General Electric CT7-8A
Exact General Electric CT7-8A turboshaft model within the CT7-8 line. EASA and FAA-adopted airworthiness records identify the exact suffix; this identity-only packet does not infer a family link, actor IDs, S-92 installation, or lineage edge.
Identity
- Aliases
- CT7-8AGE CT7-8AGeneral Electric CT7-8A
- Domains
- aviation
- Identity Level
- variant
- Kind
- turboshaft
- Name
- General Electric CT7-8A
- Status
- unknown
Details
- Description
- Exact General Electric CT7-8A turboshaft model within the CT7-8 line. EASA and FAA-adopted airworthiness records identify the exact suffix; this identity-only packet does not infer a family link, actor IDs, S-92 installation, or lineage edge.
Links
- Official Url
- https://ad.easa.europa.eu/ad/US-2024-06-51
Assets & Meta
- Creation Time
- August 8, 2026 at 07:33:37 UTC
- Updated Time
- August 8, 2026 at 07:33:37 UTC
Other
- Sources
- Accessed Date
- 2026-08-08
- Note
- Current EASA-adopted safety publication explicitly lists General Electric CT7-8A among the affected engine models.
- Publisher
- European Union Aviation Safety Agency
- Title
- US-2024-06-51 Engine — CT7-8A
- Accessed Date
- 2026-08-08
- Note
- Official EASA safety publication independently enumerates CT7-8A alongside CT7-8, CT7-8A1, CT7-8E, and CT7-8F5.
- Publisher
- European Union Aviation Safety Agency
- Title
- US-2011-19-03 CT7-8 Turboshaft Engine
- Accessed Date
- 2026-08-08
- Note
- Official EASA aircraft noise record identifies General Electric CT7-8A as the engine type designation for S-92A, but this packet intentionally does not create that installation relationship.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.IM.R.001 S-92A noise TCDSN — CT7-8A