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1560-01-151-9458

Aircraft Structural Component Web

1560011519458 011519458 25-2605-808

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

1560-01-151-9458 WEB,STRUCTURAL COMPONENT,AIRCRAFT 1560011519458 011519458

Managed by United States
NSN Created on 25 Apr 1983
Data Last Changed
January 2023
NATO Update Count
6
NATO Data Quality
1560-01-151-9458 WEB,STRUCTURAL COMPONENT,AIRCRAFT 1560011519458 011519458 1/1
NSN 1560-01-151-9458 (Generic Image) 1/1

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1560-01-151-9458 Related Documents Related Documents 1560-01-151-9458 1+ Documents (More...)

25-2605-808 An item designed as a principal member of various primary structures within an aircraft.
United States (US) 4. 1560-01-151-9458 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-151-9458 Demil Restrictions 1560-01-151-9458

DEMIL: D | DEMILI: 1 | CRITICALITY: X | HMIC: P | PMIC: A | EDC: | ADPEC:

1560-01-151-9458 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. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. 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.

1560-01-151-9458 HTS and ScheduleB Import and Export 1560-01-151-9458

1560-01-151-9458 End Users End Users 1560-01-151-9458

US Air Force (FXX5)
Effective Date:
1 Apr 1991

1560-01-151-9458 Manufacturers Approved Sources 1560-01-151-9458

1560-01-151-9458 Technical Data Datasheet 1560-01-151-9458

Characteristic
Specifications
FIIG
A11800
Aircraft Mission Design Series [CZEK]
B-52
Aircraft Location [CZDJ]
Torque Bulkhead,Inboard Strut
Material Document And Classification [MDCL]
Qq-A-287 Fed Spec Single Material Response
Material Thickness [ABPX]
0.063 Inches Nominal
Material [MATT]
Aluminum Alloy 7075
Overall Length [ABHP]
23.300 Inches Nominal
Overall Width [ABMK]
17.700 Inches Nominal

1560-01-151-9458 Management Data Management Data 1560-01-151-9458

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Feb 2015
Department of the Air Force (DF)
EA
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1

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1560-01-151-9458 Freight Data Freight Information 1560-01-151-9458

1560-01-151-9458 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 011760. A Sub NMFC of X. It has a NMFC Description of AIRCRAFT/AIRCRAFT PART VIZ:. 1560-01-151-9458 is rated as class 200 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 04705 which rates the freight between FCL and LCL. 1560-01-151-9458 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 594 for ocean manifesting and military sealift. 1560-01-151-9458 is not classified as a special type of cargo when transported by water. 1560-01-151-9458 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.