Textron Cessna Grand Caravan Ex 208B, Pilot'S Operating Handbook And Faa Approved Airplane Flight Manual

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CESSNA SECTION 6
MODEL 208B 867 SHP WEIGHT AND BALANCE/
GARMIN G1000 EQUIPMENT LIST
U.S.
INTRODUCTION
This section describes the procedure for establishing the basic empty
weight and moment of the airplane. Sample forms are provided for
reference. Procedures for calculating the weight and moment for
various operations are also provided. For additional information
regarding Weight and Balance procedures, refer to the Aircraft Weight
and Balance Handbook (FAA-H-8083-1).
In order to achieve the performance and flight characteristics which are
designed into the airplane, it must be flown within approved weight and
center of gravity limits. Although the airplane offers flexibility of loading,
it cannot be flown with full fuel tanks and a full complement of
passengers or a normal crew and both cabin and cargo pod (if
installed) loading zones filled to maximum capacity. The pilot must
utilize the loading flexibility to make sure the airplane does not exceed
its maximum weight limits and is loaded within the center of gravity
range before takeoff.
Weight is important because it is a basis for many flight and structural
characteristics. As weight increases, takeoff speed must be greater
since stall speeds are increased, the rate of acceleration decreases,
and the required takeoff distance increases. Weight in excess of the
maximum takeoff weight may be a contributing factor to an accident,
especially when coupled with other factors such as temperature, field
elevation, and runway conditions, all of which may adversely affect the
airplane’s performance. Climb, cruise, and landing performance will
also be affected. Flights at excess weight are possible, and may be
within the performance capability of the airplane, but loads for which
the airplane was not designed may be imposed on the structure,
especially during landing.
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208BPHCUS-00 6-3