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2840-01-353-4601

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840013534601 013534601 3091718-5

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

2840-01-353-4601 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013534601 013534601

Managed by United States
NSN Created on 11 Feb 1992
Data Last Changed
January 2023
NATO Update Count
9
NATO Data Quality
2840-01-353-4601 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013534601 013534601 1/1
NSN 2840-01-353-4601 (Generic Image) 1/1

2840-01-353-4601 Stock and Availability Marketplace 2840-01-353-4601

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2840-01-353-4601 Related Documents Related Documents 2840-01-353-4601 1+ Documents (More...)

3091718-5 A stationary arched metal segment used to establish clearance and a seal for the tip of a
United States (US) 4. 2840-01-353-4601 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-353-4601 RQST Updated Every Day 2840-01-353-4601 RQST NE Related Documents

2840-01-353-4601 Demil Restrictions 2840-01-353-4601

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

2840-01-353-4601 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.

2840-01-353-4601 HTS and ScheduleB Import and Export 2840-01-353-4601

2840-01-353-4601 End Users End Users 2840-01-353-4601

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

2840-01-353-4601 Manufacturers Approved Sources 2840-01-353-4601

2840-01-353-4601 Technical Data Datasheet 2840-01-353-4601

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Pacer Dawn
Criticality Code Justification [CRTL]
Agav
Engine Section Location [CZBJ]
High Pressure Turbine
Material [MATT]
Steel Overall
Material Document And Classification [MDCL]
Ems55451 Assn Std Single Material Response Overall
Overall Length [ABHP]
1.853 Inches Minimum And 1.873 Inches Maximum
Overall Width [ABMK]
1.620 Inches Minimum And 1.650 Inches Maximum

2840-01-353-4601 Related Items NATO Stock Numbers Related to 2840-01-353-4601

2840-01-353-4601 Freight Data Freight Information 2840-01-353-4601

2840-01-353-4601 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-353-4601 has a variance between NMFC and UFC when transported by rail and the description should be consulted.