2840-14-502-2151

Aircraft Gas Turbine Engine Compressor Case Plug

2840145022151 145022151 0390220440 0390220310

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

2840-14-502-2151 PLUG,COMPRESSOR CASE,AIRCRAFT GAS TURBINE ENGINE 2840145022151 145022151

Managed by France
NSN Created on 26 Nov 1997
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-502-2151 PLUG,COMPRESSOR CASE,AIRCRAFT GAS TURBINE ENGINE 2840145022151 145022151 1/1
NSN 2840-14-502-2151 (Generic Image) 1/1

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0390220440 0390220310 A usually round item of various cross sections designed for temporary installation
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2840-14-502-2151 Demil Restrictions 2840-14-502-2151

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2840-14-502-2151 is a Aircraft Gas Turbine Engine Compressor Case Plug

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