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5306-01-484-8319

Machine Bolt

5306014848319 014848319 ST1315-07

An externally threaded fastener designed for insertion through holes in assembled parts and normally intended to be tightened or released by torquing a nut. The threaded and unthreaded portions are both of one nominal diameter of 0.190 inch (5 mm) or larger. The head is not designed to be held or driven with an inserted driver or by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads. Head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. For items having a grip length portion machined to a tolerance of 0.0015 inch (0.038 mm) or less, BOLT, SHEAR. See also SCREW, CAP, HEXAGON HEAD and SCREW, MACHINE. View more Machine Bolt

5306-01-484-8319 BOLT,MACHINE 5306014848319 014848319

Managed by United States
NSN Created on 9 May 2001
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
5306-01-484-8319 BOLT,MACHINE 5306014848319 014848319 1/1
NSN 5306-01-484-8319 (Generic Image) 1/1

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ST1315-07 An externally threaded fastener designed for insertion through holes in assembled parts and
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5306-01-484-8319 Demil Restrictions 5306-01-484-8319

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

5306-01-484-8319 is a Machine 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.

5306-01-484-8319 HTS and ScheduleB Import and Export 5306-01-484-8319

5306-01-484-8319 End Users End Users 5306-01-484-8319

Federal Bureau of Investigation (FDD5)
Effective Date:
1 May 2001

5306-01-484-8319 Manufacturers Approved Sources 5306-01-484-8319

5306-01-484-8319 Technical Data Datasheet 5306-01-484-8319

Characteristic
Specifications
FIIG
A003B0
Nominal Thread Diameter [AHYM]
0.250 Inches
Thread Quantity Per Inch [CMLP]
28
Material [MATT]
Nickel Alloy Overall
Special Features [FEAT]
Overall Length 0.552-0.572; Unthreaded Length 0.074-0.099
End Item Identification [AGAV]
F119-Pw-100 Engine Onf-22 Aircraft

5306-01-484-8319 Management Data Management Data 5306-01-484-8319

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Jan 2014
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
RF
F-119-PW-100 FOR ATF-ENGINE
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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5306-01-484-8319 Freight Data Freight Information 5306-01-484-8319

5306-01-484-8319 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 093486. A Sub NMFC of Z. It has a NMFC Description of BOLTS,NUTS OR SCREWS, NOI (SUB 3). 5306-01-484-8319 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 48950 which rates the freight between FCL and LCL. 5306-01-484-8319 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 573 for ocean manifesting and military sealift. 5306-01-484-8319 is not classified as a special type of cargo when transported by water. 5306-01-484-8319 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.