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1560-01-433-5204

Aircraft Structural Component Support

1560014335204 014335204 371423-1

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

1560-01-433-5204 SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT 1560014335204 014335204

Managed by United States
NSN Created on 1 Jul 1996
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
1560-01-433-5204 SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT 1560014335204 014335204 1/1
NSN 1560-01-433-5204 (Generic Image) 1/1

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371423-1 A device of various shapes to be permanently attached to the structure of an aircraft.
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1560-01-433-5204 Demil Restrictions 1560-01-433-5204

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

1560-01-433-5204 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 considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). 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.

1560-01-433-5204 HTS and ScheduleB Import and Export 1560-01-433-5204

1560-01-433-5204 End Users End Users 1560-01-433-5204

Poland (WP01)
Effective Date:
1 Aug 2011
United Kingdom (ZK01)
Effective Date:
1 Jul 1996

1560-01-433-5204 Manufacturers Approved Sources 1560-01-433-5204

1560-01-433-5204 Technical Data Datasheet 1560-01-433-5204

Characteristic
Specifications
FIIG
A11800
Material [MATT]
Aluminum Alloy 2024
Aircraft Location [CZDJ]
Wing
Aircraft Mission Design Series [CZEK]
C130j
Material Thickness [ABPX]
0.091 Inches Nominal
End Item Identification [AGAV]
Aircraft C130 J

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1560-01-433-5204 Freight Data Freight Information 1560-01-433-5204

1560-01-433-5204 has freight characteristics managed by the Bureau of Accounts.. 1560-01-433-5204 has a variance between NMFC and UFC when transported by rail and the description should be consulted.