2995-14-553-8237
Turbine Engine Supervisory Control Unit
2995145538237 145538237 S732A10A1004 HEC400-03AC 10184002
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 23 May 2007
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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S732A10A1004 HEC400-03AC 10184002 An electronic unit that continously monitors engine speed, temperature
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Turbine Engine Supervisory Control Unit Supervisory Control Unit2995145538237 145538237 https//
Turbine Engine Supervisory Control Unit Supervisory Control Unit2995145538237 145538237 https//
319-1772 Degiv Prise Manchon 0000241220RNCC: 3 | RNVC: 2 | DAC: 4 1 Jan 1975 2995-14-251-3278 2995-14-553-8237
Restrictions 2995-14-553-8237
End Users 2995-14-553-8237
- Finland (WF)
- Australia (ZA)
- Belgium (ZB)
- New Zealand (ZE)
- France (ZF)
- Germany (ZG)
- Netherlands (ZN)
Approved Sources 2995-14-553-8237
- Part Number
- Manufacturer
- Status
- S732A10A1004
- Manufacturer
- F0210 - Airbus Helicopters (Ets De (Active)
- Source Control
- Source Control
- HEC400-03AC
- U4287 - Rolls-Royce Controls And Data (Active)
- Primary Buy
- Primary Buy
- 10184002
- A486G - Nimikkeistokeskus Ncb Finland (Active)
- NATO Reference
- NATO Reference
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