2840-99-322-3506

Aircraft Gas Turbine Engine Front Frame Strut

2840993223506 993223506

A rigid piece designed to resist pressure in the direction of its length. It is positioned between the inner and outer rings and is a main component of a FRAME, FRONT, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Front Frame Strut

Managed by United Kingdom

Data Last Changed
January 2024

NATO Update Count
1

NATO Data Quality

2840-99-322-3506 STRUT,FRONT FRAME,AIRCRAFT GAS TURBINE ENGINE 2840993223506 993223506 1/1 — NSN 2840-99-322-3506 (Generic Image) 1/1

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2840-99-322-3506 is a Aircraft Gas Turbine Engine Front Frame Strut

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