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1560-01-152-6586
Aircraft Stringer
1560011526586 011526586 35-10703-520
An auxiliary longitudinal member of the structural framework of a fuselage, nacelle, empennage, wing, and the like. It is designed to stiffen and/or support the skin by attachment of bulkheads, formers, frames, ribs, and the like. View more Aircraft Stringer
January 2023
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Restrictions 1560-01-152-6586
1560-01-152-6586 is a Aircraft Stringer 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 1560-01-152-6586
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-152-6586
- US Air Force (FXX5)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-01-152-6586
- Part Number
- Manufacturer
- Status
- 35-10703-520
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-152-6586
- Characteristic
- Specifications
- FIIG
- Specifications
- A11400
- Aircraft Location [CZDJ]
- Panel-Engine Wrap Cowl, Upper, Assy
- Aircraft Mission Design Series [CZEK]
- B-52
- Material Document And Classification [MDCL]
- Qq-A-287 Fed Spec Single Material Response
- Material Thickness [ABPX]
- 0.040 Inches Nominal
- Material [MATT]
- Aluminum Alloy 7075
- Overall Length [ABHP]
- 39.000 Inches Nominal
- Overall Width [ABMK]
- 3.200 Inches Nominal
- Special Features [FEAT]
- Matt: Clad Sht; 0 Temper; Ht T6; Opp -519
Management Data 1560-01-152-6586
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Freight Information 1560-01-152-6586
1560-01-152-6586 has freight characteristics.. 1560-01-152-6586 has a variance between NMFC and UFC when transported by rail and the description should be consulted.