General Electric CF34-10E2A1
General Electric CF34-10E2A1 exact turbofan variant in the CF34-10E series. EASA rates normal five-minute takeoff thrust at 75.44 kN (16,960 lbf), maximum takeoff thrust at 75.44 kN (16,960 lbf), and maximum continuous thrust at 67.21 kN (15,110 lbf). EASA records 1 August 2006 type certification for the CF34-10E2A1/10E7 group, and a current 2025 safety publication covers CF34-10E2A1. No exact aircraft-family installation or service-entry date is asserted here without a source-specific record.
Identity
- Aliases
- CF34-10E2A1GE CF34-10E2A1General Electric CF34-10E2A1
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- General Electric CF34-10E2A1
- Status
- active
Details
- Air Breathing Specs
- Max Thrust Kn
- 75.44
- Sea Level Static Thrust Kn
- 75.44
- Description
- General Electric CF34-10E2A1 exact turbofan variant in the CF34-10E series. EASA rates normal five-minute takeoff thrust at 75.44 kN (16,960 lbf), maximum takeoff thrust at 75.44 kN (16,960 lbf), and maximum continuous thrust at 67.21 kN (15,110 lbf). EASA records 1 August 2006 type certification for the CF34-10E2A1/10E7 group, and a current 2025 safety publication covers CF34-10E2A1. No exact aircraft-family installation or service-entry date is asserted here without a source-specific record.
- Developers
- Family
- Manufacturers
Links
- Official Url
- https://www.easa.europa.eu/en/downloads/7761/en
Assets & Meta
- Creation Time
- August 7, 2026 at 02:43:39 UTC
- Updated Time
- August 21, 2026 at 15:36:44 UTC
Other
- Sources
- Accessed Date
- 2026-08-21
- Note
- EASA type-certificate material names CF34-10E2A1 as an exact engine model, records 1 August 2006 type certification for the CF34-10E2A1/10E7 group, and provides its normal takeoff, maximum takeoff, and maximum continuous thrust ratings used here.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.IM.E.021 — GE CF34-10E series engines
- Accessed Date
- 2026-08-21
- Note
- EASA's 21 August 2025 safety publication explicitly includes CF34-10E2A1 in its applicability, supporting an active lifecycle status; it does not establish an aircraft-family installation or service-entry date.
- Publisher
- European Union Aviation Safety Agency
- Title
- US-2025-14-03 Engine safety publication