2840-15-207-0104

Aircraft Gas Turbine Engine Diffuser

2840152070104 152070104 4150T34G01 (241)A34604150T34G01

A frame with stationary struts, designed to diffuse and direct air from the COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may have mounting facilities for external components. It may provide support and house a compressor rear bearing. May include a CASE (3), DIFFUSER, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Diffuser

2840-15-207-0104 DIFFUSER,AIRCRAFT GAS TURBINE ENGINE 2840152070104 152070104

Managed by Italy
NSN Created on 8 Aug 2012
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-15-207-0104 DIFFUSER,AIRCRAFT GAS TURBINE ENGINE 2840152070104 152070104 1/1
NSN 2840-15-207-0104 (Generic Image) 1/1

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4150T34G01 (241)A34604150T34G01 A frame with stationary struts, designed to diffuse and direct air from
2840-15-207-0104 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-207-0104
Aircraft Gas Turbine Engine Diffuser 4150T34G01 (241)A34604150T34G01 A frame with stationary struts,

2840-15-207-0104 Demil Restrictions 2840-15-207-0104

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

2840-15-207-0104 is a Aircraft Gas Turbine Engine Diffuser

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