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CFM International CFM56-5B9/P

Exact CFM International CFM56-5B9/P turbofan variant under the canonical CFM56 family. EASA TCDS E.003 Issue 06 lists 10,364 daN constant takeoff thrust below 45 °C (103.64 kN; 23,300 lbf) and 9,008 daN maximum continuous thrust below 25 °C (90.08 kN; 20,250 lbf). This record preserves the distinct certified /P variant boundary without asserting a specific aircraft installation or service-entry date.

Identity

Aliases
CFM56-5B9/PCFM56-5B9-PCFM International CFM56-5B9/P
Domains
aviation
Identity Level
variant
Kind
turbofan
Name
CFM International CFM56-5B9/P
Status
active

Details

Air Breathing Specs
Max Thrust Kn
103.64
Sea Level Static Thrust Kn
103.64
Description
Exact CFM International CFM56-5B9/P turbofan variant under the canonical CFM56 family. EASA TCDS E.003 Issue 06 lists 10,364 daN constant takeoff thrust below 45 °C (103.64 kN; 23,300 lbf) and 9,008 daN maximum continuous thrust below 25 °C (90.08 kN; 20,250 lbf). This record preserves the distinct certified /P variant boundary without asserting a specific aircraft installation or service-entry date.
Developers
Family
Manufacturers

Links

Assets & Meta

Creation Time
August 7, 2026 at 20:36:41 UTC
Updated Time
August 21, 2026 at 15:48:52 UTC

Other

Sources
  • Accessed Date
    2026-08-21
    Note
    EASA TCDS E.003 Issue 06 lists CFM56-5B9/P at 10,364 daN take-off/static thrust and 9,008 daN maximum continuous thrust; the take-off/static rating is normalized to 103.64 kN in airBreathingSpecs.
    Publisher
    European Union Aviation Safety Agency
    Title
    TCDS E.003 — CFM56-5B and CFM56-5C series engines
  • Accessed Date
    2026-08-21
    Note
    Manufacturer family reference supports the CFM56 turbofan identity; this packet keeps the certified CFM56-5B9/P variant boundary separate.
    Publisher
    CFM International
    Title
    CFM56 engine family