General Electric CF34-8C5A3
General Electric CF34-8C5A3 exact turbofan variant in the CF34-8 series. EASA rates normal five-minute takeoff thrust at 64.54 kN (14,510 lbf), maximum takeoff thrust at 64.54 kN (14,510 lbf), and maximum continuous thrust at 60.84 kN (13,680 lbf). EASA and FAA safety material independently list CF34-8C5A3 among the exact GE CF34-8 models; no exact aircraft-family installation is asserted here without a source-specific relationship.
Identity
- Aliases
- CF34-8C5A3General Electric CF34-8C5A3GE CF34-8C5A3CF34-8C5A3 turbofan
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- General Electric CF34-8C5A3
- Status
- active
Details
- Air Breathing Specs
- Max Thrust
- …
- Sea Level Static Thrust
- …
- Description
- General Electric CF34-8C5A3 exact turbofan variant in the CF34-8 series. EASA rates normal five-minute takeoff thrust at 64.54 kN (14,510 lbf), maximum takeoff thrust at 64.54 kN (14,510 lbf), and maximum continuous thrust at 60.84 kN (13,680 lbf). EASA and FAA safety material independently list CF34-8C5A3 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 07:38:45 UTC
- Updated Time
- August 21, 2026 at 15:12:07 UTC
Other
- Sources
- Accessed Date
- 2026-08-13
- Note
- EASA CF34-8 series TCDS lists CF34-8C5A3 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
- 2026-08-21
- Note
- EASA TCDS IM.E.053 lists CF34-8C5A3 ratings of 64.54 kN (14,510 lbf) normal five-minute takeoff, 64.54 kN (14,510 lbf) maximum takeoff, and 60.84 kN (13,680 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 CF34-8C5A3 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
- EASA type-certificate material includes the CF34-8C5A3 model-list designation, independently confirming the exact variant boundary.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA CF34-8 series type certificate