TM 55-2840-254-23
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INSPECT SECOND TURBINE NOZZLE, SPACER AND CASE (AVIM) (Continued)
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g. Inspect inner shroud (64) as follows:
(1)
There shall be no cracks (65) between
trailing edges of vanes (66).
(2)
There shall be no circumferential cracks
(67) in inner shroud to support braze-
ment (68).
(3)
There shall be no converging cracks (69).
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