2840-12-327-4310
Turbo-Shaft Aircraft Engine
2840123274310 123274310 LN32392-GCM28835
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 Germany
NSN Created on 22 Jan 1992
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 2840-12-327-4310 2+ Documents (More...)
LN32392-GCM28835 A continuous-combustion type engine, may be with or without container, designed to
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Turbo-Shaft Aircraft Engine 2840123274310 JavaScript in your web browser . 2840-12-327-4310Turbo-Shaft
Aircraft Engine2840123274310 123274310 LN32392 Restrictions 2840-99-742-1392 DEMIL: | DEMILI : | CRITICALITY
Turbo-Shaft Aircraft Engine 2840123274310 JavaScript in your web browser . 2840-12-327-4310Turbo-Shaft
Aircraft Engine2840123274310 123274310 LN32392 Restrictions 2840-99-742-1392 DEMIL: | DEMILI : | CRITICALITY
Restrictions 2840-12-327-4310
End Users 2840-12-327-4310
- Germany (ZG)
Approved Sources 2840-12-327-4310
- Part Number
- Manufacturer
- Status
- LN32392-GCM28835
- Manufacturer
- D0272 - Rolls-Royce Deutschland Ltd & Co Kg (Active)
- Primary Buy
- Primary Buy
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