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2840-01-347-8986

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840013478986 013478986 3091603-1

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

2840-01-347-8986 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013478986 013478986

Managed by United States
NSN Created on 31 Oct 1991
Data Last Changed
January 2023
NATO Update Count
8
NATO Data Quality
2840-01-347-8986 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013478986 013478986 1/1
NSN 2840-01-347-8986 (Generic Image) 1/1

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2840-01-347-8986 Related Documents Related Documents 2840-01-347-8986 1+ Documents (More...)

3091603-1 A stationary arched metal segment used to establish clearance and a seal for the tip of a
United States (US) 4. 2840-01-347-8986 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-347-8986 RQST Updated Every Day 2840-01-347-8986 RQST NE Related Documents

2840-01-347-8986 Demil Restrictions 2840-01-347-8986

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

2840-01-347-8986 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.

2840-01-347-8986 HTS and ScheduleB Import and Export 2840-01-347-8986

2840-01-347-8986 End Users End Users 2840-01-347-8986

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

2840-01-347-8986 Manufacturers Approved Sources 2840-01-347-8986

2840-01-347-8986 Technical Data Datasheet 2840-01-347-8986

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Pacer Dawn
Criticality Code Justification [CRTL]
Agav
Design Type [APGF]
Compressor
Diameter [ABMZ]
15.750 Inches Minimum And 15.770 Inches Maximum
Engine Section Location [CZBJ]
Intermediate Pressure Compressor
Material [MATT]
Titanium Alloy Overall
Material Document And Classification [MDCL]
Ems55464 Assn Std Single Material Response Overall
Overall Length [ABHP]
0.605 Inches Minimum And 0.610 Inches Maximum
Stage Number [CZCJ]
3

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2840-01-347-8986 Freight Data Freight Information 2840-01-347-8986

2840-01-347-8986 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-347-8986 has a variance between NMFC and UFC when transported by rail and the description should be consulted.