WELCOME ADVANCE FLYING ACADEMY
GROUND CONTROL
Effective ground control while taxiing is accomplished through nose wheel steering by using the rudder pedals; left rudder pedal to steer left and right rudder pedal to steer right. When a rudder pedal is depressed, a spring-loaded steering bungee (which is connected to the nose gear and to the rudder bars) will turn the nose wheel through an arc of approximately 8.5° each side of center. By applying either left or right brake, the degree ©f turn may be increased up to 30° each side of center.
Moving the airplane by hand is most easily accomplished by attaching a tow bar to the nose gear strut. If a tow bar is not available, or pushing is required, use the wing struts as push points. Do not use the vertical or horizontal surfaces to move the airplane. If the airplane is to be towed by vehicle, never turn the nose wheel more than 30° either side of center or structural damage to the nose gear could result.
The minimum turning radius of the airplane, using differential braking and nose wheel steering during taxi, is approximately 24 feet 8 inches. To obtain a minimum radius turn during ground handling, the airplane may be rotated around either main landing gear by pressing down on the tail cone just forward of the vertical stabilizer to raise the nose wheel off the ground
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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