2840-15-207-0122
Aircraft Gas Turbine Engine Turbine Shroud Segment
2840152070122 152070122 6068T35G16 (241)A34606068T35G16
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 Italy
NSN Created on 8 Aug 2012
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-15-207-0122
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Related Documents 2840-15-207-0122 1+ Documents (More...)
6068T35G16 (241)A34606068T35G16 A stationary arched metal segment used to establish clearance and a
RQST NE Updated Every Day 2840-15-207-0122 RQST Updated Every Day 2840-15-207-0122 RQST NE Related Documents
152070122,6068T35G16 6068T35G16 (241)A34606068T35G16 A stationary arched metal segment used to establish
RQST NE Updated Every Day 2840-15-207-0122 RQST Updated Every Day 2840-15-207-0122 RQST NE Related Documents
152070122,6068T35G16 6068T35G16 (241)A34606068T35G16 A stationary arched metal segment used to establish
Restrictions 2840-15-207-0122
End Users 2840-15-207-0122
- Italy (ZR)
Approved Sources 2840-15-207-0122
- Part Number
- Manufacturer
- Status
- 6068T35G16
- Manufacturer
- A3460 - Ge Avio Srl (Active)
- Primary Buy
- Primary Buy
- (241)A34606068T35G16
- A3460 - Ge Avio Srl (Active)
- Secondary Buy
- Secondary Buy
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