Turmo IV C
Safran Helicopter Engines TURMO IV C is a type-certified turboshaft in the TURMO IV series. EASA rates the model at 1,115 kW five-minute takeoff, 960 kW maximum continuous, and 1,160 kW two-and-a-half-minute contingency power, and documents SA 330 G/J Puma use plus return-to-service controls for engines previously operated by military or state users. Current lifecycle remains unknown.
Identity
- Aliases
- TURMO IV C
- Domains
- aviation
- Identity Level
- model
- Kind
- turboshaft
- Name
- Turmo IV C
- Status
- unknown
Details
- Air Breathing Specs
- Shaft Power Kw
- 1,115
- Description
- Safran Helicopter Engines TURMO IV C is a type-certified turboshaft in the TURMO IV series. EASA rates the model at 1,115 kW five-minute takeoff, 960 kW maximum continuous, and 1,160 kW two-and-a-half-minute contingency power, and documents SA 330 G/J Puma use plus return-to-service controls for engines previously operated by military or state users. Current lifecycle remains unknown.
- Developers
- Family
- Lineage
- Note
- EASA states that TURMO IV C engines can be created by converting TURMO III C4 engines.
- Related Propulsion System
- Relationship
- direct-derivative-of
- Sources
- Nested value
- Note
- EASA states that TURMO IV C engines can be created by converting TURMO IV B engines.
- Related Propulsion System
- Relationship
- direct-derivative-of
- Sources
- Nested value
- Manufacturers
Links
Assets & Meta
- Creation Time
- August 14, 2026 at 21:14:03 UTC
- Updated Time
- August 15, 2026 at 07:34:38 UTC
Other
- Sources
- Accessed Date
- 2026-08-14
- Note
- EASA lists Safran Helicopter Engines as manufacturer/type-certificate holder for the TURMO IV series; the linked TCDS download covers the exact series.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.E.074 - Turmo IV Series engines
- Accessed Date
- 2026-08-14
- Note
- The directive identifies TURMO IV C turboshaft engines, states they equip SA 330 G and SA 330 J PUMA helicopters, and distinguishes previously military/state-operated configurations requiring civil return-to-service controls.
- Published Date
- 2005-04-13
- Publisher
- European Union Aviation Safety Agency
- Title
- Airworthiness Directive F-2005-060 - TURMO IV C civil use
- Accessed Date
- 2026-08-15
- Note
- The EASA TURMO IV type-certificate sheet gives 1,115 kW five-minute takeoff, 960 kW maximum-continuous, and 1,160 kW two-and-a-half-minute contingency shaft-power ratings for the series/model.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.E.074 - Turmo IV Series engines TCDS
- Accessed Date
- 2026-08-15
- Note
- Airbus customer-support data names two TM Turmo IV C engines and 1,494 shp per engine for the SA330J Puma, corroborating the exact Puma application and power class.
- Publisher
- Airbus Helicopters
- Title
- Customer Support Directory 2023