2840-12-343-4571
Aircraft Gas Turbine Engine Turbine Nozzle Assembly
2840123434571 123434571 VG95211-ML-123434571 1AK0038G02
A stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Turbine Nozzle Assembly
Managed by Germany
NSN Created on 24 Jun 1997
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-12-343-4571
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Related Documents 2840-12-343-4571 1+ Documents (More...)
VG95211-ML-123434571 1AK0038G02 A stationary item designed for the purpose of directing air at the proper
Germany (DE) 4. 2840-12-343-4571 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 2840-12-343-4571 RQST Updated Every Day 2840-12-343-4571 RQST NE Related Documents
Germany (DE) 4. 2840-12-343-4571 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 2840-12-343-4571 RQST Updated Every Day 2840-12-343-4571 RQST NE Related Documents
Restrictions 2840-12-343-4571
End Users 2840-12-343-4571
- Germany (ZG)
Approved Sources 2840-12-343-4571
- Part Number
- Manufacturer
- Status
- VG95211-ML-123434571
- Manufacturer
- D3030 - Wehrtechnische Dienststelle Fur (Active)
- Definitive Standard
- Definitive Standard
- 1AK0038G02
- D3309 - Mtu Aero Engines Ag (Active)
- Primary Buy
- Primary Buy
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