CESSNA SECTION 6
MODEL T182T NAV III WEIGHT AND BALANCE/
GFC 700 AFCS 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). A comprehensive list of
Cessna equipment available for this airplane is included at the back of
this section.
Specific information regarding the weight, arm, moment and installed
equipment for this airplane as delivered from the factory can be found
in the plastic envelope in the back of this POH.
IT IS THE RESPONSIBILITY OF THE PILOT TO MAKE
SURE THE AIRPLANE IS LOADED PROPERLY.
OPERATION OUTSIDE OF PRESCRIBED WEIGHT AND
BALANCE LIMITATIONS COULD RESULT IN AN
ACCIDENT AND SERIOUS OR FATAL INJURY.
AIRPLANE WEIGHING PROCEDURES
1. Preparation:
a. Inflate tires to recommended operating pressures.
b. Defuel airplane. Refer to the Maintenance Manual.
c. Service engine oil as required to obtain a normal full
indication (approximately 8 quarts on dipstick).
d. Move sliding seats to the most forward position.
e. Raise flaps to the fully retracted position.
f. Place all control surfaces in neutral position.
g. Remove all non-required items from airplane.
(Continued Next Page)
T182TPHBUS-01
6-3
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