2925-01-682-0541
Gas Turbine Engine Spark Igniter
2925016820541 016820541 CH31975-2
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
January 2023
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Gas Turbine Engine Spark Igniter 016820541 CH31975-2 An item having one or more electrodes arranged
Restrictions 2925-01-682-0541
2925-01-682-0541 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. Demilitarization of this item has been confirmed and is not currently subject to changes. 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. This item does not contain a precious metal.
Import and Export 2925-01-682-0541
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Approved Sources 2925-01-682-0541
- Part Number
- Manufacturer
- Status
- CH31975-2
- Manufacturer
- 0AFL4 - Champion Aerospace Llc (Active)
- Incomplete Reference
- Incomplete Reference