WELCOME ADVANCE FLYING ACADEMY
BRAKE SYSTEM
The airplane has a single-disc, hydraulically-actuated brake on each main landing gear wheel. Each brake is connected, by a hydraulic line, to a master cylinder attached to each of the pilot's rudder pedals. The brakes are operated by applying pressure to the top of either the left (pilot's) or right (copilot's) set of rudder pedals, which are interconnected. When the airplane is parked, both main wheel brakes may be set by utilizing the parking brake which is operated by a knob on the lower left side of the instrument panel. For maximum brake life, keep the brake system properly maintained, and minimize brake usage during taxi operations and landings. Some of the symptoms of impending brake failure are: gradual decrease in braking action after brake application, noisy or dragging brakes, soft or spongy pedals, and excessive travel and weak braking action. If any of these symptoms appear, the brake system is in need of immediate attention. If, during taxi or landing roll, braking action decreases, let up on the pedals and then re-apply the brakes with heavy pressure. If the brakes become spongy or pedal travel increases, pumping the pedals should build braking pressure. If one brake becomes weak or fails, use the other brake sparingly while using opposite rudder, as required, to offset the good brake
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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