2840-14-521-9857

Aircraft Gas Turbine Engine Compressor Blade

2840145219857 145219857 01AT1185

An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Compressor Blade

2840-14-521-9857 BLADE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840145219857 145219857

Managed by France
NSN Created on 27 Sep 2000
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-521-9857 BLADE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840145219857 145219857 1/1
NSN 2840-14-521-9857 (Generic Image) 1/1

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2840-14-521-9857 Related Documents Related Documents 2840-14-521-9857 5+ Documents (More...)

7643-01-579-1185 7643015791185 015791185 is a map, chart, or geodetic product, distributed by agencies such as the defense mapping agency, which is associated with land navigation, tracking, and charting.
5340-01-391-1185 5340013911185 013911185 is a rigid item usually fabricated from flat material, forming two alternate or two adjacent interior angles, both which are less than 180 degrees (3.141 radians). it is designed to position, align, and/or support an item. it may be reinforced. see also bracket, angle and bracket (1), mounting.
5305-01-703-1185 5305017031185 017031185 is an externally threaded fastener designed for insertion into holes in assembled parts, for mating with a preformed internal thread and for tightening or releasing by torquing the head. the threaded and unthreaded portions are both of the same nominal diameter of 0.190 inch (5 mm) or larger. head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. the thread length being the controlled dimension, the grip length is not specified. a locking feature may be incorporated in the design of the head or threads. the head is not designed to be held or driven with an inserted driver or by the thumb and fingers. excludes bolt,machine; bolt,externally relieved body; bolt,internal wrenching; and screw,cap,socket head.

2840-14-521-9857 Demil Restrictions 2840-14-521-9857

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2840-14-521-9857 is a Aircraft Gas Turbine Engine Compressor Blade

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