(1)
Remove retaining ring from forward end of LPT shaft, using a scriber.
S 022-004-C00
(2)
Remove LPT shaft plug using puller adapter, 856A2573 or 856A2632. S 022-005-C00
(3)
Remove and discard O-rings located in forward/aft grooves. S 022-006-C00
(4)
AIRPLANES WITH CFMI SB 72-069; Remove and discard O-rings located in machining undercut relief.
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S 022-007-C00
(5) Remove the puller adapter from the LPT shaft plug. Install the LPT shaft plug in the storage box.
D. Installation of LPT shaft plug
S 462-013-C00
CAUTION: IT IS ESSENTIAL TO CORRECTLY INSTALL NEW O-RING INTO THE SEAL
_______ GROOVE PROVIDED FOR THIS PURPOSE AT THE FORWARD END OF THE LPT SHAFT PLUG.
(1)
Lightly coat new O-rings with engine oil (CP2442) and install into forward groove and machined undercut relief of LPT shaft plug forward end.
S 642-010-C00
(2)
Lightly coat new O-ring with engine oil (CP2442) and install into aft groove of LPT shaft plug.
S 422-011-C00
(3)
Install LPT shaft plug assembly into forward end of LPT shaft and onto center vent tube.
NOTE: Insert lug of LPT shaft plug in aligned slots of LPT coupling
____
nut and LPT shaft.
S 422-012-C00
(4) Install retaining ring onto LPT shaft (Fig. 201).
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SEE A
ADAPTER
SNAP ON PULLER
O-RING
A
LPT SHAFT
PLUG
O-RINGS
LPT SHAFT
RETAINING RING
A
A
Low Pressure Turbine Shaft Assembly Figure 201 (Sheet 1)
K66523
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B
Low Pressure Turbine Shaft Assembly
Figure 201 (Sheet 2)
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K66525
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TURBINE FRAME - DESCRIPTION AND OPERATION
_________________________________________
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