Cessna 172s full training pilot course step by step,

 

LONG RANGE CRUISE ALTITUDE CAPABILITY 

The table shows the maximum altitude that can be maintained at a given weight and air temperature (ISA Deviation) based on Long Range Cruise speed, Max Continuous thrust, and 100 ft/min residual rate of climb. 

LONG RANGE CRUISE CONTROL 

The table provides target %N1,  engine inoperative Long Range Cruise Mach number, IAS and fuel flow for the airplane weight and pressure altitude. The fuel flow values in this table reflect single engine fuel burn. 

LONG RANGE CRUISE DIVERSION FUEL AND TIME 

Tables are provided for crews to determine the fuel and time required to proceed to an alternate airfield with one engine inoperative. The data is based on single engine Long Range Cruise speed and 78/280/250 descent. Enter with Air distance as determined from the ground to air miles conversion table and read fuel and time required at the cruise pressure altitude. Adjust the fuel obtained for deviation from the reference weight at checkpoint as required by entering the off reference fuel adjustments table with the fuel required for the reference weight and the actual weight at checkpoint. Read fuel required and time for the actual weight. 

HOLDING 

Target %N1,  indicated airspeed and fuel flow per engine information is tabulated for holding with flaps up based on the FMC optimum holding speed schedule. This is the higher of the maximum endurance speed and the maneuvering speed. Small variations in airspeed will not appreciably affect the overall endurance time. Enter the table with weight and pressure altitude to read %N1, IAS and fuel flow per engine. 

GEAR DOWN LANDING RATE OF CLIMB AVAILABLE 

Rate of climb data is provided as guidance information in the event an engine inoperative landing (manual or Autoland) is planned. The tables show gear down rate of climb available for flaps 15 and flaps 30 Enter the table with TAT and pressure altitude to read rate of climb available. Apply adjustments shown to correct for weight. 

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