2995-14-549-1298
Turbine Engine Supervisory Control Unit
2995145491298 145491298 S732A10A1003 HEC400-02AC
An electronic unit that continously monitors engine speed, temperature, and air flow and adjusts the FUEL CONTROL, MAIN, TURBINE ENGINE to compensate for changes. Features may include load sharing capabilities, rotor speed governing, loss-of-load protection and analog or manual backup modes. It may contain automatic start capability or self-diagnostic circuitry. View more Turbine Engine Supervisory Control Unit
Managed by France
NSN Created on 2 Mar 2006
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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S732A10A1003 HEC400-02AC An electronic unit that continously monitors engine speed, temperature, and
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1988 2995-14-522-8735 Gas Turbine Engine Starter 086-12-01RNCC: 3 | RNVC: 2 | DAC: 2 6 Dec 2000 2995-14-549-1298
Restrictions 2995-14-549-1298
End Users 2995-14-549-1298
- France (ZF)
- Netherlands (ZN)
Approved Sources 2995-14-549-1298
- Part Number
- Manufacturer
- Status
- S732A10A1003
- Manufacturer
- F0210 - Airbus Helicopters (Ets De (Active)
- Source Control
- Source Control
- HEC400-02AC
- U4287 - Rolls-Royce Controls And Data (Active)
- Primary Buy
- Primary Buy
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