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2840-00-157-3604

Aircraft Gas Turbine Engine Compressor Vane Assembly

2840001573604 001573604 3011163 3011963 3017763

A stationary item designed for the purpose of directing air at the proper angle and velocity from a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Compressor Vane Assembly

2840-00-157-3604 VANE ASSEMBLY,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840001573604 001573604

Managed by United States
NSN Created on 20 May 1970
Data Last Changed
November 2023
NATO Update Count
11
NATO Data Quality
2840-00-157-3604 VANE ASSEMBLY,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840001573604 001573604 1/1
NSN 2840-00-157-3604 (Generic Image) 1/1

2840-00-157-3604 Stock and Availability Marketplace 2840-00-157-3604

2840-00-157-3604 Related Documents Related Documents 2840-00-157-3604 5+ Documents (More...)

4730-01-301-1163 4730013011163 013011163 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.
6150-99-301-1963 6150993011963 993011963 is a definite continuous length of cable, special purpose, electrical with branches (forks), and having one or more ends processed and/or terminated in fittings to provide for connection to other items. excludes lead, test. see also wiring harness.
5340-12-301-1163 5340123011163 123011163 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.
5305-01-301-1963 5305013011963 013011963 is a headed, threaded fastening device over which may be assembled; (1) a stand-off; (2) a flanged bushing with washer(s) and/or a shouldered bushing without a flange, or it may have an internally threaded sleeve that is an integral part of the screw; a washer and an externally thread self-locking bushing that is driven by an inserted driver. attached to panel by threaded bushing or by flaring end of stand-off, or bushing. used in conjunction with a speed nut, nut plate, or driven into a threaded hole in the item that the panel is fastened to. may be spring loaded.
4730-12-301-7763 4730123017763 123017763 is a fitting having three connections with the branch connection fixed at 90 degrees (1.5705 radians) to the run. the connections have standard hose threads, an incomplete part of a threaded end connection that grips the hose directly, or is unthreaded and designed to accommodate a hose. it may have side inlet(s). it is used as a junction at the intersection of hose or hose fitting.

2840-00-157-3604 Demil Restrictions 2840-00-157-3604

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

2840-00-157-3604 is a Aircraft Gas Turbine Engine Compressor Vane Assembly 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 is not suspected to be hazardous. This item does not contain a precious metal.

2840-00-157-3604 Management Data Management Data 2840-00-157-3604

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 1999
Department of the Navy (DN)
EA
Subscribe
1
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Navy (DN)
N
V
Discontinued Without Replacement

Navy Navy

Cognizance:
9W

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