General Electric CF34-10E7
General Electric CF34-10E7 exact turbofan variant in the CF34-10E series. EASA rates normal five-minute takeoff thrust at 83.72 kN (18,820 lbf), maximum takeoff thrust at 90.57 kN (20,360 lbf), and maximum continuous thrust at 75.80 kN (17,040 lbf). EASA records 1 August 2006 type certification for the CF34-10E2A1/10E7 group, and a current 2025 safety publication covers CF34-10E7. The canonical installation index records this exact variant on the first-generation Embraer E195 branch, consistent with GE's CF34-10E family-level E190/195 application statement; no exact service-entry date is asserted here.
Identity
- Aliases
- CF34-10E7GE CF34-10E7General Electric CF34-10E7
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- General Electric CF34-10E7
- Status
- active
Details
- Air Breathing Specs
- Max Thrust Kn
- 90.57
- Sea Level Static Thrust Kn
- 83.72
- Description
- General Electric CF34-10E7 exact turbofan variant in the CF34-10E series. EASA rates normal five-minute takeoff thrust at 83.72 kN (18,820 lbf), maximum takeoff thrust at 90.57 kN (20,360 lbf), and maximum continuous thrust at 75.80 kN (17,040 lbf). EASA records 1 August 2006 type certification for the CF34-10E2A1/10E7 group, and a current 2025 safety publication covers CF34-10E7. The canonical installation index records this exact variant on the first-generation Embraer E195 branch, consistent with GE's CF34-10E family-level E190/195 application statement; no exact service-entry date is asserted here.
- Developers
- Family
- Manufacturers
Links
- Official Url
- https://www.easa.europa.eu/en/downloads/7761/en
Assets & Meta
- Creation Time
- August 7, 2026 at 02:40:36 UTC
- Updated Time
- August 21, 2026 at 15:32:52 UTC
Other
- Sources
- Accessed Date
- 2026-08-21
- Note
- EASA type-certificate material names CF34-10E7 as an exact engine model, records 1 August 2006 type certification for the CF34-10E2A1/10E7 group, and provides this variant's 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
- 2026-08-06
- Note
- EASA safety material independently enumerates CF34-10E7 and CF34-10E7-B within the CF34-10 series; this source does not assert an aircraft installation.
- Publisher
- European Union Aviation Safety Agency
- Title
- US-2018-19-22 Engine safety publication
- Accessed Date
- 2026-08-21
- Note
- EASA's 21 August 2025 safety publication explicitly includes CF34-10E7 in its applicability, supporting an active lifecycle status; it does not establish an exact service-entry date.
- Publisher
- European Union Aviation Safety Agency
- Title
- US-2025-14-03 Engine safety publication
- Accessed Date
- 2026-08-21
- Note
- GE identifies the CF34-10E family as powering Embraer 190/195 aircraft; this supports the family-level E195 application and is not treated as proof that every CF34-10E subvariant has the same installation.
- Publisher
- GE Aerospace
- Title
- CF34 Engine Family