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1560-01-150-7372
Aircraft Structural Component Support
1560011507372 011507372 39-8227-2
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
January 2023
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United States (US) 4. 1560-01-150-7372 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-150-7372
1560-01-150-7372 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 1560-01-150-7372
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-150-7372
- US Air Force (FXX5)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-01-150-7372
- Part Number
- Manufacturer
- Status
- 39-8227-2
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-150-7372
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Aircraft Mission Design Series [CZEK]
- B-52
- Material Document And Classification [MDCL]
- Qq-A-362 Fed Spec Single Material Response
- Material Thickness [ABPX]
- 0.090 Inches Nominal
- Material [MATT]
- Aluminum Alloy 2024
- Side For Which Designed [BWJF]
- Right Side
- Overall Length [ABHP]
- 2.500 Inches Nominal
- Overall Width [ABMK]
- 2.400 Inches Nominal
Management Data 1560-01-150-7372
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Jan 2015
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 1560-01-150-7372
1560-01-150-7372 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 106280. A Sub NMFC of X. It has a NMFC Description of PLATES STRUCTURAL I/S NOI. 1560-01-150-7372 is rated as class 50 when transported by Less-Than Truckload (LTL) freight. 1560-01-150-7372 is rated as class 50 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 54650 which rates the freight between FCL and LCL. 1560-01-150-7372 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 671 for ocean manifesting and military sealift. 1560-01-150-7372 is not classified as a special type of cargo when transported by water. 1560-01-150-7372 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.