2540-99-391-2418

Blank Panel

2540993912418 993912418 00A0645A FV2294782

A panel designed to fill a space not occupied by actual operating components, and may have instructions, component designations, or component identifications etched or printed thereon. View more Blank Panel

2540-99-391-2418 PANEL,BLANK 2540993912418 993912418

Managed by United Kingdom
NSN Created on 3 Jun 2009
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2540-99-391-2418 PANEL,BLANK 2540993912418 993912418 1/1
NSN 2540-99-391-2418 (Generic Image) 1/1

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2540-99-391-2418 Related Documents Related Documents 2540-99-391-2418 5+ Documents (More...)

4730-00-054-0645 4730000540645 000540645 is a fitting having three connections with the branch connection fixed at 90 degrees (1.5705 radians) to the run. the connections have machine threads (straight threads other than pipe or hose series) designed to accommodate a tube, or are unthreaded and designed to accommodate a tube. it may have side inlet(s). it is used as a junction at the intersection of a tube or tube fitting.
5975-00-665-0645 5975006650645 006650645 is an item of metal and/or insulating material having internal threads designed to fit over the end of electrical conduit and/or fittings to provide a smooth interior with a rounded edge to prevent damage to the insulation of the wire or cable emerging therefrom. it may be designed to fit over the end of thin wall conduit, and to be fitted with holding (staking) screws, or it may be provided with internal straight threads for attaching to thick wall electrical conduit or fittings. it may be fitted with a temporary knockout cap (bushcap), and grounding or bonding facilities. for externally threaded items, see box connector, electrical; bushing, electrical conductor; chase nipple, conduit and bushing, strain relief, cable. see also ferrule, electrical conduit. excludes plain sleeve bushings.
3120-00-662-0645 3120006620645 006620645 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.
1560-00-960-0645 1560009600645 009600645 is 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.

2540-99-391-2418 Demil Restrictions 2540-99-391-2418

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2540-99-391-2418 is a Blank Panel

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