Cessna 172s full training pilot course step by step,

  WELCOME ADVANCE FLYING ACADEMY 

CESSNA 172N SKYHAWK

BRAKE SYSTEM

The airplane has a single-disc, hydraulically-actuated brake on each

main landing gear wheel. Each brake is connected, by ahydraulicline,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 handle under the left side of the Instrument panel. To apply the parking brake, set the brakes with the

rudder pedals, pull the handle aft, and rotate it 90® down.

Por maximum brake life, keep the brake System properly maintained, and minimize brake usage during taxi operations and landings. 

Some of the S3anptoms 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. K, 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.

 👉 CESSNA 172N  HANDBOOK 

👉 PREFLIGHT INSPECTION 

👉 BEFORE STARTING ENGINE

👉 STARTING ENGINE

👉 TAXIING

👉 BEFORE TAKEOFF

👉 NORMAL TAKEOFF

👉 SHORT FIELD TAKEOFF

👉 ENROUTE CLIMB

👉 DESCENT

👉 CESSNA 172N BEFORE LANDING

👉 NORMAL LANDING

👉 SHORT FIELD LANDING

👉 BALKED LANDING

👉 AFTER LANDING

👉 SECURING AIRPLANE 

👉 ENGINE FAILURE DURING TAKEOFF RUN

👉 ENGINE FAILURE AFTER TAKEOFF

👉 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

👉 ENGINE FIRE IN FLIGHT

👉 ELECTRICAL FIRE IN FLIGHT

👉 CABIN FIRE

👉 WING FIRE

👉 INADVERTENT ICING ENCOUNTER

👉 LANDING WITH A FLAT MAIN TIRE

👉 FLIGHT CONTROLS

👉 TRIM SYSTEM

👉 WING FLAP SYSTEM

👉 LANDING GEAR SYSTEM

👉 BAGGAGE COMPARTMENT

👉 CONTROL LOCKS

👉 ENGINE CONTROLS

👉 IGNITION-STARTER SYSTEM

👉 AIR INDUCTION SYSTEM

👉 EXHAUST SYSTEM

👉 CARBURETOR AND PRIMING SYSTEM

👉 COOLING SYSTEM

👉 BRAKE SYSTEM

👉 MASTER SWITCH

👉 AVIONICS POWER SWITCH

👉 AMMETER

👉 CIRCUIT BREAKERS AND FUSES

👉 GROUND SERVICE PLUG RECEPTACLE

👉 EXTERIOR LIGHTING

👉 AIRSPEED INDICATOR

👉 VERTICAL SPEED INDICATOR

👉 ALTIMETER

👉 VACUUM SYSTEM AND INSTRUMENTS

👉 ATTITUDE INDICATOR

👉 DIRECTIONAL INDICATOR

👉 SUCTION GAGE

👉 STALL WARNING SYSTEM

👉 AVIONICS SUPPORT EQUIPMENT

👉 AVIONICS COOLING FAN

👉 ALTERATIONS OR REPAIRS

👉 GROUND HANDLING TOWING

👉 PARKING

👉 TIE-DOWN

👉 JACKING

👉 LEVELING

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