2840-99-343-2002
Aircraft Gas Turbine Engine Turbine Nozzle Assembly
2840993432002 993432002 NJ193160
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 United Kingdom
NSN Created on 28 Aug 2013
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-99-343-2002
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Related Documents 2840-99-343-2002 1+ Documents (More...)
NJ193160 A stationary item designed for the purpose of directing air at the proper angle and velocity
RQST NE Updated Every Day 2840-99-343-2002 RQST Updated Every Day 2840-99-343-2002 RQST NE Related Documents
,NJ193160 NJ193160 A stationary item designed for the purpose of directing air at the proper angle and
RQST NE Updated Every Day 2840-99-343-2002 RQST Updated Every Day 2840-99-343-2002 RQST NE Related Documents
,NJ193160 NJ193160 A stationary item designed for the purpose of directing air at the proper angle and
Restrictions 2840-99-343-2002
End Users 2840-99-343-2002
- Belgium (ZB)
Approved Sources 2840-99-343-2002
- Part Number
- Manufacturer
- Status
- NJ193160
- Manufacturer
- K0378 - Rolls-Royce Plc (Active)
- Primary Buy
- Primary Buy
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