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2840-01-015-1751

Aircraft Gas Turbine Engine Combustion Chamber Liner

2840010151751 010151751 643E406G9

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

2840-01-015-1751 LINER,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840010151751 010151751

Managed by United States
NSN Created on 15 Jan 1976
Data Last Changed
January 2023
NATO Update Count
23
NATO Data Quality
2840-01-015-1751 LINER,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE 2840010151751 010151751 1/1
NSN 2840-01-015-1751 (Generic Image) 1/1

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2840-01-015-1751 Related Documents Related Documents 2840-01-015-1751 1+ Documents (More...)

643E406G9 A cylindrical shaped item positioned inside the CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE
United States (US) 4. 2840-01-015-1751 Marketplace Restrictions Approved Sources Datasheet Management
NE Updated Every Day 2840-01-015-1751 RQST Updated Every Day 2840-01-015-1751 RQST NE Related Documents

2840-01-015-1751 Demil Restrictions 2840-01-015-1751

DEMIL: A | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC:

2840-01-015-1751 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 is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-015-1751 HTS and ScheduleB Import and Export 2840-01-015-1751

2840-01-015-1751 End Users End Users 2840-01-015-1751

Italy (ZR01)
Effective Date:
1 Dec 2007
Greece (ZU01)
Effective Date:
1 Apr 1991
Turkey (ZW01)
Effective Date:
1 Dec 1995

2840-01-015-1751 Manufacturers Approved Sources 2840-01-015-1751

2840-01-015-1751 Technical Data Datasheet 2840-01-015-1751

Characteristic
Specifications
FIIG
A530F0
End Item Identification [AGAV]
J-79 Aircraft Turbine Engines
Criticality Code Justification [CRTL]
Agav
Engine Section Location [CZBJ]
Combustion Chamber
Overall Length [ABHP]
12.030 Inches Minimum And 12.080 Inches Maximum
Special Features [FEAT]
Used On -7B, -11A, -11B And -19 Series Engines

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2840-01-015-1751 Freight Data Freight Information 2840-01-015-1751

2840-01-015-1751 has freight characteristics.. 2840-01-015-1751 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

2840-01-015-1751 Packaging Data Packaging Data 2840-01-015-1751

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
Packaging Data does not meet current MIL-STD-2073-1E

Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
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--
--
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Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
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--
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Physical Protection
Any Suitable Process
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
No Requirement
MIL-DTL-17667, Neutral Wrapping Paper
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ASTM-D5118, Type CF, Class Domestic, Corrugated Fiberboard Box
No special marking

Intermediate Pack Level

Quantity of Unit Packs
Container
ASTM-D5118, Type CF, Class Domestic, Corrugated Fiberboard Box