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

2840-14-538-4838 NOZZLE,AUGMENTER EXHAUST,AIRCRAFT GAS TURBINE ENGINE 2840145384838 145384838

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NSN Created on 9 Dec 2003
Data Last Changed
January 2023
NATO Update Count
1
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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.

2840-14-538-4838 Demil Restrictions 2840-14-538-4838

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

2840-14-538-4838 is a Aircraft Gas Turbine Engine Augmenter Exhaust Nozzle

2840-14-538-4838 End Users End Users 2840-14-538-4838

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