cessna 414 fuel burn

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. (RVSM rules have generally limited 414s to 28,000 feet.) The 441 Conquest II was purposely produced to fill the gap between Cessna’s jet and piston engine aircraft. Electronic prop synchrophasers became standard equipment in 1976, when two versions of the airplane were put on the market: a bare-bones 414 and a 414II, which came with an assortment of ARC 400-series avionics equipment.That year, most limiting and recommended airspeeds were boosted a few knots (except Vmc, which was lowered from 84 to 82 knots), and the -J engines were replaced with TSIO-520-Ns. Contribute / share information, experience and/or images, The fields marked with * are required to be entered. Issued : 2/8/1996: SA00419NY : Installation of cockpit utility light. The exhaust system AD must be followed carefully, including the 30-day checks whether the airplane flies or not. It's a gyroplane, not a gyrocopter and it's nothing at all like a helicopter. 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. Admittedly, the 414As wet-wing fuel system is an improvement and is simplified. TSIO-520-NB Horsepower@altitude: 310 to 20,000 ft. An AD issued in 1986 requires cylinders to be pressure-checked for leaks every 50 hours until the engine has amassed 500 hours. What a difference! Payload max fuel: 671 lb. Engines two 310-hp turbocharged Continentals. Stall: 74-86 kt. 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. The system left room for error, not only on the part of the pilot, but among line personnel. Once again, SIDs are completely optional in piston Part 91 operations. Stall: 70-85 kt. (See page 25 for an abbreviated AD list.). ROC: 2180 fpm. The exhaust system sees a great deal of heat and vibration, thus components wear out. 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. 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. bfRegisterSummarize("ff_elem13", "", "", "not available", false) (As of this writing there is an alternative method of compliance published by the FAA in CE-05-35.) Endurance at 65% pwr @ 18,000 ft: 6.5 hrs: Econ cruise, 60.8% power at 20,000 ft: 187 kts. The series of engines available for the 414’s are the RAM IV, RAM VI and the RAM VII. TBO: 1400 hrs. 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. Another point of consideration for a 414 buyer is the SB/AD on the wing spar. Fuel, Known Ice, Heated Glass Windshield, Av... See More Details Maximum landing weight: 6750 lbs. 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. View Cessna … The pressure differential - five pounds per square inch - is greater so that the airplane can cruise at higher altitudes. The 414 usually has a different cabin layout, so i thought it was different/smaller. All 414s are basically the cabin of the Cessna 421 with engines from the 340.) 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). He uses a contract pilot for flying the 414. 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. A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. 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. 2. They said that the Cessna inspection procedure manual for the airplane is one of the best such manuals written. That way, “I … 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. I have had my share of problems with turbos, turbo controllers, cylinders and cracked cases. Issued : 2/8/1996: SA00419NY : Installation of cockpit utility light. 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. First deliveries of this business/commuter/cargo aircraft were in October of 1976. Empty wt: 4126 lb. The 414 has the capacity for 1-2 crew members and … Do you have any perspective on the significance of the differences of the 4141A over the 414 ? The exhaust system sees a great deal of heat and vibration, thus components wear out. googletag.cmd.push(function() { googletag.display('inline'); }); Initial climbout increased by at least 200 FPM to more than 1000 FPM. Prices range between $165,000 and $1,399,000 with 73 currently advertised for sale. Wing loading: 29.7 lb/sq.ft. WORLD'S PREMIER INDEPENDENT AVIATION NEWS RESOURCE. 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. Some potties have a flushing feature. SE ceiling: 11,350 ft. Min field length: 2350 ft. Fuel cap: 600/1218 lb. In the years following its introduction, the airplane saw few major changes. 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. Powered by Joomla!. Cessna 414 Series Aircraft Information. Most prefer the upper teens and lower 20s, where they get about 190 knots on 32 to 34 GPH at 65 percent power. 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. This can be a great aircraft and a good buy, but only for a pilot who doesnt need lots of payload. Reissued : 12/31/2002: SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Insurance costs have equaled $7000 per year for the last couple of years for $1 million smooth with a hull value of $350,000. Also worth joining is the Cessna Pilots Association (www.cessna.org and 805-934-0493). 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. It had basically the same tail and “wide-oval” fuselage as the 421B, and the 401s wing. Range max fuel / 55%: 1309nm/7.2hr. (The A models have the much- improved, 206-gallon wet-wing fuel system. Maximum takeoff weight was 6350 pounds; max landing, 6200 pounds. /* custom css */ Based on 450 annual owner-operated hours and $5.00-per-gallon fuel cost, the CESSNA 421C has total variable costs of $251,550.00, total fixed … 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. I planned for 55 Gallons of fuel burn the first hour (both ROP&LOP). 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. It was available for 1976 in standard and Model 414 II versions, the latter incorporating a package of factory-installed avionics and equipment. 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. I’ve previously owned and flown a Seneca and a Mooney, both of which were equipped with weather radar, full deice and Stormscope. Fuel burn: 35.8GPH @ 185-195K @ 16000 – 17000 Ft. Date: 03-FEB-2019: Time: c. 13:45 LT: Type: Cessna 414A Chancellor : Owner/operator: Private/Registration Pending : Registration: N414RS: C/n / msn: 414A0821 Most 421's burn about 40 gph in cruise and fly at 210 to 230 kts, depending on altitude. 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. Copyright © 2020 all-aero. 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. 414A v 414 Also, my mechanic suggested the 414A over the 414. (RVSM rules have generally limited 414s to 28,000 feet.) The hydraulic landing gear, with its high gear speed is a great by-product of the wet wing. The big cabin, wider than it is tall, makes for comfortable seating and copious baggage space is the 414s forte. Owner-pilots give high marks to cockpit room and layout of systems controls and enthuse about handling characteristics. By all accounts, vortex generators reduce Vmc and stall speeds. Single-engine climb gradient: 161 ft/nm. Specs, range, speed, operating weights and performance for the Cessna 414A RAM here We use cookies to help you get the best experience when using our website. The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. A simpler fuel system was among a host of improvements unveiled in 1978 with introduction of the Model 414A Chancellor. 288 With a range of approximately 2,200 nautical miles and a relative low cost, the Conquest II was an unparalleled aircraft in its time. When Model 414/414A production ended in 1986 a total of 1,067 variants had been built.The old 414's service ceiling was 11,350 feet, and with the same engines and gross weight 400 pounds greater, the new airplane does 19,850 feet. 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. Modification of the Cessna 421C for installation of a Space Imaging System. The nose baggage compartment of the 414A made CG juggling easier. As has often been said, Cessna really got it right with the 414/414As. The winglet mod works; I typically get 215 to 218 knots at mid-weight at FL220, running 72 percent power. 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. Pwr loading: 7.7 lb/hp. Thanks, Mark (All the best for a good holiday weekend. Seats: 6/8. Although it carries a 300-series number, the 340 and 414 share the same wing, flaps, ailerons, landing gear and engines.

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