9905-14-213-1198
Marker Band
9905142131198 142131198 202097-4
An item cut to a specific length suitable for wrapping around a cable, pipe, wire, wire rope and the like. It is secured by crimping, slot and tongue, or similar method of fastening. It is intended to provide identification. It may be blank, specifically color coded, or inscribed with information. Excludes TAG, MARKER. View more Marker Band
Managed by France
NSN Created on 1 Jan 1964
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 9905-14-213-1198
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Related Documents 9905-14-213-1198 5+ Documents (More...)
9905-14-238-4209 9905142384209 142384209 is an item cut to a specific length suitable for wrapping around a cable, pipe, wire, wire rope and the like. it is secured by crimping, slot and tongue, or similar method of fastening. it is intended to provide identification. it may be blank, specifically color coded, or inscribed with information. excludes tag, marker.
CAGE 1CN40 The Zee Company in San Antonio, TX United States
https//www.nsnlookup.com
/fsg-16/fsc-1660/us
/fsg-16/fsc-1660/us
1660-00-251-2552 Aircraft Cooling Turbine Turbine Wheel
1660-00-251-2552 1660002512552 002512552 is an item consisting of blades or vanes equally spaced around the periphery or face of a hub, rotor or wheel. designed to receive the energy of compressed air directed through nozzle vanes and impinged upon the blades of the turbine wheel creating rotary energy and motion. drives an impeller or fan and discharges cool air. consists of a single one piece wheel. it is a rotating part of an aircraft cooling turbine.
4730-27-058-0968 4730270580968 270580968 is a fitting that forms an angle of less than 180 degrees (3.141 radians) from the straight flow. both connecting ends have standard pipe threads or are unthreaded and designed to accommodate a pipe. it may have side or heel inlet(s). see also elbow, tube; and connector, multiple, fluid pressure line. excludes bend, soil pipe.
1660-00-594-8346 1660005948346 005948346 is an item consisting of blades or vanes equally spaced around the periphery or face of a hub, rotor, or wheel. designed to receive the energy of compressed air directed through nozzle vanes and impinged upon the blades of the turbine wheel creating rotary energy and motion. drives an impeller or fan and discharges cool air. consists of two matched wheels, one smaller than the other, mounted together to form a single turbine wheel. it is a rotating part of an aircraft cooling turbine.
Restrictions 9905-14-213-1198
Approved Sources 9905-14-213-1198
- Part Number
- Manufacturer
- Status
- 202097-4
- Manufacturer
- F5350 - Dga/Do/Um Esio (Active)
- Primary Buy
- Primary Buy
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