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1560-01-355-1103

Aircraft Structural Component Web

1560013551103 013551103 68A325122-2160

An item designed as a principal member of various primary structures within an aircraft. It provides strength, rigidity and the like while maintaining the proper dimensional distances as required. It may include holes for mounting and/or joining to other items to form an assembly. View more Aircraft Structural Component Web

1560-01-355-1103 WEB,STRUCTURAL COMPONENT,AIRCRAFT 1560013551103 013551103

Managed by United States
NSN Created on 11 Mar 1992
Data Last Changed
January 2023
NATO Update Count
5
NATO Data Quality
1560-01-355-1103 WEB,STRUCTURAL COMPONENT,AIRCRAFT 1560013551103 013551103 1/1
NSN 1560-01-355-1103 (Generic Image) 1/1

1560-01-355-1103 Stock and Availability Marketplace 1560-01-355-1103

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1560-01-355-1103 Related Documents Related Documents 1560-01-355-1103 1+ Documents (More...)

68A325122-2160 An item designed as a principal member of various primary structures within an aircraft
United States (US) 4. 1560-01-355-1103 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-355-1103 RQST Updated Every Day 1560-01-355-1103 RQST NE Restrictions

1560-01-355-1103 Demil Restrictions 1560-01-355-1103

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

1560-01-355-1103 is a Aircraft Structural Component Web that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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.

1560-01-355-1103 HTS and ScheduleB Import and Export 1560-01-355-1103

1560-01-355-1103 End Users End Users 1560-01-355-1103

US Air Force (FGG5)
Effective Date:
1 Apr 1991

1560-01-355-1103 Manufacturers Approved Sources 1560-01-355-1103

1560-01-355-1103 Technical Data Datasheet 1560-01-355-1103

Characteristic
Specifications
FIIG
A11800
Aircraft Mission Design Series [CZEK]
F-15A/B/C/D/E
Aircraft Location [CZDJ]
Support,Main Landing Gear,Twist Link And Door Sill
Material Document And Classification [MDCL]
Qq-A-250/5,T62 Fed Spec Single Material Response
Material [MATT]
Aluminum Alloy 2024

1560-01-355-1103 Management Data Management Data 1560-01-355-1103

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Jan 2019
Department of the Air Force (DF)
EA
Subscribe
1
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Air Force (DF)
I
V
Discontinued Without Replacement

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1560-01-355-1103 Freight Data Freight Information 1560-01-355-1103

1560-01-355-1103 has freight characteristics managed by the General Services Administration (GSA).It has a National Motor Freight Classification (NMFC) of 011790. A Sub NMFC of B. It has a NMFC Description of AIRCRAFT PARTS NOI SUB2. 1560-01-355-1103 is rated as class 150 when transported by Less-Than Truckload (LTL) freight. 1560-01-355-1103 is rated as class 200 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 04720 which rates the freight between FCL and LCL. 1560-01-355-1103 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 671 for ocean manifesting and military sealift. 1560-01-355-1103 is not classified as a special type of cargo when transported by water. 1560-01-355-1103 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.