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2840-01-380-3615

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840013803615 013803615 3091718-7

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

2840-01-380-3615 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013803615 013803615

Managed by United States
NSN Created on 17 Sep 1993
Data Last Changed
January 2023
NATO Update Count
8
NATO Data Quality
2840-01-380-3615 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013803615 013803615 1/1
NSN 2840-01-380-3615 (Generic Image) 1/1

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2840-01-380-3615 Related Documents Related Documents 2840-01-380-3615 1+ Documents (More...)

3091718-7 A stationary arched metal segment used to establish clearance and a seal for the tip of a
United States (US) 4. 2840-01-380-3615 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-380-3615 RQST Updated Every Day 2840-01-380-3615 RQST NE Related Documents

2840-01-380-3615 Demil Restrictions 2840-01-380-3615

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

2840-01-380-3615 is a Aircraft Gas Turbine Engine Turbine Shroud Segment that does not have a nuclear hardened feature or any other critical feature 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.

2840-01-380-3615 HTS and ScheduleB Import and Export 2840-01-380-3615

2840-01-380-3615 End Users End Users 2840-01-380-3615

Czech Republic (WZ01)
Effective Date:
1 Feb 2013
Taiwan, Province of China (YE01)
Effective Date:
1 Feb 2015

2840-01-380-3615 Manufacturers Approved Sources 2840-01-380-3615

2840-01-380-3615 Technical Data Datasheet 2840-01-380-3615

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Pacer Dawn
Diameter [ABMZ]
18.680 Inches Minimum And 18.700 Inches Maximum
Engine Section Location [CZBJ]
High Pressure Turbine
Material [MATT]
Steel Overall
Material Document And Classification [MDCL]
Ems5545 Mfr Ref Single Material Response Overall
Overall Length [ABHP]
1.853 Inches Minimum And 1.873 Inches Maximum

2840-01-380-3615 Related Items NATO Stock Numbers Related to 2840-01-380-3615

2840-01-380-3615 Freight Data Freight Information 2840-01-380-3615

2840-01-380-3615 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-380-3615 has a variance between NMFC and UFC when transported by rail and the description should be consulted.