2840-00-134-0014
Aircraft Gas Turbine Engine Turbine Nozzle
2840001340014 001340014 2-121-100-09
A single 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. View more Aircraft Gas Turbine Engine Turbine Nozzle
Managed by United States
NSN Created on 20 Sep 1968
Data Last Changed
November 2023
November 2023
NATO Update Count
13
13
NATO Data Quality
Marketplace 2840-00-134-0014
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Related Documents 2840-00-134-0014 1+ Documents (More...)
2-121-100-09 A single stationary item designed for the purpose of directing air at the proper angle
United States (US) 4. 2840-00-134-0014 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-00-134-0014 RQST Updated Every Day 2840-00-134-0014 RQST NE Related Documents
United States (US) 4. 2840-00-134-0014 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-00-134-0014 RQST Updated Every Day 2840-00-134-0014 RQST NE Related Documents
Restrictions 2840-00-134-0014
2840-00-134-0014 is a Aircraft Gas Turbine Engine Turbine Nozzle that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.
Approved Sources 2840-00-134-0014
- Part Number
- Manufacturer
- Status
- 2-121-100-09
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
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