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1560-01-357-6540
Aircraft Structural Component Support
1560013576540 013576540 68A620040-2002
A device of various shapes to be permanently attached to the structure of an aircraft. It is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. It may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. Excludes items which are primarily designed for dampening shock and/or vibration. Excludes BRACKET, ANGLE; BRACKET, DOUBLE ANGLE; BRACKET, SHELF; BRACKET, MOUNTING; BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT; and RADIUS BLOCK. View more Aircraft Structural Component Support
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January 2023
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United States (US) 4. 1560-01-357-6540 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-357-6540
1560-01-357-6540 is a Aircraft Structural Component Support 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.
Import and Export 1560-01-357-6540
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-357-6540
- US Air Force (FGG5)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-01-357-6540
- Part Number
- Manufacturer
- Status
- 68A620040-2002
- Manufacturer
- 76301 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-357-6540
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Aircraft Mission Design Series [CZEK]
- F-15A/B
- Aircraft Location [CZDJ]
- Support-Bell Crank Aileron
- Aircraft Station Number [CZEJ]
- Xw63.864,Yw234.388
- Height [HGTH]
- 2.942 Inches Nominal
- Material [MATT]
- Aluminum Alloy 7075
- Overall Length [ABHP]
- 7.910 Inches Nominal
- Overall Width [ABMK]
- 6.210 Inches Nominal
Management Data 1560-01-357-6540
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Freight Information 1560-01-357-6540
1560-01-357-6540 has freight characteristics managed by the General Services Administration (GSA).It has a National Motor Freight Classification (NMFC) of 013120. A Sub NMFC of J. It has a NMFC Description of ALUMINUM ARTICLE NOI SUB 9. 1560-01-357-6540 is rated as class 70 when transported by Less-Than Truckload (LTL) freight. 1560-01-357-6540 is rated as class 77.5 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 05380 which rates the freight between FCL and LCL. It has a Water Commodity Code (WCC) of 732 for ocean manifesting and military sealift. 1560-01-357-6540 is not classified as a special type of cargo when transported by water. 1560-01-357-6540 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.
Packaging Data 1560-01-357-6540
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- Packaging Data does not meet current MIL-STD-2073-1E
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- --
- --
- --
- --
- --
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- 1
- --
- --
- --
- Physical Protection
- Any Suitable Process
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- No Requirement
- No Requirement
- No Requirement
- Not Applicable
- Bags made of material conforming to MIL-P-130, MIL-DTL-17667, MIL-PRF-121, or any material authorized by MIL-DTL-117. Closure may be by staples, tape, adhesive or heat seal
- No special marking
- No Requirement
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --