CFM International CFM56-7B24/3B1
Exact CFM International CFM56-7B24/3B1 high-bypass turbofan in the CFM56-7B TI model group. EASA E.004 Issue 07 lists 10,765 daN take-off thrust and 10,142 daN maximum continuous thrust for CFM56-7B24/3B1; take-off thrust is normalized to 107.65 kN in airBreathingSpecs. Its canonical CFM56 family link, GE/Safran developers, CFM International manufacturer, and existing Boeing 737-family installation are preserved.
Identity
- Aliases
- CFM56-7B24/3B1CFM56-7B24-3B1CFM International CFM56-7B24/3B1
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- CFM International CFM56-7B24/3B1
- Status
- active
Details
- Air Breathing Specs
- Max Thrust Kn
- 107.65
- Sea Level Static Thrust Kn
- 107.65
- Description
- Exact CFM International CFM56-7B24/3B1 high-bypass turbofan in the CFM56-7B TI model group. EASA E.004 Issue 07 lists 10,765 daN take-off thrust and 10,142 daN maximum continuous thrust for CFM56-7B24/3B1; take-off thrust is normalized to 107.65 kN in airBreathingSpecs. Its canonical CFM56 family link, GE/Safran developers, CFM International manufacturer, and existing Boeing 737-family installation are preserved.
- Developers
- Family
- Manufacturers
Links
- Official Url
- https://www.easa.europa.eu/en/downloads/7795/en
Assets & Meta
- Creation Time
- August 7, 2026 at 09:50:14 UTC
- Updated Time
- August 21, 2026 at 14:00:28 UTC
Other
- Sources
- Accessed Date
- 2026-08-21
- Note
- EASA E.004 Issue 07 lists CFM56-7B24/3B1 in the TI take-off group with 10,765 daN take-off thrust and in the TI maximum continuous group with 10,142 daN; take-off thrust is normalized to 107.65 kN in airBreathingSpecs.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA E.004 Issue 07 — CFM International S.A. CFM56-7B series engines
- Accessed Date
- 2026-08-07
- Note
- The regulatory type-acceptance report lists CFM56-7Bxx/3B1 among covered TI variants and preserves the exact suffix boundary.
- Publisher
- Civil Aviation Authority of New Zealand
- Title
- Type Acceptance Report TAR 19/21B/9 — CFM56-7B Series