PILOT’S OPERATING HANDBOOK
SECTION 6
WEIGHT AND BALANCE
Edition 0 -- October 31, 2013
Rev. 1
Page 6.4.11
DETERMINING EMPTY AIRPLANE CHARACTERISTICS
Empty airplane characteristics (weight and balance) may vary with regard to those indicated on weighing form
according to installed optional equipment and installed seats.
List of equipment (refer to paragraph 6.5) contains the standard and optional equipment, as well as their
characteristics (weight, arm), except those listed in this Chapter.
Use the chart below to compute new empty weight and corresponding balance if necessary.
DATE
EQUIPMENT OR MODIFICATION DESCRIPTION
(+)
(-)
WEIGHT MODIFICATION
BASIC EMPTY WEIGHT
Weight
lb
Arm
in.
Moment
lb.in/1000
Weight
W
Arm
”d
o
”
Moment
According to delivery
Figure 6.4.3 - SAMPLE WEIGHT AND BALANCE RECORD
CG m.a.c.%
=
(do
−
172.93)
59.45
×
100
Use the above formula to express arm ”d
o
” in % of mean aerodynamic chord.
NOTE
Arm expressed in inches with regard to reference.
FWD baggage compartment :
128.0 in. (3.250 m)
Baggage compartment in pressurized cabin : 303.0 in. (7.695 m)
Fuel :
189.8 in. (4.820 m)
Содержание TBM 900
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