2840-00-943-2215

Turbine Engine Turbine Disk And Hub email this page
ITAR Registered

Model or part number: 1-140-272-01

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About this product
Cres;m3603;electrofilm p6435-2 internal spline;rockwell a scale 69 min;73 max hardness;9.913 in. Nom o/a lg; 8.629 in. Min;8.639 in. Max od;7.730 in min;7.770 in. Max id 1st end;1.905 in. Min;1.910 in.Max od 2nd end;1.882 in. Min;1.892 in. Max od 2nd end 1st step;0.550 in. Nom lg 2nd end;externalthd 1st step 2nd end;1.9670-18 ns cl 3thd;1.9264 in. Min;1.9309 in. Max pitch dia;0.450 in. Nom thd lg;1.877 in. Min;1.887 in. Max dia 2nd step 2nd end0.100 in. Lg 2nd step 2nd step 2nd end;1.9683 in. Min;1.965 in. Max od 3rd step 2nd end;1.770 in. Nom lg 4th step2nd end end;2.740 in. Nom lg 4th step 2nd end;2.1655 in. Min;2.1658 in. Max 0d 5th step 2nd end;1.520 in. Nom lg 5th step 2nd end;2.410 in. Nom od 6th step 2nd end;internal thd 2nd end;0.390 in. Thd lg;1.5620-16 uns cl 3b;1.5214 in. Min;1.5254 in. Max pitch dia;internal spline;24 teeth;1.438 in. Min;1.443 in. Max id;1.5000 in. Nom pitch dia;30 deg pressure angle

pdf NSN 2840-00-943-2215 Datasheet

MRC:
A recording of the physical,functional,and performance characteristics for an item of supply.TEXT
General Description:
Cres; m3603; electrofilm p6435-2 internal spline; rockwell a scale 69 min; 73 maximum hardness; 9.913 in. Nom o/a lg; 8.629 in. Min; 8.639 in. Maximum od; 7.730 in min; 7.770 in. Maximum id 1st end; 1.905 in. Min; 1.910 in.Max od 2nd end; 1.882 in. Min; 1.892 in. Maximum od 2nd end 1st step; 0.550 in. Nom lg 2nd end; externalthd 1st step 2nd end; 1.9670-18 ns cl 3thd; 1.9264 in. Min; 1.9309 in. Maximum pitch dia; 0.450 in. Nom thd lg; 1.877 in. Min; 1.887 in. Maximum diameter 2nd step 2nd end0.100 in. Lg 2nd step 2nd step 2nd end; 1.9683 in. Min; 1.965 in. Maximum od 3rd step 2nd end; 1.770 in. Nom lg 4th step2nd end end; 2.740 in. Nom lg 4th step 2nd end; 2.1655 in. Min; 2.1658 in. Maximum 0d 5th step 2nd end; 1.520 in. Nom lg 5th step 2nd end; 2.410 in. Nom od 6th step 2nd end; internal thd 2nd end; 0.390 in. Thd lg; 1.5620-16 uns cl 3b; 1.5214 in. Min; 1.5254 in. Maximum pitch dia; internal spline; 24 teeth; 1.438 in. Min; 1.443 in. Maximum id; 1.5000 in. Nom pitch dia; 30 degrees pressure angle
MRC:
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NIIN:
009432215
MRC:
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NATO Stock Number:
2840-00-943-2215
MRC:
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Shelf Life:
N/A
MRC:
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UOM:
--
MRC:
--
DEMIL:
FIIG:
--
FIIG:
A23900
MRC:
--
INC:
61833
MRC:
--
IMM:
CX CX
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Formal Definition

Government issue definition of NSN 2840-00-943-2215

Inc 61833 cancelled/replaced by ,inc 50566, fiig a10700, app-key f ,inc 50565, fiig a10700, app-key f ,on 021513 ~(all except usa). A disk having provisions on the outer periphery for attaching turbine blades and an integral hub that provides support for the turbine and/or a means of attachment for a shaft. See also disk,turbine,turbine engine.

Import / Export

Schedule B Classification
Schedule B Number
NAIC National Association of Insurance Commissioners
End Use A classification system for U.S. exported and imported merchandise based on principal use rather than the physical characteristics of the merchandise. End-Use codes are assigned by the Bureau of Economic Analysis under the U.S. Department of Commerce.
SITC Commodity classification system defined by the United Nations.
USDA
HITECH
Schedule B:
8411997050
NAICS:
336412
End Use Class:
50020
SITC:
71499
USDA:
1
HITECH:
8

Schedule B Codes Definitions:

Schedule B 8411997050

Parts Of Gas Turbine Aircraft Engines, Other Than For Use In Civil Aircraft

End Use Code 50020

Engines and Turbines For Military Aircraft

Standard Intl. Trade Class (SITC) 71499

Parts For Gas Turbines, N.e.s.

Manufacturers

This NSN is registered to the following cage codes.
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