2840-14-309-5747
Aircraft Gas Turbine Engine Turbine Nozzle Assembly
2840143095747 143095747 0205121130
A stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Turbine Nozzle Assembly
Managed by France
NSN Created on 1 Jan 1974
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-14-309-5747
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0205121130 A stationary item designed for the purpose of directing air at the proper angle and velocity
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2840005669163 005669163 223-3775 2840-12-367-7151 2840-01-525-4101 2840-14-309-5747 -2840/us 2840-00
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2840005669163 005669163 223-3775 2840-12-367-7151 2840-01-525-4101 2840-14-309-5747 -2840/us 2840-00
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2840-14-526-7413 2840-14-383-1690 -2840/uk 2840 2840-14-309-5747 2840-14-526-7413 2840-14-383-1690
Restrictions 2840-14-309-5747
End Users 2840-14-309-5747
- France (ZF)
Approved Sources 2840-14-309-5747
- Part Number
- Manufacturer
- Status
- 0205121130
- Manufacturer
- F0228 - Safran Helicopter Engines (Active)
- Primary Buy
- Primary Buy
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