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1560-01-488-1386
Aircraft Structural Plate
1560014881386 014881386 5HB45333-105
A flat or preformed item of metallic or nonmetallic material. It may vary in shape and its surface may be smooth and/or serrated. Its thickness is small in comparison to both its length and width. It is designed to be mounted upon a surface or between two surfaces. Its primary function is to strengthen, join, or separate aircraft structural parts. Excludes PLATE, MENDING; SHIM; and SPACER, PLATE. View more Aircraft Structural Plate
January 2023
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Related Documents 1560-01-488-1386 2+ Documents (More...)
United States (US) 4. 1560-01-488-1386 Marketplace Restrictions Approved Sources Datasheet Management
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Aircraft Structural Plate 1560014881386 Plate,Mounting-External Power ReceptacleSpecial Features
Restrictions 1560-01-488-1386
1560-01-488-1386 is a Aircraft Structural Plate that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. 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 1560-01-488-1386
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-488-1386
- US Air Force (FLL5)
- Effective Date:
- 1 Aug 2001
Approved Sources 1560-01-488-1386
- Part Number
- Manufacturer
- Status
- 5HB45333-105
- Manufacturer
- 81755 - Lockheed Martin Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-488-1386
- Characteristic
- Specifications
- FIIG
- Specifications
- A11400
- End Item Identification [AGAV]
- F/A-22 Raptor
- Aircraft Mission Design Series [CZEK]
- F/A-22 Raptor
- Material Document And Classification [MDCL]
- Qq-A-250/11 Assn Std All Material Responses
- Material Thickness [ABPX]
- 0.125 Inches Nominal
- Material [MATT]
- Aluminum Alloy
- Overall Length [ABHP]
- 10.000 Inches Nominal
- Overall Width [ABMK]
- 7.000 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Plate,Mounting-External Power Receptacle
- Special Features [FEAT]
- Consists Of 1 5Hb45333-103 Plate; 1 R22-C10t12 Stud
Management Data 1560-01-488-1386
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Sep 2018
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- MOE
- USC
- Code
- Statement
- Order of Use
- Jump To Code
- Qty Per Assy
- UOM
- Technical Document
- Quantative Expression
- Code
- Department of the Air Force (DF)
- I
- V
- Discontinued Without Replacement
- V
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Freight Information 1560-01-488-1386
1560-01-488-1386 has freight characteristics.. 1560-01-488-1386 has a variance between NMFC and UFC when transported by rail and the description should be consulted.