NSN 2840-00-582-1471

Turbine Engine Turbine Rotor Case

FSC: 2840     NIIN: 005821471
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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 2840-00-582-1471 to receive an up to date pricing and availability quote by email.

Product Characteristics

NSN:
2840005821471
Demilitarization:
DEMIL/MLI
INC:
61679
Shelf Life:
N/A
Special Features:
Flange, cres ams5645, body, cres ams5510, rockwell b scale 90 max hardness, 125 microinch aa surface finish, 7.165 in. Nom o/a lg, 19.240 in. Nom od flange, tapered body, 18.279 in. Min, 18.280 in. Max largest od body, 16.730 in. Min, 16.731 in. Max smallest od body, tapered id, 16.560 in. Min, 16.561 in. Max smallest id countersunk 0.015 in. Nom lg by 45 deg, 18.000 in. Min, 18.001 in. Max largest id countersunk 0.060 in. Nom lg by 45 deg, 42 holes 0.271 in. Min, 0.291 in. Max diameter through flange equally spaced on 18.740 in. Nom bolt circle dia, 3 holes 0.190 in.-32 nf series cl 3b thd through flange on 18.740 in. Nom bolt circle dia, thd holes countersunk 90 degrees by 0.220 in. Nom diameter on back surface of flange, 3 thd holes, 0.250 in.-28 unf series cl 3b thd, through flange on 18.740 in. Nom bolt circle dia, thd holes countersunk 90 degrees by 0.280 in. Nom diameter on back surface of flange, 14 holes 0.256 in. Min, 0.261 in. Max diameter through body equally spaced on outer periphery, 2.264 in. Min, 2.274 in. Ma
General Description:
Flange, cres ams5645, body, cres ams5510, rockwell b scale 90 max hardness, 125 microinch aa surface finish, 7.165 in. Nom o/a lg, 19.240 in. Nom od flange, tapered body, 18.279 in. Min, 18.280 in. Max largest od body, 16.730 in. Min, 16.731 in. Max smallest od body, tapered id, 16.560 in. Min, 16.561 in. Max smallest id countersunk 0.015 in. Nom lg by 45 deg, 18.000 in. Min, 18.001 in. Max largest id countersunk 0.060 in. Nom lg by 45 deg, 42 holes 0.271 in. Min, 0.291 in. Max diameter through flange equally spaced on 18.740 in. Nom bolt circle dia, 3 holes 0.190 in.-32 nf series cl 3b thd through flange on 18.740 in. Nom bolt circle dia, thd holes countersunk 90 degrees by 0.220 in. Nom diameter on back surface of flange, 3 thd holes, 0.250 in.-28 unf series cl 3b thd, through flange on 18.740 in. Nom bolt circle dia, thd holes countersunk 90 degrees by 0.280 in. Nom diameter on back surface of flange, 14 holes 0.256 in. Min, 0.261 in. Max diameter through body equally spaced on outer periphery, 2.264 in. Min, 2.274 in. Max dista

Part Numbers

  • 2-140-073-06
    HONEYWELL INTERNATIONAL INC.
  • 2-140-073-07
    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: 2840-00-582-1471 case,turbine rotor,turbine engine
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HONEYWELL INTERNATIONAL INC. - 99193