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1560-01-378-9752
Aircraft Structural Component Web
1560013789752 013789752 114S2312-11
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
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January 2023
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Related Documents 1560-01-378-9752 1+ Documents (More...)
United States (US) 4. 1560-01-378-9752 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-378-9752 RQST Updated Every Day 1560-01-378-9752 RQST NE Restrictions
Restrictions 1560-01-378-9752
1560-01-378-9752 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.
Import and Export 1560-01-378-9752
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-378-9752
- United Kingdom (ZK01)
- Effective Date:
- 1 Aug 1993
Approved Sources 1560-01-378-9752
- Part Number
- Manufacturer
- Status
- 114S2312-11
- Manufacturer
- 77272 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-378-9752
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Special Features [FEAT]
- Used On A Chinook Helicopter
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Freight Information 1560-01-378-9752
1560-01-378-9752 has freight characteristics.. 1560-01-378-9752 has a variance between NMFC and UFC when transported by rail and the description should be consulted.