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1560-01-048-1775
Aircraft Structural Component Support
1560010481775 010481775 66-2448-3
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 1560-01-048-1775 1+ Documents (More...)
United States (US) 4. 1560-01-048-1775 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-048-1775 RQST Updated Every Day 1560-01-048-1775 RQST NE Restrictions
Restrictions 1560-01-048-1775
1560-01-048-1775 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 has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). 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. The precious metals content of this item is unknown.
Import and Export 1560-01-048-1775
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-048-1775
- US Air Force (FXX5)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-01-048-1775
- Part Number
- Manufacturer
- Status
- 66-2448-3
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-048-1775
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Aircraft Mission Design Series [CZEK]
- Kc-135
- Material Document And Classification [MDCL]
- Qq-A-362 Fed Spec Single Material Response
- Material [MATT]
- Aluminum Alloy 2024
- Overall Length [ABHP]
- 1.200 Inches Nominal
- Overall Width [ABMK]
- 0.090 Inches Nominal
Management Data 1560-01-048-1775
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Freight Information 1560-01-048-1775
1560-01-048-1775 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 013140. A Sub NMFC of X. It has a NMFC Description of ALUMINUM ANGLES. 1560-01-048-1775 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 05390 which rates the freight between FCL and LCL. 1560-01-048-1775 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 594 for ocean manifesting and military sealift. 1560-01-048-1775 is not classified as a special type of cargo when transported by water. 1560-01-048-1775 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.