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1560-01-061-1001
Aircraft Structural Component Web
1560010611001 010611001 53-11028-17
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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RQST NE Updated Every Day 1560-01-061-1001 RQST Updated Every Day 1560-01-061-1001 RQST NE Restrictions
1560-01-061-1001 DEMIL: B | DEMILI : | CRITICALITY : X | HMIC : P | PMIC : A | EDC: | ADPEC : 0 1560
Restrictions 1560-01-061-1001
1560-01-061-1001 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 1560-01-061-1001
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-061-1001
- Turkey (ZW01)
- Effective Date:
- 1 Dec 1995
Approved Sources 1560-01-061-1001
- Part Number
- Manufacturer
- Status
- 53-11028-17
- Manufacturer
- 76301 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-061-1001
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Aircraft Mission Design Series [CZEK]
- F-4
- Material Document And Classification [MDCL]
- Qq-A-250 Fed Spec Single Material Response
- Material Thickness [ABPX]
- 0.063 Inches Nominal
- Overall Length [ABHP]
- 11.700 Inches Nominal
- Overall Width [ABMK]
- 9.150 Inches Nominal
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Freight Information 1560-01-061-1001
1560-01-061-1001 has freight characteristics.. 1560-01-061-1001 has a variance between NMFC and UFC when transported by rail and the description should be consulted.