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2840-01-421-9735
Aircraft Gas Turbine Engine Combustion Chamber Liner
2840014219735 014219735 4083067
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
January 2023
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2840014219735 014219735,4083067 Upgrade 2840-01-421-9735Aircraft Gas Turbine Engine Combustion
Restrictions 2840-01-421-9735
2840-01-421-9735 is a Aircraft Gas Turbine Engine Combustion Chamber Liner that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal. This item is ADP supplies or support equipment. It may be consumable supplies such as continuous flat fold paper, sheet paper, seal bands, tape, empty tape reels and hubs, tape canisters or tape carrying cases. It may also be support equipment such as magnetic tape testing, certifying and cleaning equipment, disk pack testing, certifying and cleaning equipment, tape winders snd splicers or card reconditioners.
Import and Export 2840-01-421-9735
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-421-9735
- Singapore (YJ01)
- Effective Date:
- 1 Sep 1998
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1998
- Greece (ZU01)
- Effective Date:
- 1 May 2008
Approved Sources 2840-01-421-9735
- Part Number
- Manufacturer
- Status
- 4083067
- Manufacturer
- 77445 - Rtx Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-421-9735
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- End Item Identification [AGAV]
- F100-Pw-229 Aircraft Gas Turbine Engine
- Criticality Code Justification [CRTL]
- Stdc And Czbj And Abhp And Abmk And Feat
- Engine Section Location [CZBJ]
- Combustion Chamber
- Material Document And Classification [MDCL]
- Pwa 1475 Mfr Ref Single Material Response Overall
- Material [MATT]
- Nickel Alloy Overall
- Overall Length [ABHP]
- 4.276 Inches Minimum And 4.388 Inches Maximum
- Overall Width [ABMK]
- 1.415 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Liner Segment,Combustion Chamber Duct
- Special Features [FEAT]
- Thermal Barrier Coating Added Per Ecn 95Qa006
- Surface Treatment Document And Classification [STDC]
- Spec Pwa 265-1 Mfr Ref Single Treatment Response Overall
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Freight Information 2840-01-421-9735
2840-01-421-9735 has freight characteristics.. 2840-01-421-9735 has a variance between NMFC and UFC when transported by rail and the description should be consulted.