TM 55-2840-254-23
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INSPECT SECOND TURBINE NOZZLE, SPACER AND CASE (AVIM) (Continued)
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(4)
There shall be no radial cracks (12) from
inner shroud (13) longer than 3/4 inch.
(5)
There shall be no more than four vanes
(15) with radial cracks (14) from inner
shroud (13) longer than 3/8 inch.
(6)
There shall be no cracks (16) with vane
core visible.
(7)
There shall be no vane with more than
three radial cracks longer than 3/8 inch.
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