2840-21-920-1934

Aircraft Gas Turbine Engine Combustion Chamber Liner

2840219201934 219201934 3122633-01

A cylindrical shaped item positioned inside the CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. It is designed to direct the flow of hot gasses to the TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Combustion Chamber Liner

2840-21-920-1934 LINER,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840219201934 219201934

Managed by Canada
NSN Created on 14 Jun 1999
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-920-1934 LINER,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840219201934 219201934 1/1
NSN 2840-21-920-1934 (Generic Image) 1/1

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2840-21-920-1934 Related Documents Related Documents 2840-21-920-1934 5+ Documents (More...)

https//www.nsnlookup.com
/fsg-28/fsc-2840/us
2840-01-449-4089 2840014494089 014494089,4083173
2840/uk 2840-99-607-0091 2840996070091 996070091,RK42057A www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-920-1934
2840219201934 219201934,3122633-01 491-0006 2840-01-449-4089 https//www.nsnlookup.com /fsg-28/fsc
https//www.nsnlookup.com
/fsg-28/fsc-2840/uk
2840-99-607-0091 2840996070091 996070091,RK42057A
2840-01-421-9737 2840-01-419-8772 2840-99-607-0091 https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-920-1934
2840219201934 219201934,3122633-01 491-0006 2840-01-449-4089 2840-01-360-4057 2840-01-608-9103
https//www.nsnlookup.com
/fsg-28/fsc-2840/us
2840-01-608-9103 2840016089103 016089103,6900T52G02
2840-01-608-9103 2840016089103 016089103 is a cylindrical shaped item positioned inside the chamber, combustion, aircraft gas turbine engine. it is designed to direct the flow of hot gasses to the turbine assembly, aircraft gas turbine engine.
https//www.nsnlookup.com
/fsg-28/fsc-2840/us
2840-01-419-8772 2840014198772 014198772,2783692-1
2840-01-419-8772 2840014198772 014198772 is a cylindrical shaped item positioned inside the chamber, combustion, aircraft gas turbine engine. it is designed to direct the flow of hot gasses to the turbine assembly, aircraft gas turbine engine.
https//www.nsnlookup.com
/fsg-28/fsc-2840/us
2840-01-421-9737 2840014219737 014219737,4083057
2840-01-421-9737 2840014219737 014219737 is a cylindrical shaped item positioned inside the chamber, combustion, aircraft gas turbine engine. it is designed to direct the flow of hot gasses to the turbine assembly, aircraft gas turbine engine.

2840-21-920-1934 Demil Restrictions 2840-21-920-1934

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

2840-21-920-1934 is a Aircraft Gas Turbine Engine Combustion Chamber Liner

2840-21-920-1934 End Users End Users 2840-21-920-1934

Brazil (YA)
France (ZF)
Republic of Korea (ZH)
Netherlands (ZN)

2840-21-920-1934 Manufacturers Approved Sources 2840-21-920-1934

Part Number
Manufacturer
Status
3122633-01
00198 - Pratt & Whitney Canada Cie (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 5

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2840-99-607-4662 2840-14-550-0857 2840-21-856-8513 2840-21-908-1854 2840-21-913-0334 2840-01-491-0006 2840-01-449-4089 2840-01-360-4057 2840-01-608-9103 2840-01-421-9737 2840-01-419-8772 2840-99-607-0091 2840-21-869-4198 2840-00-184-5042 2840-01-683-0618 2840-01-111-1894 2840-00-126-2836 2840-00-110-6045