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TROUBLE-FREE STARTING AND OPERATION OF LYCOMING ENGINES IN LOW TEMPERATURES
Let’s start with the overall condition of the engine.
When attempting to start an engine in adverse conditions, it is essential that the engine is well-maintained and in perfect working order.
The spark plug gaps and magnetos should be properly set and ready to operate efficiently. In addition to the ignition system, other systems can also affect the proper operation of the engine.
Regular maintenance should include checking the heating system for leaks. It is worth taking this opportunity to remind you that you cannot smell carbon monoxide in the cabin!
In cold weather, another factor to consider before starting the engine is preheating.
The Lycoming service manuals provide specific guidelines as to when preheating should be used, but the timing or method of preheating is generally left to the good judgment of the pilot or the person performing the preheating.
Lycoming does not recommend the use of a heated oil dipstick, although most other methods are considered satisfactory.
In cold countries, pilots can be observed using home remedies before a cold start, such as an electric heater that blows warm air directed at, for example, the filter housing 10 minutes before takeoff. Of course, remember not to place such devices directly under a component from which, for example, fuel could leak!!
For most Lycoming models, preheating should be used whenever the temperature is -12 ° C or below. The exception to this rule are the 76 series models, which include the O-320-H and O/LO-360-E. These engines should be preheated when the temperature drops below -6 ° C.
It is recommended that these guidelines be followed even when using oil of different viscosities. In addition to difficult starting, failure to properly preheat the entire engine and oil system as recommended can cause small amounts of abnormal wear to internal engine parts, and ultimately reduce engine performance and shorten the time to overhaul.
Water is one of the most likely contaminants in aviation gasoline.
The engine will not run on water and although we can get away with a little moisture in the fuel in warm weather, flying in freezing temperatures makes any moisture in the fuel system very critical. Even a small bubble of moisture can freeze in the fuel line and completely cut off the fuel supply.
If the helicopter/aircraft is parked outside in rain or snow, first, keep the fuel tanks full to prevent condensation and make sure the fuel caps are tight. Second, check the fuel for contaminants before each flight by draining fuel samples from the tanks.
If flying in cold weather is planned, the pre-flight inspection should also include an inspection of the engine breather pipe opening to eliminate any moisture freezing at the end of the breather, which could result in a loss of engine oil.
Starting any engine is usually considered a very simple process. You simply turn the starter and wait for the engine to start purring. Unfortunately, when it gets cold, it is not always that easy. In the case of a piston aircraft engine, there are several factors to consider in order to start on the first try.
Using an external power source to start in very cold weather can be a good procedure. Most of us expect our battery to do the job, but let's not forget that in cold weather, the battery is limited, especially when using single viscosity grade oil. The lower the temperature, the more energy is needed to start the engine.
Speaking of batteries, remember that freezing temperatures are a perfect opportunity to destroy your battery. A fully charged battery will last, but a discharged one... will die.
When this happens, the only way to fix the problem is to replace the battery, so it is very important to take preventive measures.
If the battery dies while trying to start, do not leave it! We must charge the battery immediately.
It is worth noting here that it is easy to overheat the aircraft battery during charging due to its design, which is designed to reduce weight/size, so it is worth using chargers designed for this purpose.
Finally, make sure that the main power switch is turned off when the aircraft/helicopter is parked between flights. If left on, it will drain the battery, and this small mistake can be quite costly.
Oil is another factor to consider in the cold weather starting process. All oils are affected by temperature, as they tend to thicken as temperatures drop. The engine may be reluctant to crank when the oil is thick.
Summer oil is not suitable for use in cold weather, so using multi-viscosity oil and warming up the engine before starting is a good argument here. Because multi-viscosity oils are thinner (lower viscosity), they allow the engine to crank more easily. The easier and faster oil flow also helps to lubricate the internal engine parts more quickly after starting. Proper oil viscosity is very important in all aspects of engine starting and operation. The recommendations for oil grade and temperature range in Lycoming Service Manual 1014 should be followed.
Probably the most important factor in starting an engine is obtaining a satisfactory fuel/air mixture for combustion. Because the engine usually starts very easily, many pilots are unaware of the change in starting procedure required for a successful start under varying temperature conditions.
