Cessna 172s full training pilot course step by step,

 

WELCOME ADVANCE FLYING ACADEMY 

WEIGHT LIMITS

Maximum Takeoff Weight: 1600 lbs.

Maximum Landing Weight: 1600 lbs.

Maximum Weight in Baggage Compartment:

Baggage Area 1 (or passenger on child's seat)-Station 50 to 76:

120 lbs. See note below.

Baggage Area 2 -Station 76 to 94: 40 lbs. See note below.

NOTE

The maximum combined weight capacity for baggage

areas 1 and 2 is 120 lbs

 Click 👉  CESSNA 150 HANDBOOK 

👉 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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