2840-12-184-0768

Aircraft Gas Turbine Engine Exhaust Duct

2840121840768 121840768 105-60163

A cylindrical shaped item designed to direct the hot gases that are discharged from an ENGINE, GAS TURBINE, AIRCRAFT. It is the outer portion of a DUCT AND CONE, EXHAUST, AIRCRAFT GAS TURBINE ENGINE. It may be attached directly to the engine. View more Aircraft Gas Turbine Engine Exhaust Duct

2840-12-184-0768 DUCT,EXHAUST,AIRCRAFT GAS TURBINE ENGINE 2840121840768 121840768

Managed by Germany
NSN Created on 19 Jun 1980
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-12-184-0768 DUCT,EXHAUST,AIRCRAFT GAS TURBINE ENGINE 2840121840768 121840768 1/1
NSN 2840-12-184-0768 (Generic Image) 1/1

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2840-12-184-0768 Related Documents Related Documents 2840-12-184-0768 5+ Documents (More...)

Documents 2840-00-134-5088 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-184-0768
Aircraft Gas Turbine Engine Exhaust Duct 2840-12-184-0768 2840121840768 121840768 is a cylindrical
Plates from Germany (DE) Jan 2000 9905-12-349-7733 https//www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-184-0768
1560-12-352-2493 1560123522493 123522493 is an item of unique shapes and cross-sectional configurations specifically designed with dimensional tolerances and finishes. it may be metallic and/or nonmetallic and must be able to mate with or join to like items with aircraft application. the item may consist of more then one (1) piece to form an assembly. do not use if a more specific item name exists. excludes bracket (1), structural component, aircraft.
2840-00-115-9507 2840001159507 001159507 is a cylindrical shaped item designed to direct the hot gases that are discharged from an engine, gas turbine, aircraft. it is the outer portion of a duct and cone, exhaust, aircraft gas turbine engine. it may be attached directly to the engine.
May 1969 9905-12-349-7733 Designation Plate 105-41222.25RNCC: 3 | RNVC: 2 | DAC: 3 6 Jan 2000 2840-12-184-0768

2840-12-184-0768 Demil Restrictions 2840-12-184-0768

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

2840-12-184-0768 is a Aircraft Gas Turbine Engine Exhaust Duct

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