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2920-00-720-3344

Gas Turbine Engine Spark Igniter

2920007203344 007203344 PS351092-1 FHE537

An item having one or more electrodes arranged to form an air gap across which an electric spark is introduced and discharged to ignite fuel and air mixture in an internal combustion engine for the purpose of initial starting only. In engines designed for the single electrode type, two plugs are required within the combustion chamber in proper placement to effect the air gap. An igniter plug differs from a spark plug by always having cooling facilities in the form of holes or slots in the plug casing to allow entry of air currents around the electrode(s). Excludes SPARK PLUG; GLOW PLUG and ELECTRODE. View more Gas Turbine Engine Spark Igniter

2920-00-720-3344 IGNITER,SPARK,GAS TURBINE ENGINE 2920007203344 007203344

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
November 2023
NATO Update Count
6
NATO Data Quality
2920-00-720-3344 IGNITER,SPARK,GAS TURBINE ENGINE 2920007203344 007203344 1/1
NSN 2920-00-720-3344 (Generic Image) 1/1

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2920-00-720-3344 Related Documents Related Documents 2920-00-720-3344 5+ Documents (More...)

| RNVC: 2 | DAC: 5 8 Mar 1999 8105-13-117-4591 https//www.nsnlookup.com /fsg-29/fsc-2920/us 2920-00-720-3344
Gas Turbine Engine Spark Igniter 007203344 2920-00-720-3344 2920007203344 007203344 is an item
Documents 6130-01-193-1581 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-29/fsc-2920/us 2920-00-720-3344
Gas Turbine Engine Spark Igniter 007203344 720-3344 https//www.nsnlookup.com /cage Champion Aerospace
Documents 2920-00-960-7758 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-29/fsc-2920/us 2920-00-720-3344
Gas Turbine Engine Spark Igniter 007203344 nato-stock-numbers/inc Gas Turbine Engine Spark Igniter
2925-00-585-5084 2925005855084 005855084 is an item having one or more electrodes arranged to form an air gap across which an electric spark is introduced and discharged to ignite fuel and air mixture in an internal combustion engine for the purpose of initial starting only. in engines designed for the single electrode type, two plugs are required within the combustion chamber in proper placement to effect the air gap. an igniter plug differs from a spark plug by always having cooling facilities in the form of holes or slots in the plug casing to allow entry of air currents around the electrode(s). excludes spark plug; glow plug and electrode.
1 | RNVC: 2 | DAC: 2 4 Jul 1975 2920-00-960-7758 Gas Turbine Engine Spark Igniter 1 Jan 1962 2920-00-720-3344

2920-00-720-3344 Demil Restrictions 2920-00-720-3344

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

2920-00-720-3344 is a Gas Turbine Engine Spark Igniter that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. The precious metals content of this item is unknown.

2920-00-720-3344 Management Data Management Data 2920-00-720-3344

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 2000
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:
9C

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