2840-14-562-3701

Turbine Engine Air Intake

2840145623701 145623701 502800-1A

An item designed to provide an optimum flow of air to the fore part of a turbine engine. Excludes AIR FLOW, NON AIRCRAFT GAS TURBINE ENGINE and BAFFLE AIR FLOW AIRCRAFT GAS TURBINE ENGINE. View more Turbine Engine Air Intake

2840-14-562-3701 AIR INTAKE,TURBINE ENGINE 2840145623701 145623701

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NSN Created on 19 Oct 2009
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
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2840-14-562-3701 Related Documents Related Documents 2840-14-562-3701 5+ Documents (More...)

https//www.nsnlookup.com /nato/nato-stock-numbers/inc Turbine Engine Air Intake (INC 53628) 2003 2840-14-562-3701
2835-14-514-3052 2835145143052 145143052 is an item designed to provide an optimum flow of air to the fore part of a turbine engine. excludes air flow, non aircraft gas turbine engine and baffle air flow aircraft gas turbine engine.
2840-99-574-0128 Turbine Engine Air Intake NH24468-158RNCC: 3 | RNVC: 2 | DAC: 2 12 May 2003 2840-14-562-3701
4820-00-849-0444 4820008490444 008490444 is a valve permitting flow in one direction only. it does not have a stem, except when equipped with a lever and weight and has no pressure adjustment. it may be inline or cartridge (manifold) design.
2840-14-519-9144 2840145199144 145199144 is an item designed to provide an optimum flow of air to the fore part of a turbine engine. excludes air flow, non aircraft gas turbine engine and baffle air flow aircraft gas turbine engine.

2840-14-562-3701 Demil Restrictions 2840-14-562-3701

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

2840-14-562-3701 is a Turbine Engine Air Intake

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