Speed has always been a strong 310 selling point, for good reason. As the maximum weights increased, the single-engine climb rate decreased; the T310R, at its 5,500-pound maximum, is supposed to ascend at 390 fpm at sea level with one feathered. Cessna C310 aircraft specifications history and performance. Windows were added and lengthened through the 310's gestation as well. This airplane is certificated in the normal category. Please send us your experiences on your aircraft. Wing locker tanks, each with 20 gallons total capacity, became options with the 1967 models. ( Share your invaluable experience. 1959 Cessna 310-C For Sale. Many early 310s suffer substantial corrosion at the aft spar and wing skins, and such trouble unnoticed during the prepurchase inspection can leave the new 310 owner feeling a bit blue. Get the latest news on coronavirus impacts on general aviation, including what AOPA is doing to protect GA, event cancellations, advice for pilots to protect themselves, and more. You are disciplined and relentless in chasing after big dreams. A 310 Cessna twin-engine airplane is having a landing gear problem and is circling the Bert-Mooney Airport in Butte in an attempt to burn off fuel before making an emergency landing. Single-engine service ceiling is about 7000 to 7500 feet, or 17,000-18,000 for the turbo. Two main traps await the unwary 310 driver. In general terms, the 310's a sweetheart, a veritable immovable object on instruments and a good, if somewhat stiff, rider in turbulence. If you have a hankering for old and complex airplanes, the 310 might well fit the bill, so long as you know that the initial maintenance bills can be thrilling. They are fast, carry large loads and have excellent range. ... Find and Compare CESSNA 310 for sale Also Consider. Other variations on the 310 theme will tip you off to the airplane's age. ( The 310J seats up to 5 passengers plus 1 pilot. Airplanes such as Mike Busch’s magnificently restored T310R will obviously demand a premium price, but that’s perhaps only appropriate for Cessna’s piston-powered Learjet with props. It is their shape … Marc E. Cook, AOPA Pilot, May 1994. Cessna's landmark twin also begat a larger turbocharged model, the 320, in 1963, and provided the basis for the pressurized 340. Single-engine service ceiling went up with the turbo models, to 17,200 feet in the T310R; a 310B could hold 7,700 feet on one engine. My rule of thumbhere is to increase the cost figure by 25% for each 10 years since the airplane wasmanufactured. ). Thanks to the long life of the airplane and the many changes made to it, an almost bewildering array of choices exist for the 310 buyer. In the spring of 1954, Cessna received a Type Certificate for the 310, launching a production run that lasted until 1981 of general aviation’s most desired light twin-engine airplane. Specs, range, speed, operating weights and performance for the Cessna 310R here TSIO-520-NB Horsepower@altitude: 310 to 20,000 ft. A Cessna 310, with its 28 gallon per hour fuel burn, should cost$112 per hour to operate. Stall Speed: 65 KIAS . Several variants of the IO-470 were used through the 1975 model year in the 310Q. Horsepower: 260 Gross Weight: 5100 lbs Top Speed: 209 kts Empty Weight: 3063 lbs Cruise Speed: 194 kts Fuel Capacity: 102 gal Stall Speed (dirty): 65 kts Range: 687 nm Takeoff: Landing: Ground Roll: 1920 ft Ground Roll 690 ft: Over 50 ft obstacle: 1545 ft Over 50 ft obstacle: 1900 ft Rate Of Climb: 1690 fpm Rate of Climb (One Engine): 380 fpm Ceiling: 21100 ft Ceiling (One Engine): 7450 ft The Cessna 310 was a common charter aircraft for the many air taxi firms that sprang up in the general aviation boom that followed World War II. Flying the Cessna 310 is, on the other hand, a pleasure. It goes faster, climbs faster and gives the owner a bit of brag-ging rights on the ramp. Please login below for an enhanced experience. Another significant change came with the 1964 I model: The overwing augmenter tubes gave way to conventional exhaust plumbing. Although it carries a 300-series number, the 340 and 414 share the same wing, flaps, ailerons, landing gear and engines. Wilmington, DE. Fuel Burn 14.8 GPH of Jet A at 75% power Cruise Speed 187 knots at 75% power Cruise: 198 knots (14,000 feet @95% power, 17 gph) Fuel Consumption @60% power: 11.8 gph Useful Load with full fuel: 1021 lbs (this includes full auxiliary tanks!) The engines are Continental Model IO-520-Ms and are rated at 285 horsepower each. One of the earmarks of the line's changes concerns horsepower. Operators say the T310s work best in the high teens. Fuel Burn @ 75%: 25.0 GPH. Notes on Maintenance You could say that it has substantial roll inertia. And although the system worked, exhaust gases, being quite corrosive, wreaked havoc on the wing structure. Rate of climb: 1,590 FPM. 91 or F.A.R 135. Starting with pressure-carbureted 240-hp O-470 Continentals, the 310 gained real fuel injection and an additional 20 hp per side with the C model, in 1959. Experienced 310 pilots say that minimizing aileron inputs is the only way to prevent the 310 from rocking around the pattern like a rowboat in high seas. Already a member? This instant recognition was the case in the 1950s and it's still the case today. ( Fortunately, aside from the gear troubles noted earlier, there doesn't seem to be any one recurring trouble spot with the 310s. Horsepower for takeoff: 310 TBO hrs. ), in the end you have to burn fuel … Best Cruise Speed: 193 KIAS . (Go faster at a lower climb rate, or slower at a higher climb rate, depending on trip profile, etc. A fuel flow gauge, fuel quantity gauge, and a fuel low level warning light are located in the cockpit. wing tip tanks and two 15 gallon (56.8 L). Rate of climb: 1540 FPM . When a Cessna 310 taxis onto an FBO ramp, virtually everyone watching knows what it is and what company made it. Maladies include broken or cracked mounts, support structures, actuator rods, door hinges and actuators, shock struts, and bellcranks. Cessna entered the light-twin market a clear overdog in late 1954. General opinion of the IO-470 has always been good, and it seems the model has performed quite well in the 310. If you can comfortably handle a 310, the transition to a 400 series Cessna, including a Conquest I or II (425 or 441) will be a virtual nonevent. With the 240-hp engines, the 310 will turn in cruise speeds of 183 knots (70-percent power at 7,500 feet, burning 25 gallons per hour total) and climb with both engines at better than 1,600 fpm from sea level. Spins and aerobatic maneuvers are not permitted in normal category airplanes. 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 … Gross Weight: 5200 LBS . Now we need to connect them with products and services. You may have to leave some fuel behind. Naturally, the turbocharged 310s are the quickest, showing 198 knots at 10,000 feet (on 74 percent and 31 gph) and 220 knots at 20,000 feet with the same settings. We also sat down with a warm stack of service difficulty reports and discovered that the 310's gear system is, quite literally, its Achilles' heel. According to owners and mechanics, the 470s live a long and happy life under 310 cowls, and the number of service difficulty reports slated for the 470-powered airplanes is proportionally lower than for the IO-520 and TSIO-520 versions. Designed to shear off in the event of a crash, the tips were the only tanks until the 1958 B model. Fuel capacity 102-207. This topic is now archived and is closed to further replies. - Send us pictures of your plane. Second, is the locker-tank scheme. PERFORMANCE: Top mph 238. Turbo owners report fuel burns of 27 GPH LOP and 33 GPH ROP. We have the aviators. A nice flight from FMY to SPG for breakfast. The necessary fuel for the craft and its contents will further increase the weight, and therefore the fuel burn. As Cessna did to virtually all its models in the late 1950s and early 1960s, the 310 received a swept vertical fin in place of the upright tail used through the 1959 model. Three-ten shoppers (and pilots) would do well to sit down with a jug of coffee and a good reading lamp and bone up on this airplane's fuel system. CESSNA FLYER (32) JULY 2019 CESSNA FLYER (33) JULY 2019 eople look at upgrading their Cessna 172 Skyhawk engine for a number of reasons, and there’s a great deal of validity for them all. Cessna C310 aircraft specifications history and performance. Potential business lines include aviation data services (to consumers or manufacturers), aircraft brokerage, financing and insurance, marketing and advertising, and targeted sales of products ranging from avionics to t-shirts, and services ranging from overhauls to flight instruction. The main tanks are integrally sealed aluminum tanks mounted on each wing tip and each contain an auxiliary fuel pump and transfer pump. Compensation is based purely on revenue built, but with significant equity. The Cessna 310 has fuel tanks shaped like a fish at the tip of its wings. Aircraft Owners & Pilots Association Find it free on the store. : 1400 Fuel Type: … Read More "Cessna 340" Check all 4 fuel gauges for full tank, if appropriate. The Cessna 310 first flew in January 1953. ) What needs to be done? Become an Ambassador and broaden the awareness of your wonderful airplane! Both are strong points of the Cessna 310, especially the turbocharged versions. Then Cessna installed auxiliary tanks in the wings, good for an extra 40 total gallons. Pitch response is heaviest, roll the lightest, with generally good stick force per G and longitudinal stability. This means that using fuel from either the auxiliary tank on the same side, or the main tank on the opposite side, about half the fuel flow will be moving to the same-side main. By GUY R. MAHER. 1959 was the last year of the straight-tail but the first year of the Fuel-injected engines with the increase to 260 HP, yielding in my opinion the best looking and probably the fastest normally-aspirated 310 out there (since they went up in weight from there). It’s not that much more expensive than a rebuild for TBO. Early 310s could manage 415 feet per minute on one engine at maximum gross weight (4,700 pounds in the 310B). A long-range airplane has six tanks and 10 fuel pumps. Out of 225 SDRs (for about 150 different airplanes), we counted more than 40 regarding the gear alone. Fuel Burn at 75% power in standard conditions per hour. The fuel system consists of two main tanks, two optional auxiliary tanks, two optional wing locker tanks, fuel selectors for selection of main, auxiliary or crossfeed and other necessary components to complete the system. 5,500. Remember, also, that the cost of maintaining an airplane like the 310 is keyed more to its health and the price of parts than the purchase price. At the other extreme of the line, the last models of the 310 can be counted on to perform transportation duties with the capability of newer models, and the prices reflect this ability. Yes, we're talking tuna tanks, those slightly clunky vessels at the ends of the wings, slated to hold 50 gallons of fuel each. Confused? At the other extreme of the line, the last models of the 310 can be counted on to perform transportation duties with the capability of newer models, and the prices reflect this ability. 0 The airplane is approved for day and night VFR/IFR operations when equipped in accordance with F.A.R. Fuelburn: 25.0 GPH Reduced power settings get 175 k… The optional wing locker fuel tanks are located in the forward portion of each wing locker baggage area. The normally aspirated models are happiest in the low teens, while the turbos have service ceilings in the mid-20s. Advertisement STANDARD DATA: (310R) Seats 4-6. And the 310 needed help in this department, what with 300 pounds of avgas way out there on the wing. (Such nicknames come from the tank's fish-like profile.) Early models feature high-speed cruise in the neighborhood of 175 knots while later ones will top out at around 190. We have worked for six years to create 700,000 aircraft homepages that contain detailed aircraft information (think Zillow) giving us the opportunity to bring together consumers with the aviation products and services they need most in a way never before possible. More than half of the reports target the main gear. Wait until you have to manage the tanks. Twin engine piston aircraft with retractable landing gear. In summary, 310 owners who run LOP burn about 15% less fuel per hour than those running ROP. Through its 28-year production span, the 310 evolved from a five-seater with pressure-carbureted engines to a high- flying turbocharged six-placer with known-icing certification. More weight in later models about makes up for the extra power: A 260-hp-a-side Q model turns in 186 knots (71 percent at 7,500 feet, on 26.5 gph) and climbs at 1,495 fpm; not bad considering the Q's 600-pound higher maximum gross weight. According to owners and 310 support groups, parts are readily available for the airplane, although, as is true with any model these days, the costs can be dear. The bigger Continental came aboard in the 1975 model, the R. It's interesting to note that through the life of the 310, engine power was increased only 45 hp a side. We have a reporter at the scene and will update this story as more information becomes available. 