SOLOY TURBINE PAC
SECTION 6
POHS CESSNA T206H/206H
WEIGHT & BALANCE/
EQUIPMENT LIST
6
-3
F.A.A. Approved
May 23, 2003
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
WEIGHT AND BALANCE
– No Change
SAMPLE WEIGHT AND BALANCE FORMS (FIGURES 6-1
AND 6-2)
–
Add the Following Changes:
Figure 6
-1:
Oil Quantity:
9 U.S. Quarts
Oil Weight:
8 lbs./gal.
Oil Arm:
-32.0 inches
Fuel Weight:
6.7 lbs./gal.
Loading Arrangements (Figures 6-3, 6-4, 6-5 and 6-6) -- No Change
NOTE
Cessna Cargo Pod not approved for use
with turbine powered Cessna 206.
Sample Loading Problem – See Figure 6-7
See Loading Graph – See Figure 6-8
Center of Gravity Moment Envelope (Figure 6-9) – No Change
Center of Gravity Limits (Figure 6-10) – No Change
UNCONTROLLED
COPY
