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5340-01-488-4342

Aircraft Structural Component Bracket

5340014884342 014884342 5HM40055-185

A ridge item, usually of flat material, formed into a dihedral angle (generally a right angle) which may be reinforced; it is designed to position, align, or support an item(s) in relation to another. Excludes BRACE (as modified); BRACKET (1), MOUNTING; and BRACKET, SHELF. View more Angle Bracket

5340-01-488-4342 BRACKET,STRUCTURAL COMPONENT,AIRCRAFT 5340014884342 014884342

Managed by United States
NSN Created on 24 Aug 2001
Data Last Changed
May 2023
NATO Update Count
2
NATO Data Quality
STYL Style 6 for 5340-01-488-4342 1/1
NSN 5340-01-488-4342 (Identification) 1/1

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5340-01-488-4342 Demil Restrictions 5340-01-488-4342

DEMIL: B | DEMILI: 3 | CRITICALITY: X | HMIC: P | PMIC: A | EDC: A | ADPEC: 0

5340-01-488-4342 is a Aircraft Structural Component Bracket that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a US Munitions List Item and must be mutilated to scrap. This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.

5340-01-488-4342 HTS and ScheduleB Import and Export 5340-01-488-4342

5340-01-488-4342 End Users End Users 5340-01-488-4342

US Air Force (FLL5)
Effective Date:
1 Aug 2001

5340-01-488-4342 Manufacturers Approved Sources 5340-01-488-4342

5340-01-488-4342 Technical Data Datasheet 5340-01-488-4342

Characteristic
Specifications
FIIG
A042A0
End Item Identification [AGAV]
F/A-22 Raptor
First Leg Angle [CSSQ]
90.0 Degrees Nominal
First Leg Thickness [AHPW]
0.071 Inches Nominal
First Leg Length [ADLK]
1.890 Inches Nominal
Material Document And Classification [MDCL]
Qq-A-250/4 Fed Spec Single Material Response
Material [MATT]
Aluminum Alloy 2024
Mounting Hole Type [ACHY]
Plain
Second Leg Length [ADLL]
3.010 Inches Nominal
Second Leg Thickness [AHPX]
0.071 Inches Nominal
Part Name Assigned By Controlling Agency [CXCY]
Bracket-Details, Harness Support
Special Features [FEAT]
Name Submitted For Catalaging-Bracket;1St Halo Has Hole W/Dia 0.204 To 0.212;From Edge To Hole Cntr Of 1St Leg Along Both Length/Width 0.380;2Nd Leg Has Opening Surrounded By 3 Holes W/Dia Of 0.221 To 0.228;Cntr To Cntr Dist Of 2 Of Tyhe Holes On 2Nd Leg Along Length Is 2.250;From Edge To Hole Cntr Of 2Nd Leg Along Both Length/Width Is 0.380
Style Designator [STYL]
Angle

5340-01-488-4342 Management Data Management Data 5340-01-488-4342

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Nov 2022
Department of the Air Force (DF)
EA
Subscribe
1
May 2018
Department of the Air Force (DF)
EA
Subscribe
1

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5340-01-488-4342 Freight Data Freight Information 5340-01-488-4342

5340-01-488-4342 has freight characteristics.. 5340-01-488-4342 has a variance between NMFC and UFC when transported by rail and the description should be consulted.