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1560-01-432-0357

Aircraft Structural Plate

1560014320357 014320357 68A230609-2003

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

1560-01-432-0357 PLATE,STRUCTURAL,AIRCRAFT 1560014320357 014320357

Managed by United States
NSN Created on 23 May 1996
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
1560-01-432-0357 PLATE,STRUCTURAL,AIRCRAFT 1560014320357 014320357 1/1
NSN 1560-01-432-0357 (Generic Image) 1/1

1560-01-432-0357 Stock and Availability Marketplace 1560-01-432-0357

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1560-01-432-0357 Related Documents Related Documents 1560-01-432-0357 1+ Documents (More...)

68A230609-2003 A flat or preformed item of metallic or nonmetallic material.
United States (US) 4. 1560-01-432-0357 Marketplace Restrictions Approved Sources Datasheet Management
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1560-01-432-0357 Demil Restrictions 1560-01-432-0357

DEMIL: B | DEMILI: | CRITICALITY: X | HMIC: P | PMIC: A | EDC: | ADPEC: 0

1560-01-432-0357 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. 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.

1560-01-432-0357 HTS and ScheduleB Import and Export 1560-01-432-0357

1560-01-432-0357 End Users End Users 1560-01-432-0357

US Air Force (FGG4)
Effective Date:
1 May 1996

1560-01-432-0357 Manufacturers Approved Sources 1560-01-432-0357

1560-01-432-0357 Technical Data Datasheet 1560-01-432-0357

Characteristic
Specifications
FIIG
A11400
Aircraft Mission Design Series [CZEK]
F-15
Aircraft Location [CZDJ]
Skin Assembly,Upper,Leading Edge,Vertical Stabilizer,Hf Antenna
Material Document And Classification [MDCL]
Mil-T-9046,Type 3,Composition C,Annealed Mil Spec Single Material Response
Material Thickness [ABPX]
0.040 Inches Nominal
Material [MATT]
Titanium Alloy
Overall Length [ABHP]
7.060 Inches Nominal
Overall Width [ABMK]
1.060 Inches Nominal
Special Features [FEAT]
Requested Name:Filler Uhf;Material:6Al-4V

1560-01-432-0357 Management Data Management Data 1560-01-432-0357

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Apr 2018
Department of the Air Force (DF)
EA
Subscribe
1

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1560-01-432-0357 Freight Data Freight Information 1560-01-432-0357

1560-01-432-0357 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 011790. A Sub NMFC of Z. It has a NMFC Description of AIRCRAFT PARTS NOI. 1560-01-432-0357 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 04720 which rates the freight between FCL and LCL. 1560-01-432-0357 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. 1560-01-432-0357 is not classified as a special type of cargo when transported by water. 1560-01-432-0357 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.