Back to Propulsion Systems

SNECMA M53-5

SNECMA M53-5 turbofan variant derived from M53-2 by modified settings, with 9,000 kgp takeoff afterburning thrust; Safran records it as the version fitted to production aircraft, and Safran’s corporate history identifies SNECMA as the predecessor of Safran Aircraft Engines. Current M53-5-specific lifecycle is not asserted.

Identity

Aliases
M53-5SNECMA M53-5Safran M53-5
Domains
aviation
Identity Level
variant
Kind
turbofan
Name
SNECMA M53-5
Status
unknown

Details

Air Breathing Specs
Afterburning Thrust
…
Description
SNECMA M53-5 turbofan variant derived from M53-2 by modified settings, with 9,000 kgp takeoff afterburning thrust; Safran records it as the version fitted to production aircraft, and Safran’s corporate history identifies SNECMA as the predecessor of Safran Aircraft Engines. Current M53-5-specific lifecycle is not asserted.
Family
Lineage
Manufacturers

Links

Assets & Meta

Creation Time
August 14, 2026 at 21:52:08 UTC
Updated Time
August 15, 2026 at 10:11:25 UTC

Other

Sources