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1560-01-373-9940
Aircraft Structural Component Web
1560013739940 013739940 114S3404-49
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
January 2023
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United States (US) 4. 1560-01-373-9940 Marketplace Restrictions Approved Sources Datasheet Management
WEB,STRUCTURAL COMPONENT,AIRCRAFT 1 EA NS Request Quotation Updated Every Day 1560-01-373-9940 RQST
Restrictions 1560-01-373-9940
1560-01-373-9940 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. The precious metals content of this item is unknown.
Import and Export 1560-01-373-9940
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-373-9940
- United Kingdom (ZK01)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-01-373-9940
- Part Number
- Manufacturer
- Status
- 114S3404-49
- Manufacturer
- 77272 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-373-9940
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Supplementary Features [SUPP]
- Cognizant User Service Royal United Kingdom Air Force
- End Item Identification [AGAV]
- Chinook Mk Ii
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Freight Information 1560-01-373-9940
1560-01-373-9940 has freight characteristics managed by the United Kingdom (UK).. 1560-01-373-9940 has a variance between NMFC and UFC when transported by rail and the description should be consulted.