2840-99-840-6414
Aircraft Gas Turbine Engine Turbine Shroud Segment
2840998406414 998406414 A17761-241-2 956.016.394.0
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
Managed by United Kingdom
NSN Created on 23 Oct 2013
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-99-840-6414
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A17761-241-2 956.016.394.0 A stationary arched metal segment used to establish clearance and a seal
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A17761 -241-2 A17761-241- Reactor 5950004222489 004222489,8551490-1 vendors Request Updated https//www.nsnlookup.com
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A17761 -241-2 A17761-241- Reactor 5950004222489 004222489,8551490-1 vendors Request Updated https//www.nsnlookup.com
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us 5950-00-422-2489 Reactor 5950004222489 004222489,8551490-1 Turbine Shroud Segment2840998406414 998406414
Restrictions 2840-99-840-6414
End Users 2840-99-840-6414
- France (ZF)
Approved Sources 2840-99-840-6414
- Part Number
- Manufacturer
- Status
- A17761-241-2
- Manufacturer
- K1209 - Cross Manufacturing Company (1938) (Active)
- Primary Buy
- Primary Buy
- 956.016.394.0
- F0228 - Safran Helicopter Engines (Active)
- Secondary Buy
- Secondary Buy
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