2840-01-613-6803

Aircraft Gas Turbine Engine Combustion Chamber Case Plug

2840016136803 016136803 8522-389A

A usually round item of various cross sections designed for temporary installation into a hole in a CASE, COMBUSION CHAMBER, AIRCRAFT GAS TURBINE ENGINE for the purpose of preventing air from escaping during engine operation. When removed, the hole is for inserting inspection probes, borescopes and the like. It may be grooved or tapered for installation and removal. It may include spacers, springs, rivets and the like. View more Aircraft Gas Turbine Engine Combustion Chamber Case Plug

2840-01-613-6803 PLUG,COMBUSTION CHAMBER CASE,AIRCRAFT GAS TURBINE ENGINE 2840016136803 016136803

Managed by United States
NSN Created on 14 Nov 2012
Data Last Changed
November 2023
NATO Update Count
2
NATO Data Quality
2840-01-613-6803 PLUG,COMBUSTION CHAMBER CASE,AIRCRAFT GAS TURBINE ENGINE 2840016136803 016136803 1/1
NSN 2840-01-613-6803 (Generic Image) 1/1

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8522-389A A usually round item of various cross sections designed for temporary installation into a
United States (US) 4. 2840-01-613-6803 Marketplace Restrictions Approved Sources Datasheet Management
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2840-01-613-6803 Demil Restrictions 2840-01-613-6803

DEMIL: A | DEMILI: 1 | CRITICALITY: | HMIC: N | PMIC: A | EDC: | ADPEC: 0

2840-01-613-6803 is a Aircraft Gas Turbine Engine Combustion Chamber Case Plug 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.

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