Cessna 172s full training pilot course step by step,

 

WELCOME ADVANCE FLYING ACADEMY 

ENROUTE CLIMB

(1) Airspeed -- 65-75 KIAS

(2) Throttle -- FULL OPEN.

(3) Mixture -- FULL RICH (mixture may be leaned above 5000 feet)

ENROUTE CLIMB

When conducting the following climbs, the mixture should be full rich below 5000 feet and may be leaned, if necessary, above 5000 feet for smoother engine operation.

NORMAL CLIMB

Normal climbs are conducted at 65 to 75 KIAS with flaps up and full throttle for best engine cooling.

BEST RATE OF CLIMB

The best rate of climb speeds range from 68 KIAS at sea level to 62 KIAS at 10, 000 feet with flaps up and full throttle.

BEST ANGLE OF CLIMB

If enroute terrain dictates the use of a steep climb angle, climb at the best angle of climb speed of 56 KIAS with flaps up and full throttle.

NOTE

Steep climbs at low airspeeds should be of short duration to allow improved engine cooling

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👉 PREFLIGHT INSPECTION

👉 BEFORE STARTING ENGINE

👉 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

👉 POWER PLANT LIMITATIONS

👉 FUEL & OIL CAPACITY

👉 INSTRUMENT PANEL VOCABULARY

👉 WEIGHT LIMITS

👉 CENTER OF GRAVITY 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

👉 ENGINE FIRE IN FLIGHT

👉 ELECTRICAL FIRE IN FLIGHT

👉 CABIN FIRE

👉 WING FIRE

👉 INADVERTENT ICING ENCOUNTER

👉 LANDING WITH A FLAT MAIN TIRE

👉 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS

👉 AMMETER SHOWS DISCHARGE

👉 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

👉 EXCESSIVE RATE OF CHARGE

👉 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

👉 IGNITION-STARTER 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

DEFROSTING SYSTEM

👉 PITOT-STATIC SYSTEM AND INSTRUMENTS

👉 AIRSPEED INDICATOR

👉 RATE-OF-CLIMB INDICATOR

👉 ALTIMETER

👉 VACUUM SYSTEM AND INSTRUMENTS

👉 ATTITUDE INDICATOR

👉 DIRECTIONAL INDICATOR

👉 SUCTION GAGE

👉 STALL WARNING SYSTEM

👉 AVIONICS SUPPORT EQUIPMENT

👉 STATIC DISCHARGERS

👉 IDENTIFICATION PLATE

👉 OWNER FOLLOW-UP SYSTEM

👉 PUBLICATIONS

👉 AIRPLANE FILE

👉 AIRPLANE INSPECTION PERIODS

👉 CESSNA PROGRESSIVE CARE

👉 CESSNA CUSTOMER CARE PROGRAM

👉 ALTERATIONS OR REPAIRS

👉 GROUND HANDLING TOWING

👉 PARKING

👉 TIE-DOWN

👉 JACKING

👉 LEVELING

👉 FLYABLE STORAGE

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