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1560-01-157-0141
Aircraft Structural Component Support
1560011570141 011570141 25-2682-1
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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Related Documents 1560-01-157-0141 1+ Documents (More...)
United States (US) 4. 1560-01-157-0141 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-157-0141 RQST Updated Every Day 1560-01-157-0141 RQST NE Restrictions
Restrictions 1560-01-157-0141
1560-01-157-0141 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. 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 1560-01-157-0141
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-157-0141
- US Air Force (FXX5)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-01-157-0141
- Part Number
- Manufacturer
- Status
- 25-2682-1
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-157-0141
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Aircraft Location [CZDJ]
- Center Side,Rib No.5,Outboard Strut
- Aircraft Mission Design Series [CZEK]
- B-52
- Material Document And Classification [MDCL]
- Qq-A-367 Fed Spec Single Material Response
- Material [MATT]
- Aluminum Alloy 2014
- Side For Which Designed [BWJF]
- Left Side
Management Data 1560-01-157-0141
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Freight Information 1560-01-157-0141
1560-01-157-0141 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. 1560-01-157-0141 is rated as class 50 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 54650 which rates the freight between FCL and LCL. 1560-01-157-0141 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 732 for ocean manifesting and military sealift. 1560-01-157-0141 is not classified as a special type of cargo when transported by water. 1560-01-157-0141 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.