The Continental IO-550 does about 0.39 lb/hp∙hr (237 g/kW∙h) when running LOP, and an angle-valve Lycoming IO-360 does about .41 (249 g/kW∙h). capacity marked on the fuel cap) is good for 4 hours plus reserve. I don't think the Lycoming fuel injection works on the same principle so there is no return line and no tank needed. Brake Specific Fuel Consumption. Range w/ 45 min. The Hawk XP was capable of a 131-knot (243 km/h) cruise speed. No airplane has ever fallen out of the sky because of high oil consumption—unless the oil consumption was so high that the engine ran out of oil before it ran out of fuel (which FIGURE 1-1. Continental’s IO-360-AF alternative fuel engine September 27, 2011 by Kent Misegades At last week’s AOPA Aviation Summit , Continental Motors impressed many with the announcement of its IO-360-AF engine, an 180-hp powerplant that is a lower-compression ratio version of the company’s IO-360 … The IO-360-AF engine family offers a maximum power output of 195 horsepower at 2800 RPM, a 2,200 hour Time Between Overhaul (TBO) and is backed by Continental… I have flown both and while there is a big performance gain going to the O-360, there is that much more going to the IO-360. 5. THREE-QUARTER RIGHT FRONT VIEW OF THE IO-520-A,E,F & K. (SANDCAST CASE) FIGURE 1-2. I got a Chart in my plane that shows fuel burn at different settings for the Avcon Conversion. 7. Lackof sufficient fuel flow Disconnect fuel line and check fuel flow. The Continental IO-360's fuel injection pumps more fuel than is needed to hold pressure with the excess fuel returned to the fuel tanks (via a small header tank). The Continental IO-360 is a family of fuel-injected air-cooled, six-cylinder aircraft engines manufactured by Continental Motors in the United States of America, and first run in 1962. Any fuel system that cannot be adjusted to meet the specified values will require repair or replacement of the affected components prior to further engine operation. The adjustment procedures provided in this document also apply to engine fuel systems equipped with Continental Motors (CM) Position Tuned Fuel Nozzles. model # cyl rated power1 bore × stroke displacement dry weight2 certified fuel grade comp. O-360 & IO-360 SERIES ENGINES INSTALLATION & OPERATION MANUAL 621 South Royal Lane, Suite 100 / Coppell, TX 75019 / 800-277-5168 P/N SVIOM01 Revision B, February, 2007 FAA Approved In the last segment, we reviewed the basic design and operation of the Continental continuous-flow fuel injection system.Now let’s take some time to review proper preventive maintenance of these rarely maintained systems. You'll have significantly better takeoff/climb but not as much gain in cruise speed. A compression check shows high compressions with the exception of #6, which has gone from 75/80 to 60… The specific data used was from: Figure 3.1. Stroke remained at 3.6250", and the compression ratio remained at the same 6.3:1 value that had been used in A-65s and A75s, allowing the use of 73 octane fuel. Authorized Full Service Master Lycoming Distributor. Continental says maximum permissible oil consumption for this 310-hp engine is about 1 quart per hour (and Ted’s oil consumption wasn’t anywhere close). Fuel consumption stated in pounds per hour per brake horsepower. : 2000 Fuel type: 100/100LL Propeller type/diameter: Hartzell CS … Read More "Cirrus SR20" New, rebuilt, overhauled Lycoming IO-360 engines for sale. disp. (You may want to consider adding aux fuel tanks. The enginewas available in both normally aspirated, fuel injected IO-360 model and a turbocharged TSIO-360 versions. IO-360-ES4, 185 hp Fuel type: 100/100LL Propeller type: FP Landing gear type: Tri/Fixed Gross weight: 2280 lb Landing weight: 2280 lb Empty weight, std: 1450 lb Useful load, std: 830 lb Payload - full std. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 (866) tell-FAA ((866) 835-5322) (L)IO-360-M1A DESCRIPTION 3 SECTION I PART 1 DESCRIPTION The Lycoming (L)IO-360-M1A is a fuel injected, direct-drive, four-cylinder, horizontally opposed, and air-cooled with a down exhaust. But some things to keep in mind is: 1. 1-10. X30631A. I cruise my Swift at 24″ x 2600 if I’m in a hurry. Horsepower is always welcome! The “lower end” of these engines is near “bullet proof” and is almost identical to the 210 hp IO-360. Swift actually holds, despite the 26 gal. I flew pretty clos… Lycoming produces a complete line of four-, six-, and eight-cylinder piston engines boasting up to 400 horsepower. X40000. TCM Ignition Systems Master Service Manual, Form No. ratio time between overhaul (tbo) faa tcds io-520-a 6 213 kw @ 2700 133.35 × 101.6 mm 8514 cm3 208.9 kg 100/100ll 8.5:1 1900 hours or 12 years e5ce 1-11. The fuel injection system of aircraft reciprocating engine has many advantages over a conventional carburetor system. I flew down to St George last week so I thought I would check it out. This engine is supplied with a starter. O-360 & IO-360 SERIES ENGINES MAINTENANCE MANUAL 621 South Royal Lane, Suite 100 / Coppell, TX 75019 / 800-277-5168 ... 73-00-00.1 Engine Fuel Pump Assembly 73 00 00 2 74-00-00.1 Magneto Components 74 00 00 3 ... 