Cessna 172s full training pilot course step by step,

 

WELCOME ADVANCE FLYING ACADEMY 

TAKEOFF

NORMAL TAKEOFF

(1) Wing Flaps -- 0°.

(2) Carburetor Heat -- COLD.

(3) Throttle -- FULL OPEN.

(4) Elevator Control -- LIFT NOSE WHEEL at 50 KIAS.

(5) Climb Speed -- 60-70 KIAS.

TAKEOFF

POWER CHECK

It is important to check full-throttle engine operation early in the takeoff run. Any sign of rough engine operation or sluggish engine acceleration is good cause for discontinuing the takeoff. If this occurs, you are justified in making a thorough full-throttle static runup before another takeoff is attempted. The engine should run smoothly and turn approximately 2460 to 2560 RPM with carburetor heat off and mixture full rich.

NOTE

At higher airport altitudes, this check should be made with the mixture leaned to provide maximum engine

Full throttle runups over loose gravel are especially harmful to propeller tips. When takeoffs must be made over a gravel surface, it is very important that the throttle be advanced slowly. This allows the airplane to start rolling before high RPM is developed, and the gravel will be blown back of the propeller rather than pulled into it. When unavoidable small dents appear in the propeller blades, they should be immediately corrected as described in Section 8 under Propeller Care. 

Prior to takeoff from fields above 5000 feet elevation, the mixture should be leaned to give maximum RPM in a full-throttle, static runup.

After full throttle is applied, adjust the throttle friction lock clockwise to prevent the throttle from creeping back from a maximum power position. Similar friction lock adjustment should be made as required in other flight conditions to maintain a fixed throttle setting.

FLAP SETTINGS

Normal and short field takeoffs are performed with flaps up. The use of 10° flaps will shorten the ground run approximately 10%, but this advantage is lost in the climb to a 50-foot obstacle. Therefore, the use of 10° flaps is reserved for minimum ground runs or for takeoff from soft or rough fields.

 If 10° of flaps are used on soft or rough fields with obstacles ahead, it is preferable to leave them extended rather than retract them in the climb to the obstacle. The exception to this rule would be in a high altitude takeoff in hot weather where climb would be marginal with flaps 10°. Flap deflections greater than 10° are not approved for takeoff.

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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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