WELCOME ADVANCE FLYING ACADEMY
IGNITION-STARTER SYSTEM
Engine ignition is provided by t
wo engine-driven magnetos, and two spark plugs in each cylinder. The right magneto fires both left and right upper spark plugs, and the left magneto fires both left and right lower spark plugs. Normal operation is conducted with both magnetos due to the more complete burning of the fuel-air mixture with dual ignition.
Ignition and starter operation is controlled by a rotary type switch located on the left subpanel. The switch is labeled clockwise, OFF, R, L, BOTH, and START. The engine should be operated on both magnetos (BOTH position) except for magneto checks. The R and L positions are for checking purposes and emergency use only. When the switch is rotated to the spring-loaded START position, (with the master switch in the ON position), the starter contactor is energized and the starter will crank the engine. When the switch is released, it will automatically return to the BOTH position.
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👉 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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