1560-00-480-5021

Aircraft Structural Component Support

1560004805021 004805021 484-1317-21

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

1560-00-480-5021 SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT 1560004805021 004805021

Managed by United States
NSN Created on 31 Aug 1970
Data Last Changed
November 2023
NATO Update Count
6
NATO Data Quality
1560-00-480-5021 SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT 1560004805021 004805021 1/1
NSN 1560-00-480-5021 (Generic Image) 1/1

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1560-00-480-5021 Related Documents Related Documents 1560-00-480-5021 3+ Documents (More...)

3120-17-108-1255 3120171081255 171081255 is a tubular shaped item with or without flange(s) designed to reduce friction and carry a kinetic load on the surface(s) parallel to the axis of the bore. it must have a visible or detectable means of lubrication or be self-lubricated. the over all length must exceed 25 percent of the outside diameter or the shortest distance between peripheral flats of the body, except for straight tubular (without flange or shoulder) items having a bearing surface(s) parallel to the axis of the bore only. includes items which are divided into two or more segments which include 180 degrees (3.141 radians) or less of the bearing periphery. see also bushing, sleeve; spacer, sleeve; and washer (as modified). excludes pin, hollow.
3040-00-588-4658 3040005884658 005884658 is a shaft having two or more different diameters (greater than 0.031 inches (0.79 millimeter)) along its length. it must have one or more of the following conditions: a specified surface finish designation in the range 1 to 125 microinches (0.025 to 3.2 micrometers) arithmetical average (aa), machined peripheral flat(s), circular groove(s), keyway(s), splines, threads, or holes. the ends and/or shoulders may be machined to accommodate bearings, couplings, and the like. it is not designed for use in aligning by fitting into corresponding holes of another item. for items used to support rotating members see axle(1), shouldered. for items not having any of the above conditions see pin, shoulder, headless. excludes shaft(1), straight; and axle(1), straight.
5020 Aircraft Structural Component Fitting 484-1323-22RNCC: 3 | RNVC: 2 | DAC: 2 31 Aug 1970 1560-00-480-5021

1560-00-480-5021 Demil Restrictions 1560-00-480-5021

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

1560-00-480-5021 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.

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