Rolls-Royce® M250 Power Turbine Coupling Nut 23030981

Rolls-Royce® M250 Power Turbine Coupling Nut 23030981

Rolls Royce M250 Piece Parts

Part # 23030981=64

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Mfr Part # 23030981

8130-3 Eligible
8130-3 Eligible
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Boeing Distribution (formerly Aviall)

Specifications

  • Nut Counterbore Depth: 0.110 Inches Nominal First End
  • Counterbore Diameter: 1.200 Inches Nominal First End
  • Nut Diameter: 1.490 Inches Nominal
  • Nominal Thread Size: 1.156 Inches
  • Small End Diameter: 1.350 Inches Nominal
  • Surface Treatment: Nickel Overall
  • Nut Counterbore Depth: 0.150 Inches Nominal Second End
  • Flange Thickness: 0.260 Inches Nominal
  • Nut Thickness: 0.520 Inches Nominal
  • Material: Steel Corrosion Resisting Overall
  • Thread Series: Buttress
  • Thread Quantity Per Inch: 24
  • Drive Point Depth: 0.070 Inches Nominal
  • Drive Point Width: 0.185 Inches Minimum and 0.195 Inches Maximum
  • Thread Pitch Diameters: +1.1312 To 1.1350 Inches
  • Drive Point Quantity: 4
  • Counterbore Diameter: 1.180 Inches Minimum Second End and 1.190 Inches Maximum Second End
  • Nut Style: Round
  • Hardness Rating: 35.0 Rockwell C Minimum and 40.0 Rockwell C Maximum
  • Undercut Thickness: 0.110 Inches Nominal
  • Thread Direction: Left-Hand

Technical Information

NIIN

011474907

NSN

5310-01-147-4907

FSCG

5310

FSCG Category

Nuts and Washers

FAA Approval Code

PC

Condition

New

CAGE Code

63005

Country of Origin

United States

Harmonized Tariff Schedule Code

7318160000

Lead Time (Days)

187

Shelf Life

No

Forecasted

Yes

Dimensions (L x W x H)

3 x 2 x 0.57 Inch

Package Weight

0.02 LB

Shipping Details

Hazmat Code

ZND

ECCN

EAR99

Schedule B

7318160000

8130-3 Eligible

Yes

Hazmat

No

Part Explosive

No

Item Replacement History

Buy now from
Boeing Distribution (formerly Aviall)
Product information provided "as is", and Boeing may add, change, discontinue or remove product information at any time. Product photos may not be exact match to product delivered. See terms & conditions.