TM 1-2840-252-23-2
4-75
INITIAL SETUP:
Materials:
Anti-Seize Compound (E6)
Applicable Configurations:
All
Lockwire (E33)
Safety Cable (E49)
Tools:
Personnel Required:
Technical Inspection Tool Kit,
Aircraft Powerplant Inspector
Equipment Condition:
Depth, Vernier
Off Engine Task
NOTE
The following steps 1 through 5 require the aid of
another mechanic to support the centerbody.
NOTE
In following step 1, be sure to orient centerbody
drain hole with respect to scribe mark at 12-
o'clock location on forward flange of tailcone
assembly.
Place centerbody (1) with drain hole (2) at 6 o'clock,
1.
aft position, inside tailcone assembly(3).
2.
Align rod holes (4 and 5).
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