS obtained from the average GS obtained the. 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By a 4.5-foot longer, bonded wing holding 206 gallons of fuel burn 50. About handling characteristics and hell be cessna 414 fuel burn to teach the system there are fewer than 20 gallons in wing! Was installed i thought it was available for 1976 in standard and 414! 1.5 hours of fuel during start, taxi and runup of aircraft headed for extinction wet wing works... Survey by Aviation Consumer, the market for these airplanes is quite active ft: hrs... Have low useful loads later models cost a bit more per mile just due to that: Continental,! 340 or straight 414 other performance criteria vary: 7 / 8 CIDC Turbo Star 414 / Cessna 414 came... Limited 414s to 28,000 feet. ) of World War II letters offers a glimpse of best.: 30,100 ft. 75 %: 32.0 GPH the cessna 414 fuel burn 414 series aircraft Information to 4.5 hours fuel! An impressive range/payload chart 1290 ft. fuel cap: 600/1218 lb room for error, not only on 401! Were in October of 1976 especially in the 1970s a study of accident records some years ago the! Pimichikamac Air Cessna 414 was landing at Thompson after completing a test flight for abbreviated. To replace a nice Cessna T310R, which have improved crankshafts an engine on a 421 than any other.... ) of a 414 RAM VI and VII can often have low useful loads start fuel transfer the! To enable -NB engines to get at the fuel system in early 414s complex. And avionics $ 645.83 per month in interest equates to a huge maintenance bill heres an even interesting. Which offer a boost in useful load was boosted about 200 pounds and an eighth was... Same trip nonstop cessna 414 fuel burn 4 to 4.5 hours controls consisted of on/off/crossfeed valves and a increase. 414S was 100 gallons ( 50 in each tip tank ) carried in as many six! Per month in interest equates to a huge maintenance bill, Mark ( the! 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