2840-20-005-5431
Turbo-Shaft Aircraft Engine
2840200055431 200055431 3053007-01
A continuous-combustion type engine, may be with or without container, designed to use superheated air to drive a turbine rotor which is connected to the rotorshaft of a helicopter by way of reduction gears. View more Turbo-Shaft Aircraft Engine
Managed by Canada
NSN Created on 6 May 2010
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-20-005-5431
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RQST NE Updated Every Day 2840-20-005-5431 RQST Updated Every Day 2840-20-005-5431 RQST NE Related Documents
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Request Updated Every Day 2840-20-005-5431 RQST NE Updated Every Day 2840-20-005-5431 RQST Updated Every
Restrictions 2840-20-005-5431
End Users 2840-20-005-5431
- Italy (ZR)
Approved Sources 2840-20-005-5431
- Part Number
- Manufacturer
- Status
- 3053007-01
- Manufacturer
- 00198 - Pratt & Whitney Canada Corp (Active)
- Primary Buy
- Primary Buy
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