SOLOY TURBINE PAC
SECTION 6
POHS CESSNA U/TU 206G
WEIGHT & BALANCE/
EQUIPMENT LIST
6
-3
F.A.A. Approved
October 4, 2005
INTRODUCTION
This section supplies supplemental information for establishing
the basic empty weight and moment of the airplane.
Supplemental information for calculating the weight and moments
for various operations is also provided.
It should be noted that specific information regarding the weight,
arm, moment and installed equipment list for this airplane can
only be found in the appropriate weight and balance records
carried in the airplane.
AIRPLANE WEIGHING PROCEDURES
– No Change
SAMPLE WEIGHT AND BALANCE FORMS
(FIGURES 6-1 AND 6-2)
–
No change except:
Figure 6
-1:
Oil Quantity:
9 U.S.
Quarts
Oil Weight:
8 lbs./gal.
Oil Arm:
Fuel Weight:
6.7
lbs./gal.
WEIGHT AND BALANCE
– No Change
Loading Arrangements (Figures 6-3, 6-4, 6-5 and 6-6) -- No
Change
Sample Loading Problem (See Figure 6-7)
Center of Gravity Moment Envelope (Figure 6-9) – No Change
Center of Gravity Limits (Figure 6-10) – No Change
EQUIPMENT LIST
– No Change except:
The equipment list description has been revised to delete certain Code
R equipment and to install items as necessary for this modification.
UNCONTROLLED
COPY
