Part Number 2-140-058-11 Turbine Nozzle Ring

Engine T-55

Cres AMS5532, rockwell 30T scale 72 min, 91.5 max hardness, 16.265 in.Min, 16.295 in. Max id 1ST end, 16.110 in. Nom id 2ND end, 0.170 in. Nomstep lg 2ND end, 16.680 in. Nom od flange 1ST end, 0.032 in. Min, 0.040 in.Max flange thk, 1.060 in. Nom o/a h, 21 holes 0.373 in. Min, 0.380 in.Max diameter equally spaced on 1ST end od, 0.396 in. Min, 0.400 in. Max lgfrom flange to center of holes

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