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5306-01-518-8705

Internal Wrenching Bolt

5306015188705 015188705 CA21387-6-9TX

An externally threaded fastener whose threaded portion is of one nominal diameter, No. 10 (0.190 IN.) (5 mm) or larger. It is designed with an internal socket or internal multiple spline for use with an internal driver. The head is beveled (conical) or cylindrical in shape. Items with cylindrical shaped heads must have an externally relieved body. A locking feature may be incorporated in the design of the head or threads. See also SCREW, CAP, SOCKET HEAD. Excludes SETSCREW; SCREW, SHOULDER; BOLT, SHOULDER; SCREW, EXTERNALLY RELIEVED BODY; BOLT, EXTERNALLY RELIEVED BODY; and SCREW, MACHINE. View more Internal Wrenching Bolt

5306-01-518-8705 BOLT,INTERNAL WRENCHING 5306015188705 015188705

Managed by United States
NSN Created on 26 Mar 2004
Data Last Changed
May 2023
NATO Update Count
3
NATO Data Quality
5306-01-518-8705 BOLT,INTERNAL WRENCHING 5306015188705 015188705 1/1
NSN 5306-01-518-8705 (Generic Image) 1/1

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CA21387-6-9TX An externally threaded fastener whose threaded portion is of one nominal diameter, No.
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5306-01-518-8705 Demil Restrictions 5306-01-518-8705

DEMIL: A | DEMILI: 7 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

5306-01-518-8705 is a Internal Wrenching Bolt that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

5306-01-518-8705 End Users End Users 5306-01-518-8705

US Air Force (FLL5)
Effective Date:
1 Mar 2004

5306-01-518-8705 Manufacturers Approved Sources 5306-01-518-8705

5306-01-518-8705 Technical Data Datasheet 5306-01-518-8705

Characteristic
Specifications
FIIG
A003B0
End Item Identification [AGAV]
F-22 Raptor
Part Name Assigned By Controlling Agency [CXCY]
Bolt,Internal Wrenching

5306-01-518-8705 Management Data Management Data 5306-01-518-8705

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Nov 2022
Department of the Air Force (DF)
EA
Subscribe
1
Dec 2011
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
FR
F-22 AIRCRAFT
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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5306-01-518-8705 Freight Data Freight Information 5306-01-518-8705

5306-01-518-8705 has freight characteristics.. 5306-01-518-8705 has a variance between NMFC and UFC when transported by rail and the description should be consulted.