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5325-01-357-4723

Panel Fastener Insert

5325013574723 013574723 NAS1836C06-21M

An insert which must have a hole that may be internally threaded with a flange on one end. It may have an undercut on the end opposite the flange to provide a shoulder to allow for mating with another insert. Pre-assembled items will consist of an expansion sleeve and a body which may be flared. Internally threaded items may have a self-locking feature. Excludes INSERT, SCREW THREAD. View more Panel Fastener Insert

5325-01-357-4723 INSERT,PANEL FASTENER 5325013574723 013574723

Managed by United States
NSN Created on 24 Apr 1992
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
CWXS Style 15 for 5325-01-357-4723 1/1
NSN 5325-01-357-4723 (Identification) 1/1

5325-01-357-4723 Stock and Availability Marketplace 5325-01-357-4723

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NAS1836C06-21M An insert which must have a hole that may be internally threaded with a flange on one
United States (US) 4. 5325-01-357-4723 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 5325-01-357-4723 RQST Updated Every Day 5325-01-357-4723 RQST NE Related Documents
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5325-01-357-4723 Demil Restrictions 5325-01-357-4723

DEMIL: A | DEMILI: 1 | CRITICALITY: N | HMIC: N | PMIC: A | EDC: | ADPEC: 0

5325-01-357-4723 is a Panel Fastener Insert Demilitarization of this item has been confirmed and is not currently subject to changes. 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.

5325-01-357-4723 HTS and ScheduleB Import and Export 5325-01-357-4723

5325-01-357-4723 End Users End Users 5325-01-357-4723

US Air Force (FBB5)
Effective Date:
1 Nov 2004
Former MOE Rule:
FXKZ

5325-01-357-4723 Manufacturers Approved Sources 5325-01-357-4723

5325-01-357-4723 Technical Data Datasheet 5325-01-357-4723

Characteristic
Specifications
FIIG
A05400
Features Provided [CBBL]
Potting Hole Or Potting Slot
Flange Diameter [ABKK]
0.441 Inches Minimum And 0.451 Inches Maximum
Flange Thickness [CWTF]
0.060 Inches Nominal
Hole Type [BQDM]
Threaded
Material [MATT]
Steel Comp 303 Overall
Insert Style [CWXS]
Protruding Flange
Material Accommodated Thickness [AGSM]
0.452 Inches Minimum And 0.457 Inches Maximum
Material Document And Classification [MDCL]
Astm A582 Assn Std Single Material Response Overall
Sleeve Diameter [AJSE]
0.260 Inches Nominal
Special Features [FEAT]
0.651 In. Long; Dry Film Lubricant Apply On Inside Of Insert Only
Thread Size And Series/Type Designator [THDS]
0.138-32 Unjc
Specification/Standard Data [ZZZK]
80205-Nas1836 Professional/Industrial Association Standard
Surface Treatment Document And Classification [STDC]
Qq-P-35 Fed Spec Single Treatment Response Overall
Surface Treatment [SFTT]
Passivate Overall

5325-01-357-4723 Management Data Management Data 5325-01-357-4723

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Nov 2018
Department of the Air Force (DF)
EA
Subscribe

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
N
The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of ā€œLā€ or ā€œFā€, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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5325-01-357-4723 Freight Data Freight Information 5325-01-357-4723

5325-01-357-4723 has freight characteristics.. 5325-01-357-4723 has a variance between NMFC and UFC when transported by rail and the description should be consulted.