TB 1-1520-238-20-109
22
21
23
24
FWD MOUNT
23.2
23.3
23.1
23
24
AFT MOUNT
AIRCRAFT WITH ELASTOMERIC MOUNTS
q. Paragraph 2.107.6.g.(1). Change note to read as follows:
NOTE
S If bond check exceeds 0.1 OHM, remove vertical stabilizer
and repeat steps a. through g.
S Step h. applies only to aircraft with non-elastomeric mounts.
r.
Paragraph 2.107.6.l. Add note, to read as follows:
NOTE
S On aircraft modified with elastomeric mounts, the two vertical
stabilizer hydraulic line assemblies are installed with the 45_
and 90_ elbows at the back of the vertical stabilizer hard lines.
S On aircraft modified with elastomeric mounts, ensure that the
quick disconnect fittings are attached to the straight end of the
hoses.
S On aircraft that have not been modified with elastomeric mounts,
the two vertical stabilizer hydraulic line assemblies are installed
with the 45_ and 90_ elbows at the bracket on the F.S. 547 frame.
10
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