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2840-01-360-4046

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840013604046 013604046 3091604-2

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

2840-01-360-4046 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013604046 013604046

Managed by United States
NSN Created on 23 Jun 1992
Data Last Changed
January 2023
NATO Update Count
8
NATO Data Quality
2840-01-360-4046 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013604046 013604046 1/1
NSN 2840-01-360-4046 (Generic Image) 1/1

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2840-01-360-4046 Related Documents Related Documents 2840-01-360-4046 1+ Documents (More...)

3091604-2 A stationary arched metal segment used to establish clearance and a seal for the tip of a
United States (US) 4. 2840-01-360-4046 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-360-4046 RQST Updated Every Day 2840-01-360-4046 RQST NE Related Documents

2840-01-360-4046 Demil Restrictions 2840-01-360-4046

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

2840-01-360-4046 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.

2840-01-360-4046 HTS and ScheduleB Import and Export 2840-01-360-4046

2840-01-360-4046 End Users End Users 2840-01-360-4046

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

2840-01-360-4046 Manufacturers Approved Sources 2840-01-360-4046

2840-01-360-4046 Technical Data Datasheet 2840-01-360-4046

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Pacer Dawn
Criticality Code Justification [CRTL]
Agav
Design Type [APGF]
Compressor
Diameter [ABMZ]
14.370 Inches Minimum And 14.390 Inches Maximum
Engine Section Location [CZBJ]
Compressor
Material [MATT]
Nickel Alloy Overall
Material Document And Classification [MDCL]
Ems55464 Assn Std Single Material Response Overall
Overall Length [ABHP]
0.735 Inches Minimum And 0.740 Inches Maximum
Stage Number [CZCJ]
4

2840-01-360-4046 Related Items NATO Stock Numbers Related to 2840-01-360-4046

2840-01-360-4046 Freight Data Freight Information 2840-01-360-4046

2840-01-360-4046 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-360-4046 has a variance between NMFC and UFC when transported by rail and the description should be consulted.