0.0 ©2020 Aircraft Owners and Pilots Association, Available with 102/143/166/184/207 gallon systems, Avg. So if you have a right-side locker, you will have to draw down the right main by at least 20 gallons to make room for the locker fuel and then crossfeed the left engine to minimize lateral imbalance from those extra 120 pounds now out on the right wing tip. Maximum boost for a sea-level takeoff is a moderate 32 inches. The airplane is powered by two horizontally opposed, six cylinder, direct drive, normally aspirated, air cooled, fuel injected engines. You have deep industry relationships or the personality that naturally builds them. These tanks are bladder-type cells which supplement the main tank fuel quantity. For one thing, the all-electric gear is not particularly quick to stow. In the single-engine category, the 310 also performs reasonably well, however few light twins are truly spectacular with one engine inoperative. As for those moving up through the Cessna line, a 210 pilot will most definitely notice the 310's heavier controls, higher wing loading, and greater approach and landing speeds. Fuel Burn @ 75%: 25.5 GPH . Gross wt. Together, this means that 310s came with total capacities of 100, 140, 163, 183, or 203 gallons. Cessna C340A Fuel System and procedures Archived. This lesson ought to be clear: Carefully and thoroughly inspect the gear system on any 310 considered for purchase. Who are you? Our mission is to empower the end-users, the aircraft owners and pilots. Where some versions of the TSIO-520 have been pushed to 325 hp, the 310's engines are practically loafing at 285 hp. Most airplanes have just one of these, and its contents cannot be consumed directly by the engines. aux tanks, giving you a possible range of 1000 miles. 3,358. Fuel cost per hour: Best Range: 687 NM The 310 is an all metal, four/six-place, low wing, twin engine airplane and is equipped with retractable tricycle landing gear. Also, consider it a bonus if the airplane is fitted with retrofit Cleveland brakes; the original Goodyears are known to be somewhat troublesome and expensive to maintain. The Cessna 310 remains one of the top non-cabin class twins you can buy, and usually for less than $150,000. ( gallons/hr @ /gal), Misc: landing, parking, supplies,catering, etc, Best Cruise: 194 KIAS Horsepower: 260 Gross Weight: 5300 lbs Top Speed: 205 kts Empty Weight: 3214 lbs Cruise Speed: 192 kts Fuel Capacity: 102.00 gal Stall Speed (dirty): 63 kts Range: 680 nm Takeoff Max Useful Load: 1609 lbs Range: 1285 nm Instead, locker fuel must be pumped to the corresponding main tank. Another tip from the 310 experts: To offset the nose-up pitching moment upon deploying the split flaps, select gear-down simultaneously. 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Model - Applied, considering the overall age of the locker tanks Association Find it free on the from! The line relatively painless for pilots, some reports will state fuel burn is not normal in low... And speed taken into account the IO-470 has always been a strong selling. Systems of the IO-470 were Used through the 1975 model year in the outboard wing,! - Applied augmenter tubes gave way to conventional exhaust plumbing: - Features that would be Useful you! Aircraft Values and total Ownership Costs flaps, select gear-down simultaneously transfer pump 112. DATA that you believe inaccurate! % power in standard conditions per hour: 204 lbs at maximum gross weight ( 4,700 in! 415 feet per minute on one engine inoperative report an average fuel burn drops off Useful Load 1609...

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