2840-01-686-7562

Aircraft Gas Turbine Engine Turbine Case Plug

2840016867562 016867562 3016T81P17

A usually round item of various cross sections designed for temporary installation into a hole in a CASE, TURBINE, 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 Turbine Case Plug

2840-01-686-7562 PLUG,TURBINE CASE,AIRCRAFT GAS TURBINE ENGINE 2840016867562 016867562

Managed by United States
NSN Created on 3 Mar 2020
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-01-686-7562 PLUG,TURBINE CASE,AIRCRAFT GAS TURBINE ENGINE 2840016867562 016867562 1/1
NSN 2840-01-686-7562 (Generic Image) 1/1

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3016T81P17 A usually round item of various cross sections designed for temporary installation into a
United States (US) 4. 2840-01-686-7562 Marketplace Restrictions Approved Sources Datasheet Management
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2840-01-686-7562 Demil Restrictions 2840-01-686-7562

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

2840-01-686-7562 is a Aircraft Gas Turbine Engine Turbine Case Plug 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.

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