General Electric CF34-8E2
General Electric CF34-8E2 exact turbofan variant in the CF34-8 series. EASA rates normal five-minute takeoff thrust at 55.20 kN (12,410 lbf), maximum takeoff thrust at 59.16 kN (13,300 lbf), and maximum continuous thrust at 55.78 kN (12,540 lbf). FAA airworthiness material independently confirms the CF34-8E2 designation within the GE CF34-8 family; no exact aircraft-family installation is asserted here without a source-specific relationship.
Identity
- Aliases
- CF34-8E2General Electric CF34-8E2GE CF34-8E2CF34-8E2 turbofan
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- General Electric CF34-8E2
- Status
- active
Details
- Air Breathing Specs
- Max Thrust
- …
- Sea Level Static Thrust
- …
- Description
- General Electric CF34-8E2 exact turbofan variant in the CF34-8 series. EASA rates normal five-minute takeoff thrust at 55.20 kN (12,410 lbf), maximum takeoff thrust at 59.16 kN (13,300 lbf), and maximum continuous thrust at 55.78 kN (12,540 lbf). FAA airworthiness material independently confirms the CF34-8E2 designation within the GE CF34-8 family; no exact aircraft-family installation is asserted here without a source-specific relationship.
- Developers
- Family
- Manufacturers
Links
Assets & Meta
- Creation Time
- August 13, 2026 at 07:39:54 UTC
- Updated Time
- August 21, 2026 at 15:08:27 UTC
Other
- Sources
- Accessed Date
- 2026-08-13
- Note
- EASA CF34-8 series TCDS lists CF34-8E2 as a distinct approved model under the General Electric CF34-8 type certificate.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.IM.E.053 — CF34-8 series engines
- Accessed Date
- 2026-08-13
- Note
- FAA airworthiness material applies to the CF34-8E2 model, independently confirming the exact designation boundary.
- Publisher
- Federal Aviation Administration
- Title
- Airworthiness Directives; General Electric CF34-8 series
- Accessed Date
- 2026-08-21
- Note
- EASA TCDS IM.E.053 lists CF34-8E2 ratings of 55.20 kN (12,410 lbf) normal five-minute takeoff, 59.16 kN (13,300 lbf) maximum takeoff, and 55.78 kN (12,540 lbf) maximum continuous thrust.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.IM.E.053 — CF34-8 series engines
- Accessed Date
- 2026-08-21
- Note
- EASA safety material lists CF34-8E2 among the exact GE CF34-8 models covered by the applicable airworthiness action.
- Publisher
- European Union Aviation Safety Agency
- Title
- US-2021-26-19 — CF34-8 series airworthiness directive
- Accessed Date
- 2026-08-21
- Note
- Current GE Aerospace technical-manual index lists CF34-8E engine manuals, supporting ongoing service support for the family.
- Publisher
- GE Aerospace
- Title
- Technical Manuals Index