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2840-01-238-3618

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840012383618 012383618 2185242

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

2840-01-238-3618 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840012383618 012383618

Managed by United States
NSN Created on 13 Aug 1986
Data Last Changed
November 2023
NATO Update Count
7
NATO Data Quality
2840-01-238-3618 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840012383618 012383618 1/1
NSN 2840-01-238-3618 (Generic Image) 1/1

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2840-01-238-3618 Related Documents Related Documents 2840-01-238-3618 5+ Documents (More...)

United States (US) 4. 2840-01-238-3618 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-238-3618 RQST Updated Every Day 2840-01-238-3618 RQST NE Related
2840012383618 012383618,2185242 117-4851 2840-21-921-4452 2840-00-730-5237 2840-14-484-7930 2840
921-4459 2840219214459 219214459,3056418CL09 2840-21-921-4459 2840-21-921-6144 2840-01-397-7192 2840012383618
921-6144 2840219216144 219216144,3055476CL09 2840-21-921-4459 2840-21-921-6144 2840-01-397-7192 2840012383618
013379543,307165-5 896-4124 2840008964124 008964124 730-5237 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-238-3618
921-44592840219214459 219214459,3056418CL09 2840-21-921-4459 2840-21-921-6144 2840-01-397-7192 2840012383618
009944729,473495 730-5237 2840-14-484-7930 2840-21-921-4459 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-238-3618
2840012383618 012383618,2185242 2840-01-397-7192 2840013977192 013977192,3070165-7 009944729,473495
009944729,473495 730-5237 2840-14-484-7930 2840-21-921-4459 2840-21-921-6144 2840-01-397-7192 2840012383618
012383618,2185242 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-238-3618 2840012383618 012383618,2185242
009944729,473495 730-5237 2840-14-484-7930 2840-21-921-4459 2840 -21-921-6144 2840-01-397-7192 2840012383618
921-6144 2840219216144 219216144,3055476CL09 2840-21-921-4459 2840-21-921-6144 2840-01-397-7192 2840012383618

2840-01-238-3618 Demil Restrictions 2840-01-238-3618

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

2840-01-238-3618 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.

2840-01-238-3618 Manufacturers Approved Sources 2840-01-238-3618

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