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5307-01-567-2212

Locked In Stud

5307015672212 015672212 23053385-201-9

A headless fastener externally threaded on both ends with each threaded portion of one but not necessarily the same nominal diameter. It is designed to be locked in place by either a RING, LOCK, SERRATED or a RING, LOCK, KEYED. View more Locked In Stud

5307-01-567-2212 STUD,LOCKED IN 5307015672212 015672212

Managed by United States
NSN Created on 20 Sep 2008
Data Last Changed
January 2023
NATO Update Count
6
NATO Data Quality
5307-01-567-2212 STUD,LOCKED IN 5307015672212 015672212 1/1
NSN 5307-01-567-2212 (Generic Image) 1/1

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5307-01-567-2212 Related Documents Related Documents 5307-01-567-2212 2+ Documents (More...)

STUD,LOCKED IN 99 EA NS Request Quotation Updated Every Day 5307-01-567-2212 RQST NE Updated Every
Day 5307-01-567-2212 RQST Updated Every Day 5307-01-567-2212 RQST NE Related Documents 5307-01-567-2212
RQST NE Updated Every Day 5307-01-567-2212 RQST Updated Every Day 5307-01-567-2212 RQST NE Related Documents
a day Upgrade your Account Upgrade 5307-01-463-8704Airc Locked In Stud5307014638704 014638704 23053385-201-9
MS51833A201-9 STUD,LOCKED IN,AIRC 99 EA NS Request Quotation 23053385-201-9 STUD,LOCKED IN,AIRC 99 EA
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5307-01-567-2212 Demil Restrictions 5307-01-567-2212

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

5307-01-567-2212 is a Locked In Stud 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.

5307-01-567-2212 End Users End Users 5307-01-567-2212

US Air Force (FII5)
Effective Date:
1 Sep 2008
Canada (ZC01)
Effective Date:
1 Mar 2015
Norway (ZT01)
Effective Date:
1 Jul 2013

5307-01-567-2212 Manufacturers Approved Sources 5307-01-567-2212

5307-01-567-2212 Technical Data Datasheet 5307-01-567-2212

Characteristic
Specifications
FIIG
A051A0
End Item Identification [AGAV]
C-130J Aircraft Rolls-Royce Jet Engine
Part Name Assigned By Controlling Agency [CXCY]
Stud,Locked In Key

5307-01-567-2212 Management Data Management Data 5307-01-567-2212

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Jun 2019
Department of the Air Force (DF)
EA
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1

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5307-01-567-2212 Freight Data Freight Information 5307-01-567-2212

5307-01-567-2212 has freight characteristics.. 5307-01-567-2212 has a variance between NMFC and UFC when transported by rail and the description should be consulted.