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2840-01-347-0815

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840013470815 013470815 3091429-3

A stationary arched metal segment used to establish clearance and a seal for the tip of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a SEAL RING, LABYRINTH, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Shroud Segment

2840-01-347-0815 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013470815 013470815

Managed by United States
NSN Created on 16 Oct 1991
Data Last Changed
January 2023
NATO Update Count
8
NATO Data Quality
2840-01-347-0815 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013470815 013470815 1/1
NSN 2840-01-347-0815 (Generic Image) 1/1

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2840-01-347-0815 Related Documents Related Documents 2840-01-347-0815 4+ Documents (More...)

3091429-3 A stationary arched metal segment used to establish clearance and a seal for the tip of a
RQST NE Updated Every Day 2840-01-347-0815 RQST Updated Every Day 2840-01-347-0815 RQST NE Related Documents
Management RQST NE Updated Every Day 2840-01-347-0815 RQST Updated Every Day 2840-01-347-0815 RQST NE
https//www.nsnlookup.com Datasheet 4920-01-458-0995 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-347-0815
2840013470815 013470815,3091429-3 Day 2840-01-347-0815 RQST NE Related Documents https//www.nsnlookup.com
CharacteristicSpecificationsFIIGA505C0Special Features [FEAT]Used On Nsn 2840-01-348-2306, 2840-01-354-8294, And 2840-01-347-0815
Day 2840-01-348-2306 RQST NE Related Documents https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-347-0815
2840013470815 013470815,3091429-3 //www.nsnlookup.com CharacteristicSpecificationsFIIGA505C0Special
Features [FEAT]Used On Nsn 2840-01-348-2306 , 2840-01-354-8294, And 2840-01-347-0815 https//www.nsnlookup.com
]Used On Nsn 2840-01-348-2306, 2840-01-354-8294 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-347-0815
2840013470815 013470815,3091429-3 www.nsnlookup.com CharacteristicSpecificationsFIIGA505C0Special

2840-01-347-0815 Demil Restrictions 2840-01-347-0815

DEMIL: A | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC: 0

2840-01-347-0815 is a Aircraft Gas Turbine Engine Turbine Shroud Segment 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.

2840-01-347-0815 HTS and ScheduleB Import and Export 2840-01-347-0815

2840-01-347-0815 End Users End Users 2840-01-347-0815

Taiwan, Province of China (YE01)
Effective Date:
1 Feb 2015

2840-01-347-0815 Manufacturers Approved Sources 2840-01-347-0815

2840-01-347-0815 Technical Data Datasheet 2840-01-347-0815

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Pacer Dawn
Criticality Code Justification [CRTL]
Agav
Design Type [APGF]
Axial-Centrifugal
Diameter [ABMZ]
15.729 Inches Minimum And 15.735 Inches Maximum
Engine Section Location [CZBJ]
High Pressure Compressor
Material [MATT]
Steel Overall
Material Document And Classification [MDCL]
Ems 55464 Assn Std Single Material Response Overall
Overall Length [ABHP]
1.224 Inches Minimum And 1.228 Inches Maximum
Stage Number [CZCJ]
2

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2840-01-347-0815 Freight Data Freight Information 2840-01-347-0815

2840-01-347-0815 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-347-0815 has a variance between NMFC and UFC when transported by rail and the description should be consulted.