TM 1-1520-218-10
6-17/(6-18 blank)
6-22. CARGO RESTRAINING METHOD.
CAUTION
To avoid structural damage, all cargo
shall be restrained in accordance with
Beech Kit Drawing No. 101-5040, which
provides
the
correct
methods
for
restraint and approved hardware.
Cargo is restrained by passing tiedown
devices over and around the cargo and attaching the
ends of the tiedown device to the seat tracks as
shown in Figure 6-9. The number of tiedown
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 C or cargo door D T .
Section VII. CENTER OF GRAVITY
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
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. The Center of Gravity
Limitations graph is designed to establish forward and
aft CG limitations. Refer to Figures 6-7 and 6-8.
