Aerospace Garage

PRODUCT PROFILE

LEAP-1A

CFM International LEAP-1A
Photo: Actualcpscm / Wikimedia Commons · CC BY-SA 4.0

HIGH-BYPASS TURBOFAN ENGINE

LEAP-1A

France / United States · verified

MAKER

CFM International →cfmaeroengines.comlast verified 6 Sept 2026
COUNTRY
France / United States
PROGRAMME STATUS
verified

Specifications

Function
Provides primary propulsion and pneumatic power for narrow-body commercial transport aircraft.
Architecture
Twin-spool turbofan featuring a 1-stage fan and a 10-stage high-pressure compressor.
Platform fit
The engine is designed exclusively for the Airbus A320neo family of aircraft.
Commercial model
Typically sold through direct procurement or long-term power-by-the-hour maintenance contracts.
Deployment status
The product is in full-rate production with thousands of units currently in active commercial service.
Evidence to demand
Public order books show a substantial multi-year backlog from major global airlines and lessors.

Description

The LEAP-1A is a high-bypass turbofan engine developed by CFM International, a 50/50 joint venture between GE Aerospace and Safran Aircraft Engines (Safran SA). It serves as the successor to the CFM56 series, incorporating ceramic matrix composites and 3D-printed fuel nozzles to improve thermal efficiency and fuel burn. The engine was designed specifically to power the latest generation of narrow-body commercial aircraft, focusing on reduced carbon emissions and noise profiles compared to legacy powerplants. Primary buyers are commercial airlines and global aircraft leasing firms who operate the Airbus A320neo family. It is sold either as part of a direct airframe purchase or through long-term Flight Hour Services agreements. Major operators include Indigo, American Airlines, and EasyJet. The engine competes directly with the Pratt & Whitney PW1100G-JM, maintaining a significant share of the A320neo market due to its conventional architecture and high dispatch reliability. The Garage desk notes that while the engine avoids the geared architecture risks of its competitor, it has faced its own durability challenges in harsh environments, particularly regarding high-pressure turbine shroud degradation. Buyers should verify the current status of service bulletins related to the Reverse Bleed System and monitor the availability of MRO slots, as global shop capacity remains constrained. We would also confirm the specific thrust rating configuration, as this is software-defined to match the specific A320, A321, or A319 airframe requirements.

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LAST VERIFIED

6 Sept 2026

SOURCE CITATION

Maker website on record

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