CFM International CFM56-7B26/3B1F
Exact CFM International CFM56-7B26/3B1F high-bypass turbofan in the CFM56-7B TI model group. EASA E.004 lists 11,699 daN take-off thrust and 11,521 daN maximum continuous thrust for this TI rating group; take-off thrust is normalized to 116.99 kN in airBreathingSpecs. No vehicle installation or unsupported sibling/lineage relationship is inferred.
Identity
- Aliases
- CFM56-7B26/3B1FCFM56-7B26-3B1FCFM International CFM56-7B26/3B1F
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbofan
- Name
- CFM International CFM56-7B26/3B1F
- Status
- active
Details
- Air Breathing Specs
- Max Thrust Kn
- 116.99
- Sea Level Static Thrust Kn
- 116.99
- Description
- Exact CFM International CFM56-7B26/3B1F high-bypass turbofan in the CFM56-7B TI model group. EASA E.004 lists 11,699 daN take-off thrust and 11,521 daN maximum continuous thrust for this TI rating group; take-off thrust is normalized to 116.99 kN in airBreathingSpecs. No vehicle installation or unsupported sibling/lineage relationship is inferred.
- Developers
- Family
- Manufacturers
Links
- Official Url
- https://www.easa.europa.eu/en/downloads/7795/en
Assets & Meta
- Creation Time
- August 7, 2026 at 09:48:21 UTC
- Updated Time
- August 21, 2026 at 13:06:47 UTC
Other
- Sources
- Accessed Date
- 2026-08-21
- Note
- EASA E.004 Issue 07 lists CFM56-7B26/3B1F in the TI model group with 11,699 daN take-off thrust and groups it at 11,521 daN maximum continuous thrust; take-off thrust is normalized to 116.99 kN in airBreathingSpecs.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA E.004 — CFM56-7B series engine type-certificate data sheet, Issue 07
- Accessed Date
- 2026-08-07
- Note
- The regulatory type-acceptance report lists CFM56-7Bxx/3B1F 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