WELCOME ADVANCE FLYING ACADEMY
ENGINE OIL SYSTEM
An oil sump on the bottom of the engine supplies a total capacity of six quarts to the engine for lubrication (one additional quart is required if a full flow oil filter is installed.) The oil is drawn from the sump through a filter screen on the end of a pick-up tube to the engine driven oil pump. The pump feeds the oil, under pressure, through a filter screen (full flow oil filter and/or oil cooler, if installed), and is then circulated to the left and right oil galleries. The engine parts are then lubricated, under pressure, from the galleries. Oil pressure to the galleries is regulated by a pressure relief valve at the rear of the right oil gallery. After lubricating the engine, the oil returns to the sump by gravity. If a full flow oil filter is installed, the filter adapter is equipped with a bypass valve which will cause lubricating oil to bypass the filter in the event the filter becomes plugged, or the oil temperature is extremely cold. An oil filler cap/oil dipstick is located at the rear of the engine on the right side. The filler cap/dipstick is accessible through an access door in the engine cowling. The engine should not be operated on less than four quarts of oil. To minimize loss of oil through the breather, fill to five quarts for normal flights of less than three hours. For extended flight,fill to six quarts (dipstick indication only). For engine oil grade and specifications,
An oil quick-drain valve is available to replace the drain plug in the oil sump drain port, and provides quicker, cleaner draining of the engine oil. To drain the oil with this valve installed, slip a hose over the end of the valve and push upward on the end of the valve until it snaps into the open position. Spring clips will hold the valve open. After draining, use a suitable tool to snap the valve into the extended (closed) position and remove the drain hose.
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👉 TAXIING
👉 TAKEOFF
👉 CRUISE
👉 LANDING
👉 ENGINE
👉 MAXIMUM CERTIFICATED WEIGHTS
👉 AIRSPEEDS FOR EMERGENCY OPERATION
👉 ENGINE FAILURE DURING TAKEOFF RUN
👉 ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
👉 ENGINE FAILURE DURING FLIGHT
👉 EMERGENCY LANDING WITHOUT ENGINE POWER
👉 PRECAUTIONARY LANDING WITH ENGINE POWER
👉 DITCHING
👉 FIRES DURING START ON GROUND
👉 LANDING WITH A FLAT MAIN TIRE
👉 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS
👉 LANDING WITHOUT ELEVATOR CONTROL
👉 FIRES
👉 EMERGENCY OPERATION IN CLOUDS
👉 EXECUTING A 180° TURN IN CLOUDS
👉 EMERGENCY DESCENT THROU GH CLOUDS
👉 SPINS
👉 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS
👉 AIRFRAME
👉 SEATS
👉 SEAT BELTS AND SHOULDER HARNESSES
👉 ENTRANCE DOORS AND CABIN WINDOWS
👉 NEW ENGINE BREAK-IN AND OPERATION
👉 CARBURETOR AND PRIMING SYSTEM
👉 OVER-VOLTAGE SENSOR AND WARNING LIGHT
👉 GROUND SERVICE PLUG RECEPTACLE
👉 PITOT-STATIC SYSTEM AND INSTRUMENTS
👉 VACUUM SYSTEM AND INSTRUMENTS
👉 CESSNA CUSTOMER CARE PROGRAM
👉 PARKING
👉 TIE-DOWN
👉 JACKING
👉 LEVELING
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