2840-20-000-8607

Aircraft Gas Turbine Engine Compressor Disk

2840200008607 200008607 3018312 (241)001983018312SB5266 3018312SB5266

An item having provisions on the outer periphery for attaching a designated number of BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Disk

2840-20-000-8607 DISK,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840200008607 200008607

Managed by Canada
NSN Created on 26 Jun 2003
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-20-000-8607 DISK,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840200008607 200008607 1/1
NSN 2840-20-000-8607 (Generic Image) 1/1

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Aircraft Gas Turbine Engine Compressor Disk 2840-20-000-8607 2840200008607 200008607 is an item
Account Upgrade 2840-00-157-2984Aircraft Gas Turbine Engine Compressor Disk2840001572984 001572984 3018312
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COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 99 EA NS Request Quotation Subscribe to View Vendor Details... 3018312
4730-12-301-8312 4730123018312 123018312 is a flanged cylindrical metallic item designed to be used on tubing to back up the flared end and to provide a bearing surface for the coupling nut, thereby reducing wear on the tubing flare. the inside diameter of the flanged end is countersunk to form a seat for the flare when assembled to a mating fitting.
5962-01-301-8312 5962013018312 013018312 is a microcircuit specifically designed to generate, modify, or process electrical signals which operate with two distinct or binary states. these states are commonly referred to as on and off, true and false, high and low, or "1" and "0".

2840-20-000-8607 Demil Restrictions 2840-20-000-8607

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-20-000-8607 is a Aircraft Gas Turbine Engine Compressor Disk

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