NSN 2840-00-943-2215

Turbine Eng Turbine Disk And Hub

FSC: 2840     NIIN: 009432215
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DODParts.com distributes prime moving; and components aircraft gas turbines and jet engines, aircraft parts and consumables, electrical parts, fittings and other components for the aerospace and defense industries. Submit the short price quote form for NSN 2840-00-943-2215 to receive an up to date pricing and availability quote by email.

Product Characteristics

NSN:
2840009432215
Demilitarization:
DEMIL/MLI
INC:
61833
Shelf Life:
N/A
Special Features:
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 diameter 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 degrees pressure angle
General Description:
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 diameter 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 degrees pressure angle

Part Numbers

  • 1-140-272-01
    HONEYWELL INTERNATIONAL INC.

Shipping & Handling

HMIRS:

No MSDS. No hazardous material.

ESD:

No known electrostatic discharge.

Schedule B:

8411997050 - Parts of gas turbine aircraft engines, other than for use in civil aircraft.

Professional Distribution

  •   ITAR Registered
  •   DDTC Registered
  •   HAZMAT Certified
  •   AS9120 Quality Standards
  •   100% Quality Inspections
ITAR registered supplier

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NSN: 2840-00-943-2215 disk and hub,turbine,turbine eng
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HONEYWELL INTERNATIONAL INC. - 99193