2840-33-209-9181
Aircraft Gas Turbine Engine Turbine Nozzle
2840332099181 332099181 M780A4021208
A single 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. View more Aircraft Gas Turbine Engine Turbine Nozzle
Managed by Spain
NSN Created on 2 Apr 2012
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-33-209-9181
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Related Documents 2840-33-209-9181 2+ Documents (More...)
Aircraft Gas Turbine Engine Airflow Baffle M541A138120200RNCC: 3 | RNVC: 2 | DAC: 1 25 Oct 2013 2840-33-209-9181
2840-33-209-7284 2840332097284 332097284 is a cylindrical shaped item or a segment thereof designed to direct air into or around a turbine assembly, aircraft gas turbine engine for cooling purposes.
Restrictions 2840-33-209-9181
End Users 2840-33-209-9181
- Spain (YB)
Approved Sources 2840-33-209-9181
- Part Number
- Manufacturer
- Status
- M780A4021208
- Manufacturer
- 0117B - Airbus Defence And Space Sau (Active)
- Primary Buy
- Primary Buy
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