WELCOME ADVANCE FLYING ACADEMY
TAXIING
When taxiing, it is important that speed and use of brakes be held to a minimum and that all controls be utilized to maintain directional control and balance.
The carburetor heat control knob should be pushed full in during all ground operations unless heat is absolutely necessary. When the knob is pulled out to the heat position, air entering the engine is not filtered.
Taxiing over loose gravel or cinders should be done at low engine speed to avoid abrasion and stone damage to the propeller tips.
The nose wheel is designed to automatically center straight ahead when the nose strut is fully extended. In the event the nose strut is over-inflated and the airplane is loaded to a rearward center of gravity position, it may be necessary to partially compress the strut to permit steering. This can be accomplished prior to taxiing by depressing the airplane nose (by hand) or during taxi by sharply applying brakes.
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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