TM 55-2840-254-23
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1-93 INSPECT ENGINE HOT END (AVIM) (Continued)
(2) There shall be no converging cracks
(171) which could result in loss of ma-
terial.
(3) There shall be no holes (172) burned
through.
d. Inspect swirler cup outer edges (173) as fol-
lows :
(1) There shall be no circular cracks (174).
(2) There shall be no radial cracks (175)
longer than 3/16-inch.
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