Center Of Gravity - Beechcraft C-12C Operator And Technical Reference Manual

6-22. CARGO RESTRAINING METHOD.
To avoid structural damage, all cargo
shall be restrained in accordance with
Beech Kit Drawing No. 101-5040, which
provides the correct
restraint and approved hardware.
Cargo is restrained by passing tiedown
devices over and around the cargo and attaching the
6-24. CENTER OF GRAVITY LIMITATIONS.
Center of gravity limitations are expressed in
ARM inches, which refers to a positive measurement
from the aircraft's reference datum. The forward CG
limit at 11,279 pounds or less is 181.0 ARM inches. At
CAUTION
methods for
Section VII. CENTER OF GRAVITY
ends of the tiedown device to the seat tracks as
shown in Figure 6-9.
devices required to restrain a given weight of cargo
may vary.
6-23. CARGO UNLOADING.
Unloading of cargo shall be accomplished
through the cabin door
12,500 pounds, the forward CG limit is 185.0 ARM
inches and a straight-line variation is used between
given points. At 12,500 pounds or less, the aft CG
limit is 196.4 ARM inches.
Limitations graph is designed to establish forward and
aft CG limitations. Refer to Figures 6-7 and 6-8.
TM 1-1520-218-10
The number of tiedown
C or cargo door D T .
The Center of Gravity
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