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Turbine Nozzle Retainer Assembly

Model / MPN: 1-140-290-02 | NSN: 2840-00-019-8009
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Product Details
NATO Stock Number
2840-00-019-8009
Sold in multiples of
1 EA
DEMIL
NO
End Application
T-53 series engines
General Description
Cres, ams5510, rockwell 30t scale 76 max hardness, 14.850 in. Min, 14.880 in. Max od, 12.780 in. Min, 12.785 in. Max id, 2.250 in. Nom o/a lg, 44 holes 0.220 in. Nom diameter through support flange, equally spaced on 14.250in. Bolt circle dia, 24 holes 0.060 in. Min, 0.065 in. Max diameter through bodyod, equally spaced, 0.105 in. Min, 0.115 in. Max from end

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1-140-290-02 Cross Reference
  • 1-140-290-02