5306-22-269-2138

Machine Bolt

5306222692138 222692138 680412 10213-00 IT 067 PL010421 99 02 IT 067

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

5306-22-269-2138 BOLT,MACHINE 5306222692138 222692138

Managed by Denmark
NSN Created on 18 Dec 1996
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
5306-22-269-2138 BOLT,MACHINE 5306222692138 222692138 1/1
NSN 5306-22-269-2138 (Generic Image) 1/1

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5306-22-269-2138 Related Documents Related Documents 5306-22-269-2138 5+ Documents (More...)

99 02 IT 054RNCC: 5 | RNVC: 2 | DAC: 410213-00 IT 054RNCC: 5 | RNVC: 2 | DAC: 4 31 Oct 1996 5306-22-269-2138
JavaScript in your web browser . 5998-00-938-4402Electronic Components Assembly5998009384402 009384402 680412
Upgrade your Account Upgrade 4320-01-511-5176Spring Loaded Shaft Seal Assembly4320015115176 015115176 680412
Upgrade your Account Upgrade 4320-01-511-5176Spring Loaded Shaft Seal Assembly4320015115176 015115176 680412
1560-01-193-8850 1560011938850 011938850 is a device of various shapes to be permanently attached to the structure of an aircraft. it is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. it may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. excludes items which are primarily designed for dampening shock and/or vibration. excludes bracket, angle; bracket, double angle; bracket, shelf; bracket, mounting; bracket (1), structural component, aircraft; and radius block.

5306-22-269-2138 Demil Restrictions 5306-22-269-2138

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

5306-22-269-2138 is a Machine Bolt

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United States of America (ZZ)

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5306-22-269-2138 Contracting Technical Data File (CTDF) Contracting Technical Data File (CTDF) 5306-22-269-2138 February 2021

Criticality and Quality

Critical Item Code:
Flight Safety:
Life Support:
Certified Samples:
Serialization:
First Article Test (FAT):
Certificate of Quality Compliance:
Production Lot Testing:
Special Testing:
Qualified Products List (QPL):

Commercial Properties

Government Furnished Material:
Government Furnished Tooling:
Government Furnished Property:
Price Evaluation Code:
Diminshing Manufacturing Sources:
Warranty:
Commerical Off The Shelf (COTS):
End Item Application:
Auctioning Candidate:
Source of Procurement:
Contract Option:

Restrictions

Boeing Rights Guard:
Export Controlled:
Controlled Technical Data Package (TDP):
Restricted Technical Data Package (TDP):
Contains Classified Material
Weapons System Indicator Code (WSIC):
L

Packaging Requirements

Packaging Determination Table:
Packaging Review Code:
Special Packaging Instruction Number (SPIN):
Special Packaging Instruction Number Revision:
Special Packaging Instruction Number Date:
Pallet Reference Number Required: