TM 55-2840-254-23
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INSPECT SECOND TURBINE NOZZLE, SPACER AND CASE (AVIM) (Continued)
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f. Inspect inner shroud (24) as follows:
(1)
(2)
(3)
There shall be no cracks (25) between
leading edges of vanes (9).
There shall be no circumferential cracks
(26) in inner shroud to support braze-
ment (27).
There shall be no converging cracks (28).
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