72-00-01.9 Excessive Oil Consumption 4 High oil consumption can be one of the curses of delivery flying, especially if you have a 15-hour leg to fly, an eight-quart capacity and a burn rate that can reach one quart every two hours. Default Title - $209.95 Microlon Engine Treatment Kit - Continental Aircraft [IO-360 Engine] fuel: 590 lb Useable fuel, std: 40 USgal Height: 8 ft. 10 in. With a reputation for meeting or exceeding TBO, it is no secret that Lycoming Engines are the power of choice for general aviation aircraft. Continental IO-360-KB : normally aspirated, direct drive, air cooled, horizontally opposed, fuel injected, six cylinder engine w/ 360 Engine: Continental. If found, complete overhaul of the engine may be indicated. 3. Lately, we've been experiencing some pretty high oil consumption with quite a bit of oil on the belly. Around 1943, Continental began work on an engine series based on a new cylinder with a 4.0625" bore, an increase of 0.1875" from the 3.875" bore used in A-series engines. 6-1 Alternator Maintenance and Parts Catalog, Form No. 60297-12).. Drain fuel injector or carburetor and fuel lines. O-360 and IO-360 Series Engines O-360 & IO-360 SERIES ENGINES INSTALLATION & OPERATION MANUAL 621 South Royal Lane, Suite 100 / Coppell, TX 75019 / 800-277-5168 P/N SVIOM01 Revision D, June 2014 I like the Lycoming 0-360 too but I feel the Continental IO-360 is a better match for this plane. During ring seating, the basic purpose is to establish metal-to-metal contact between the piston ring face and the cylinder barrel. reserve: 500 NM: Endurance @ 75% power @ 8,000ft. The IO-360 is a very expensive and time consuming conversion but you will never regret the performance. Specific fuel consumption is virtually identical between the Rotax and the Continental, but the IO-240 delivers more power which comes at the price of higher fuel burn. Fuel and oil aren’t cheap, but be generous with both during the first 25 hours after a major overhaul, a top or even after reworking one or two cylinders. In economy cruise, the Continental’s burn is comparable to the Rotax but trainers aren’t often operated in economy cruise. GAL. Fuel Injection Manual, Form 30593A. Engine Break-In Teledyne Continental Motors, Inc. TM 1 ... chamber and to keep combustion gas blow-by and oil consumption to a minimum. Title: 60297-12-360series Ops Man.pdf Author: Owner Created Date: 3/16/2010 3:19:38 PM What pressure can one expect to read on the instrument panel using the original fuel pressure gauge( as per the C125 installation, in psi) connected at the outlet of the fuel divider unit, where the fuel consumption gauge in gph would normally be connected on the IO-360 Continental motor. Water in fuel injector or carb. Fuel injection systems vary in their details of construction, arrangement, and operation. From 1977 to 1981 Cessna produced the R172K Hawk XP, a model available from both Wichita and Reims. For example, an engine developing 300 horsepower while burning 150 pounds of fuel per hour, has a BSFC of -5. Overall length: 24 ft. Wingspan: 38 ft. 6 in. 2. You'll have less endurance due to increased fuel conumption. If you live in a highly populated part of the world, the thought of survival equipment for your aircraft only comes up if you are reading about or thinking about taking a significantly adventurous trip—say, across the oceans or to a less-populated part of the world. This configuration featured a fuel injected, Continental IO-360K (later IO-360KB) derated to 195 hp (145 kW) with a two-bladed, constant-speed propeller. If I were to want more, the TCM IO-360 is what I'd do also. Fuel Capacity (Usable) 49 US. The data used in construction the models was extracted from the Operator’s Manual, Textron Lycoming O-360, IO-360, AIO-360, HIO-360 & TIO-360, 5th Edition (Part No. Fuel Injected Models / Use sparingly on male threads only Apply in accordance with Figure 8 Exhaust studs All Models (nut end before torquing) All mechanical tach drive housing threads not through to an oil source At engine assembly Plug Vernatherm All .3125 and larger studs unless otherwise noted Oil sump return fitting IO-360-ES3B & IO-360-HB9B At 9,000 ft, 17.4 MP & 2400 RPM it shows 7.4 gal/hr fuel burn. Advertisement Cirrus SR20 Price: $188,300 Engine make/model: Continental IO-360-ES Horsepower@rpm@takeoff: 200@2700@SL Horsepower for takeoff: 200 TBO hrs. Representative Effect of Fuel/Air Ratio on Cylinder Head Temperature, Power and Specific Fuel Consumption at Constant RPM and Manifold Pressure in Cruise Range Operation The above publications can be ordered through your Teledyne Continental Motors Distributor or ordered directly, if prepaid, from: Mounting pad drives for two AN-type accessories and a … 8. Starter Service Instructions, Form X30592. The most efficient piston engines are the huge diesels that power modern ships—the best ones produce over 100,000 hp with a BSFC of about 0.26 lb/hp∙hr (158 g/kW∙h). Industry’s best service and prices. 6. Internal failure Checkoil screens for metal particles. OIL CONSUMPTION. Q: We have a 1981 Cessna 182 with the Lycoming O540 L3C5D engine, which has the Cessna-installed turbo system. When operated on a rigid test stand at cruise power settings and operating within specified limits oil consumption shall not exceed 1 quart per hour and one –half.

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