General Electric CF34-8E6A1
General Electric CF34-8E6A1 exact turbofan variant in the CF34-8 series. EASA rates normal five-minute takeoff thrust at 62.50 kN (14,050 lbf), maximum takeoff thrust at 62.50 kN (14,050 lbf), and maximum continuous thrust at 60.14 kN (13,520 lbf). EASA safety material independently lists CF34-8E6A1 among the exact GE CF34-8 models; no exact aircraft-family installation is asserted here without a source-specific relationship.
Identity
- Aliases
- CF34-8E6A1General Electric CF34-8E6A1GE CF34-8E6A1CF34-8E6A1 turbofan
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- General Electric CF34-8E6A1
- Status
- active
Details
- Air Breathing Specs
- Max Thrust
- …
- Sea Level Static Thrust
- …
- Description
- General Electric CF34-8E6A1 exact turbofan variant in the CF34-8 series. EASA rates normal five-minute takeoff thrust at 62.50 kN (14,050 lbf), maximum takeoff thrust at 62.50 kN (14,050 lbf), and maximum continuous thrust at 60.14 kN (13,520 lbf). EASA safety material independently lists CF34-8E6A1 among the exact GE CF34-8 models; 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 07:47:57 UTC
- Updated Time
- August 21, 2026 at 15:07:09 UTC
Other
- Sources
- Accessed Date
- 2026-08-13
- Note
- EASA CF34-8 series TCDS lists CF34-8E6A1 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
- The official CF34-8 series type-certificate record is the authoritative model-identity source for this exact variant.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA CF34-8 series type certificate
- Accessed Date
- 2026-08-21
- Note
- EASA TCDS IM.E.053 lists CF34-8E6A1 ratings of 62.50 kN (14,050 lbf) normal five-minute takeoff, 62.50 kN (14,050 lbf) maximum takeoff, and 60.14 kN (13,520 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 publication explicitly lists CF34-8E6A1 among the exact GE CF34-8 models covered by the combustion-chamber inspection action.
- Publisher
- European Union Aviation Safety Agency
- Title
- US-2025-12-08 — Turbine Engine - Combustion Chamber Assembly - Inspection
- 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