2840-21-878-3506
Aircraft Gas Turbine Engine Turbine Nozzle
2840218783506 218783506 3010262CL13-2
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 Canada
NSN Created on 13 Jun 1978
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-21-878-3506
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Related Documents 2840-21-878-3506 1+ Documents (More...)
3010262CL13-2 A single stationary item designed for the purpose of directing air at the proper angle
RQST NE Updated Every Day 2840-21-878-3506 RQST Updated Every Day 2840-21-878-3506 RQST NE Related Documents
2840-21-878-3506 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-878-3506
RQST NE Updated Every Day 2840-21-878-3506 RQST Updated Every Day 2840-21-878-3506 RQST NE Related Documents
2840-21-878-3506 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-878-3506
Restrictions 2840-21-878-3506
Approved Sources 2840-21-878-3506
- Part Number
- Manufacturer
- Status
- 3010262CL13-2
- Manufacturer
- 00198 - Pratt & Whitney Canada Corp (Active)
- Primary Buy
- Primary Buy
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