5306-21-079-2430
Internally Relieved Body Bolt
5306210792430 210792430 231413
An externally threaded fastener whose external threaded portion is of one nominal diameter. It has a concentric hole along the longitudinal centerline which may extend a part or the full length of the bolt. The concentric hole along the centerline may be counterbored and/or internally threaded at the head end or the bolt end. The head is designed to be held or driven by an external and/or internal driver. For items having a hole(s) perpendicular to the axis which meet the concentric hole along the longitudinal centerline, see BOLT, FLUID PASSAGE. View more Internally Relieved Body Bolt
Managed by Canada
NSN Created on 12 Nov 1970
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 5306-21-079-2430
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how to enable JavaScript in your web browser . 4730-14-362-5538Tube Elbow4730143625538 143625538 231413
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7204 2+ Documents ( More... ) https//www.nsnlookup.com /cage Honeywell Ltd (CAGE Code 09706) 5306-21-079-2430
RNVC: 2 | DAC: 6 26 Mar 1965 6605-21-001-7184 Pin 316367RNCC: 3 | RNVC: 2 | DAC: 5 30 Nov 1965 5306-21-079-2430
1560-01-094-2379 1560010942379 010942379 is a principal spanwise member of the structural framework of a wing, stabilizer, other airfoil, and the like. it is designed to absorb bending loads applied to the airfoil.
for $1 a day Upgrade your Account Upgrade 5310-00-113-1625Plate Plain Nut5310001131625 001131625 231413
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Restrictions 5306-21-079-2430
End Users 5306-21-079-2430
- Canada (ZC)
Approved Sources 5306-21-079-2430
- Part Number
- Manufacturer
- Status
- 231413
- Manufacturer
- 09706 - Honeywell Ltd (Active)
- Primary Buy
- Primary Buy
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