2840-20-004-9786

Aircraft Gas Turbine Engine Combustion Chamber Duct

2840200049786 200049786 3028047

A cylindrical shaped item or a segment thereof designed to direct air into or around a CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. The internal iar is divided and directed to the burning chamber(s). The external air is used for cooling purposes. View more Aircraft Gas Turbine Engine Combustion Chamber Duct

2840-20-004-9786 DUCT,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840200049786 200049786

Managed by Canada
NSN Created on 24 Jul 2009
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-20-004-9786 DUCT,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840200049786 200049786 1/1
NSN 2840-20-004-9786 (Generic Image) 1/1

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Aircraft Gas Turbine Engine Combustion Chamber Duct (INC 52524)
Aircraft Gas Turbine Engine Combustion Chamber Duct 0265317410RNCC: 3 | RNVC: 2 | DAC: 2 1 Jan 1975 2840-20-004-9786
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1730-99-302-8047 Aircraft Landing Gear Jack 1730993028047
1730-99-302-8047 1730993028047 993028047 is a lifting device which consists basically of a ram(s) actuated by a hydraulic pump(s). one end of the ram(s) is designed specifically to mate with the jacking points on the landing gear of an aircraft. it may have a wheeled base with a drawbar for mobility. excludes jack, dolly type, hydraulic and jack, hydraulic, hand.

2840-20-004-9786 Demil Restrictions 2840-20-004-9786

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

2840-20-004-9786 is a Aircraft Gas Turbine Engine Combustion Chamber Duct

2840-20-004-9786 End Users End Users 2840-20-004-9786

United Kingdom (ZK)

2840-20-004-9786 Manufacturers Approved Sources 2840-20-004-9786

Part Number
Manufacturer
Status
3028047
00198 - Pratt & Whitney Canada Cie (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 6

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