Warm weather is thinner, so less fuel needs to be mixed with it than cold weather. Also, warm weather fuel will evaporate more easily, making starting easier. Simply put, as temperatures drop, it becomes increasingly important to have a fuel priming plan that will provide the proper fuel/air mixture.
When priming a carbureted engine, the pilot's plan must take into account the temperature, the number of cylinders with priming lines installed, and the number of primer pump strokes needed to create the proper fuel/air mixture. Fuel priming lines and pumps are ordered or installed by the airframe manufacturer, so not all airplanes/helicopters are configured the same.
For example, on Robinson helicopters, the optional fuel priming system has a fuel line to each cylinder, while some airplanes were manufactured with only one cylinder priming. Engines with single-cylinder priming are notoriously difficult to start in cold weather. The number of primed cylinders must be taken into account, since all the fuel supplied by the pump will be distributed to all the cylinders to which the primer pipe is connected. As the air becomes colder and denser, the amount of fuel pumped must be increased. The number of pumpings must be planned by some experimentation, which we will achieve by trial and error for each aircraft individually.
Once the correct number of primer pump strokes for each temperature range is established, the engine will usually start very quickly.
It may be found that the engine starts easily when one stroke of the primer is used in the range of 15˚C, two in the range of 10˚C, three in the range of 5˚C, etc.
This is just an example, which we must determine ourselves by trial and error.
When aircraft maintenance is being carried out before winter, it would be prudent to check these lines to ensure that fuel is flowing through them.
It should be noted that not every aircraft is equipped with a fuel priming system.
Some parts of this article will be aircraft specific and since we come from a helicopter industry based primarily on Robinson helicopters and since we have accustomed our clients to writing articles primarily on helicopters, we would like to address the carbureted R22 and R44 without a priming pump.
As mentioned above, the procedure for starting a cold engine from a warm one differs in the amount of fuel pumped in.
Some people in the middle of winter will crank the throttle 10-15 times to pump fuel, while others will only crank it 5 times.
It is common to see pilots who make injection easier by lifting the pitch levers all the way up during priming. Lifting the levers is related to the correlator.
The correlator is a mechanical linkage that opens the throttle when the pitch lever is raised and closes the throttle when the pitch lever is lowered.
You can observe the correlator in action when the helicopter is turned off and parked in a hangar (just lift the pitch levers and watch the throttle lever retract under the engine). The correlator, unlike the governor, does not use any information about the actual engine/rotor RPM.
Returning to the subject of engines, the amount of fuel needed to obtain the correct fuel/air mixture to start a fuel-injected engine is controlled by time rather than the number of primer pump strokes. With the electric fuel pump on, moving the mixture control to the rich position allows fuel to flow into the cylinders. To start in cold weather, it may be necessary to hold the mixture in the rich position a little longer than on warm days.
The amount of fuel in the air/fuel mixture may be the part we have the most control over when starting the engine, but remember that the amount of throttle opening affects the air that is pumped through the engine. Just as we compensate for cold/dense air by adding more fuel to start, it may also be appropriate to reduce the amount of air in the mixture when the temperature is very low. For example, if the throttle is normally set at 1 cm open for warm weather starting, it may be helpful to reduce this to 0.5 cm in cold weather. Again, this will require some experimentation to determine what is needed to obtain the proper air/fuel mixture for any particular aircraft in any temperature range.
It can be frustrating when an engine does not start easily. Of course, this can happen at any time of year, so it is very tempting to continue grinding the starter motor in order to get it started. If this happens, the starter motor should be rested, otherwise it may not start successfully.
A general rule for starter motors is that they should be used for short periods only and then allowed to cool down. If the engine has not started after three 10-second bursts of operation with rests in between, a five-minute cool-down period is required.
Without a time limit on operation and adequate time to cool down, the starter motor will overheat and will likely be damaged. ,
In the previous paragraphs, we have discussed several issues related to winter preflight and cold weather take-off. There are also other cold weather issues that must be considered when operating the engine.
