TM 55-2840-254-23
4-29 INSPECTTHIRD TURBINE NOZZLE AND SUPPORT (AVIM) (Continued)
4-29
c. Inspect inner shroud (29) as follows:
(1) a. There shall be no more than one crack
(30) per vane extending from vane slot
(31) to aft edge (32).
b. There shall be no circumferential cracks
(32.1).
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Change 2
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