2840-14-538-4838
Aircraft Gas Turbine Engine Augmenter Exhaust Nozzle
2840145384838 145384838 NGM0010038125407
A compliment of several eyelet or flap type items that form a duct like end on an ENGINE, GAS TURBINE, AIRCRAFT. The eyelets are moved by hydraulic actuators to cause the opening to become larger or smaller. The changing of the opening size controls the thrust and temperature of the engine. This item is only used on engines with an AFTERBURNER, TURBINE ENGINE attached. View more Aircraft Gas Turbine Engine Augmenter Exhaust Nozzle
Managed by France
NSN Created on 9 Dec 2003
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 2840-14-538-4838 2+ Documents (More...)
Gas Turbine Engine Augmenter Exhaust Nozzle 502-712-818-0RNCC: 3 | RNVC: 2 | DAC: 1 1 Jan 1974 2840-14-538-4838
2840-14-538-4241 2840145384241 145384241 is a compliment of several eyelet or flap type items that form a duct like end on an engine, gas turbine, aircraft. the eyelets are moved by hydraulic actuators to cause the opening to become larger or smaller. the changing of the opening size controls the thrust and temperature of the engine. this item is only used on engines with an afterburner, turbine engine attached.
Restrictions 2840-14-538-4838
End Users 2840-14-538-4838
- France (ZF)
Approved Sources 2840-14-538-4838
- Part Number
- Manufacturer
- Status
- NGM0010038125407
- Manufacturer
- FAGG5 - Mn/Ssf Marine Nationale / Service De (Active)
- Definitive Standard
- Definitive Standard
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