General Electric CF34-10E5
General Electric CF34-10E5 exact turbofan variant in the CF34-10E series. EASA rates normal five-minute takeoff thrust at 77.35 kN (17,390 lbf), maximum takeoff thrust at 83.72 kN (18,820 lbf), and maximum continuous thrust at 75.80 kN (17,040 lbf). EASA records 31 March 2006 type certification for the CF34-10E5/10E5A1/10E6/10E6A1 group, and a current 2025 safety publication covers CF34-10E5. No exact aircraft-family installation or service-entry date is asserted here without a source-specific record.
Identity
- Aliases
- CF34-10E5GE CF34-10E5General Electric CF34-10E5
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- General Electric CF34-10E5
- Status
- active
Details
- Air Breathing Specs
- Max Thrust Kn
- 83.72
- Sea Level Static Thrust Kn
- 77.35
- Description
- General Electric CF34-10E5 exact turbofan variant in the CF34-10E series. EASA rates normal five-minute takeoff thrust at 77.35 kN (17,390 lbf), maximum takeoff thrust at 83.72 kN (18,820 lbf), and maximum continuous thrust at 75.80 kN (17,040 lbf). EASA records 31 March 2006 type certification for the CF34-10E5/10E5A1/10E6/10E6A1 group, and a current 2025 safety publication covers CF34-10E5. 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 02:50:00 UTC
- Updated Time
- August 21, 2026 at 15:22:08 UTC
Other
- Sources
- Accessed Date
- 2026-08-21
- Note
- EASA type-certificate material identifies CF34-10E5 as an exact model and records 31 March 2006 type certification for the CF34-10E5/10E5A1/10E6/10E6A1 group; it provides the variant's normal takeoff, maximum takeoff, and maximum continuous 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 CF34-10E5 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