WELCOME ADVANCE FLYING ACADEMY
AIR INDUCTION SYSTEM
The engine air induction system receives ram air through an intake in the lower front portion of the engine cowling. The intake is covered by an air filter which removes dust and other foreign matter from the induction air. Airflow passing through the filter enters an airbox. After passing through the airbox, induction air enters the inlet in the carburetor which is under the engine, and is then ducted to the engine cylinders through intake manifold tubes. In the event carburetor ice is encountered or the intake filter becomes blocked, alternate heated air can be obtained from the right muffler shroud through a duct to a valve, in the airbox, operated by the carburetor heat control on the instrument panel. Heated air from the muffler shroud is obtained from an unfiltered outside source. Use of full carburetor heat at full throttle wilFresult in a loss of approximately 200 to 250 RPM.
Click 👉 CESSNA 150 HANDBOOK
👉 PREFLIGHT INSPECTION
👉 STARTING ENGINE
👉 TAXIING
👉 BEFORE TAKEOFF
👉 TAKEOFF
👉 SHORT FIELD TAKEOFF
👉 ENROUTE CLIMB
👉 CRUISE
👉 BEFORE LANDING
👉 LANDING
👉 SHORT FIELD LANDING
👉 BALKED LANDING
👉 AFTER LANDING
👉 SECURING AIRPLANE
👉 ENGINE
👉 PROPELLER
👉 MAXIMUM CERTIFICATED WEIGHTS
👉 STANDARD AIRPLANE WEIGHTS
👉 FUEL & OIL CAPACITY
👉 INSTRUMENT PANEL VOCABULARY
👉 WEIGHT LIMITS
👉 MANEUVER LIMITS
👉 FLIGHT LOAD FACTOR LIMITS
👉 KINDS OF OPERATION LIMITS
👉 FUEL LIMITATIONS
👉 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
👉 ELECTRICAL FIRE IN FLIGHT
👉 CABIN FIRE
👉 WING FIRE
👉 INADVERTENT ICING ENCOUNTER
👉 LANDING WITH A FLAT MAIN TIRE
👉 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS
👉 ENGINE FAILURE
👉 FORCED LANDINGS
👉 LANDING WITHOUT ELEVATOR CONTROL
👉 FIRES
👉 EMERGENCY OPERATION IN CLOUDS
👉 EXECUTING A 180° TURN IN CLOUDS
👉 EMERGENCY DESCENT THROU GH CLOUDS
👉 RECOVERY FROM A SPIRAL DIVE
👉 FLIGHT IN ICING CONDITIONS
👉 SPINS
👉 CARBURETOR ICING
👉 SPARK PLUG FOULING
👉 MAGNETO MALFUNCTION
👉 LOW OIL PRESSURE
👉 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS
👉 INSUFFICIENT RATE OF CHARGE
👉 NOISE ABATEMENT
👉 AIRFRAME
👉 FLIGHT CONTROLS
👉 TRIM SYSTEM
👉 INSTRUMENT PANEL
👉 GROUND CONTROL
👉 WING FLAP SYSTEM
👉 LANDING GEAR SYSTEM
👉 BAGGAGE COMPARTMENT
👉 SEATS
👉 SEAT BELTS AND SHOULDER HARNESSES
👉 ENTRANCE DOORS AND CABIN WINDOWS
👉 CONTROL LOCKS
👉 ENGINE CONTROLS
👉 ENGINE INSTRUMENTS
👉 NEW ENGINE BREAK-IN AND OPERATION
👉 ENGINE OIL SYSTEM
👉 AIR INDUCTION SYSTEM
👉 EXHAUST SYSTEM
👉 CARBURETOR AND PRIMING SYSTEM
👉 COOLING SYSTEM
👉 BRAKE SYSTEM
👉 ELECTRICAL SYSTEM
👉 OVER-VOLTAGE SENSOR AND WARNING LIGHT
👉 CIRCUIT BREAKERS AND FUSES
👉 GROUND SERVICE PLUG RECEPTACLE
👉 EXTERIOR LIGHTING
👉 INTERIOR LIGHTING
👉 VENTILATING AND
👉 PITOT-STATIC SYSTEM AND INSTRUMENTS
👉 AIRSPEED INDICATOR
👉 ALTIMETER
👉 VACUUM SYSTEM AND INSTRUMENTS
👉 ATTITUDE INDICATOR
👉 SUCTION GAGE
👉 STALL WARNING SYSTEM
👉 AVIONICS SUPPORT EQUIPMENT
👉 STATIC DISCHARGERS
👉 IDENTIFICATION PLATE
👉 PUBLICATIONS
👉 AIRPLANE FILE
👉 AIRPLANE INSPECTION PERIODS
👉 CESSNA CUSTOMER CARE PROGRAM
👉 PARKING
👉 TIE-DOWN
👉 JACKING
👉 LEVELING
👉 FLYABLE STORAGE
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