2840-14-355-3507
Aircraft Gas Turbine Engine Compressor Vane Assembly
2840143553507 143553507 70AM02103 M02103 85-801-2002
A stationary item designed for the purpose of directing air at the proper angle and velocity from a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Compressor Vane Assembly
Managed by France
NSN Created on 19 Mar 1979
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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70AM02103 M02103 85-801-2002 A stationary item designed for the purpose of directing air at the proper
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M02103 A washer of nonresilient material usually having two parallel bearing surfaces.
2840143553507 143553507,70AM02103,M02103 -14-355-3507Aircraft Gas Turbine Engine Compressor Vane
M02103 A washer of nonresilient material usually having two parallel bearing surfaces.
2840143553507 143553507,70AM02103,M02103 -14-355-3507Aircraft Gas Turbine Engine Compressor Vane
Restrictions 2840-14-355-3507
End Users 2840-14-355-3507
- France (ZF)
Approved Sources 2840-14-355-3507
- Part Number
- Manufacturer
- Status
- 70AM02103
- Manufacturer
- F0228 - Safran Helicopter Engines (Active)
- Primary Buy
- Primary Buy
- M02103
- F0228 - Safran Helicopter Engines (Active)
- Secondary Buy
- Secondary Buy
- 85-801-2002
- F5385 - Section De Codification 85 (Cancelled)
- NATO Reference
- NATO Reference
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