Assuming the engine has started, the oil pressure gauge should be checked and the oil pressure response characteristics of the engine and aircraft combination should be studied. In most single engine aircraft the response is almost instantaneous. In twin engine aircraft the response can be much slower. In some twin engine aircraft the oil pressure may rise and during warm up may drop again for a short period and then return to normal. All of the above may be normal but it is important to know what to expect.
After starting the engine do not let it run below 1000 rpm. It is not good practice to run the engine below 1000 rpm at any time. This is especially important in cold weather to prevent lead fouling of the spark plugs (exception - Piper Pressurised Navajo).
An important tip for pilots of aircraft with fuel selectors is not to run one of the fuel tanks almost dry before changing tanks! Switch when there is enough reserve fuel left in the first tank used, this can be beneficial if it turns out that the selector valve is frozen.
Although carburetor icing is not necessarily a winter phenomenon, carburetor temperature checks should be carried out during engine start-up. Generally speaking, we can say that carburetor heat should never be used for take-off, but there is one exception. This exception occurs when operating at temperatures so low that the application of carburetor heat causes an increase in RPM. Most pilots will never find themselves in circumstances requiring the use of carburetor heat for take-off and climb, but those who fly carbureted engines will certainly have occasion to use carburetor heat during cruise or descent. The use of the heat in the maximum position or none at all is recommended. The intermediate setting should only be selected if the aircraft is equipped with a Carburetor Air Temperature (CAT) gauge.
One of the major differences between helicopters and airplanes in the use of carburetor heat is that in a helicopter we can use "partial heat," while an airplane pilot should only use full heat or no heat. This operational difference is due to the helicopter being equipped with a Carburetor Air Temperature (CAT) gauge, which allows the pilot to monitor the temperature inside the carburetor. The reason for this anomaly is that an unknown amount of partial heat can actually cause induction ice in the carburetor.
A general rule on Robinson carbureted helicopters is to keep the carburetor air temperature outside the yellow zone of the gauge and apply full heat to the R22 for 15-20 seconds before lowering the pitch lever to below 18 inches on the manifold pressure gauge.
Newer carbureted Robinsons have been equipped with carburetor heat assist to minimize icing accidents. The system is only used during the movement of the pitch lever, so it is definitely too late in the case of lowering the flight and power below 18 inches. The carburetor heats up from 15 to 20 seconds, which means that we still have to remember to heat it up before lowering the lever.
We could go on and on about icing in piston helicopter carburetors, but that would require a separate article.
Engine operating temperature is another issue that is often overlooked in cold weather. We tend to be very cautious about high oil temperatures that we know are detrimental to engine health, while low oil temperatures are more tolerable. The desired oil temperature range for Lycoming engines is 165˚ to 220˚ F (74˚C to 93˚C). If the aircraft is equipped with a winterization kit, it should be installed when operating in outside air temperatures (OAT) below 7˚ C. If a winterization kit is not provided and the engine is not equipped with a thermostatic bypass valve, it may be necessary to improvise a way to shut off some of the airflow to the oil cooler. Maintaining oil temperatures above the minimum recommended temperature is a factor in engine life. Low operating temperatures do not evaporate moisture that accumulates in the oil when the engine breathes moist air for normal combustion. If the minimum recommended oil temperatures are not maintained, the oil should be changed more frequently than the usual 50-hour change interval. This is necessary to eliminate moisture that accumulates and contaminates the oil.
Airplane pilots should avoid power-off descents. This is especially true in cold weather operations where shock cooling of the cylinder heads is likely. It is recommended that the cylinder head temperature change not exceed 50 °F (10 °C) per minute. Plan ahead, reduce power gradually, and maintain some power throughout the descent. Also, maintain a lean fuel-air mixture during the descent. If an exhaust gas temperature gauge is installed on a naturally aspirated engine, it should be kept at the peak position to maximize engine heat at the selected power setting. For turbocharged installations, maximum lean during descent is recommended unless otherwise specified in the aircraft operating manual for the pilot or in conditions where the turbine inlet temperature limit would be exceeded.
Exposure to snow, frost and cold during flight requires consideration of many factors, both airframe and engine related. This article deals with engine related issues and although there may be other issues, only the most frequently asked questions have been addressed.
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