NSN 2840-00-591-0741

Turbine Eng Turbine Disk And Hub

FSC: 2840     NIIN: 005910741
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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 2840-00-591-0741 to receive an up to date pricing and availability quote by email.

Product Characteristics

NSN:
2840005910741
Demilitarization:
DEMIL/MLI
INC:
61833
Shelf Life:
N/A
Special Features:
Cres, m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 3.805 in. Min, 3.815 in. Max o/a lg, 9.820 in. Nom od disk, 1.394 in.Min, 1.397 in. Max lg disk, 60 blade grooves equally spaced on diskod, 2 stepped hubs, 2.830 in. Min, 2.840 in. Max od 1st step 1st end, 0.700 in. Nom lg 1st step 1st end, 3.320 in. Nom diameter 2nd step 1stend, 0.603 in. Min, 0.607 in. Max lg 2nd step 1st end, externalsplines 1st step 2nd end, 69 teeth, 30 degrees pressure angle, 2.8750 in.Nom pitch dia, 0.380 in. Min, 0.420 in. Max lg splines, 0.681 in.Min, 0.738 in. Max lg 2nd step 2nd end, stepped bore, 3.805 in. Min, 3.815 in. Max o/a lg bore, 2.5576 in. Min, 2.5579 in. Max diameter 1ststep 1st end, 0.950 in. Nom lg 1st step 1st end, 2.566 in. Min, 2.576 in. Max diameter 2nd step 1st end, 0.600 in. Nom lg 2nd step 1stend, 2.2133 in. Min, 2.2137 in. Max diameter 1st step 2nd end, 0.275 in.Min, 0.295 in. Max lg 1st step 2nd end, 2.425 in. Min, 2.435 in. Maxdia 2nd step 2nd end, 0.165 in. Min, 0.205 in. Max lg 2nd step 2ndend, internal splines 3rd s
General Description:
Cres, m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 3.805 in. Min, 3.815 in. Max o/a lg, 9.820 in. Nom od disk, 1.394 in.Min, 1.397 in. Max lg disk, 60 blade grooves equally spaced on diskod, 2 stepped hubs, 2.830 in. Min, 2.840 in. Max od 1st step 1st end, 0.700 in. Nom lg 1st step 1st end, 3.320 in. Nom diameter 2nd step 1stend, 0.603 in. Min, 0.607 in. Max lg 2nd step 1st end, externalsplines 1st step 2nd end, 69 teeth, 30 degrees pressure angle, 2.8750 in.Nom pitch dia, 0.380 in. Min, 0.420 in. Max lg splines, 0.681 in.Min, 0.738 in. Max lg 2nd step 2nd end, stepped bore, 3.805 in. Min, 3.815 in. Max o/a lg bore, 2.5576 in. Min, 2.5579 in. Max diameter 1ststep 1st end, 0.950 in. Nom lg 1st step 1st end, 2.566 in. Min, 2.576 in. Max diameter 2nd step 1st end, 0.600 in. Nom lg 2nd step 1stend, 2.2133 in. Min, 2.2137 in. Max diameter 1st step 2nd end, 0.275 in.Min, 0.295 in. Max lg 1st step 2nd end, 2.425 in. Min, 2.435 in. Maxdia 2nd step 2nd end, 0.165 in. Min, 0.205 in. Max lg 2nd step 2ndend, internal splines 3rd step 2nd

Part Numbers

  • 2-141-057-17
    HONEYWELL INTERNATIONAL INC.
  • V2-141-057-17
    VERICOR POWER SYSTEMS LLC

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: 2840-00-591-0741 disk and hub,turbine,turbine eng
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Cage Codes
HONEYWELL INTERNATIONAL INC. - 99193
VERICOR POWER SYSTEMS LLC - 1N8S8