General Electric F414 Engine

F414-GE-400 is a turbofan engine developed and manufactured by General Electric (GE). This engine is used in the U.S. Navy’s F/A-18E/F Super Hornet fighter aircraft and EA-18G Growler electronic warfare aircraft. Built upon the successful design of the F404 engine family, the F414-GE-400 provides approximately 35 percent more thrust than the F404. This increase has significantly enhanced the aircraft’s range, payload capacity and survivability, thereby improving its multirole mission capabilities.

F414-GE-400 Turbofan Engine (

Design and Performance Characteristics

The F414-GE-400 is a low-bypass-ratio, afterburning turbofan engine. Designed with a modular structure, it is optimized for ease of maintenance, interchangeable modules and operational flexibility. Thanks to the Full Authority Digital Electronic Control (FADEC) system, the engine’s operational characteristics are digitally managed, enhancing operational precision and fuel efficiency.

The engine’s key technical specifications are as follows:

• Maximum thrust (with afterburner): 22,000 lbf (98 kN)
• Pressure ratio: 30:1
• Thrust-to-weight ratio: 9:1
• Airflow rate: 170 lb/s (77.1 kg/s)
• Length: 154 in (391 cm)
• Inlet diameter: Approximately 31–32 in (79–81 cm)

Modular Structure and Maintenance Process

The F414-GE-400 engine consists of six distinct modules: the fan module, high-pressure compressor (HPC), combustor, high-pressure turbine (HPT), low-pressure turbine (LPT), and afterburner module. This modular design accelerates maintenance and repair processes. The modules do not need to be matched to each other, providing flexibility during component replacement.

• Fan Module: Features a three-stage axial-flow design and directs approximately 80 percent of the airflow as bypass air.
• HPC: A seven-stage compressor incorporating advanced 3D aerodynamic profiles and high-strength materials.
• HPT and LPT: Drive the HPC and fan module respectively via a common shaft; manufactured using modern cooling techniques and single-crystal alloys.
• Afterburner Module: Injects fuel directly into the exhaust stream to generate additional thrust. Repair capability for this module is available only at the Fleet Readiness Center (FRC) West in NAS Lemoore.

F414-GE-400 Modular Structure (NPS)

Usage and Logistics Support

F414-GE-400 engines are operated by carrier-based air wings, with maintenance conducted under a three-level system: organizational level (unit-level maintenance), intermediate level (Intermediate Maintenance Activity – IMA), and depot level (Depot Maintenance). The FRC West at Naval Air Station Lemoore serves as the primary maintenance center for this engine. The unit at Lemoore is responsible for disassembly, inspection, reassembly and testing of the engines. More advanced module repairs are carried out at the FRC Southeast facility in Jacksonville, Florida.

Forecasting and Logistics Planning

The maintenance and replacement needs of F414-GE-400 engines are predicted based on factors such as flight hours, age and operational load. Data such as Engine Operating Time (EOT) and Life Usage Index (LUI) are utilized in this process. These data, collected via the Integrated Engine Condition Assessment and Monitoring System (IECAMS) integrated into the aircraft, are analyzed after every flight and fed into logistics decision-making processes.

International Use and Development

The F414-GE-400 engine is also employed in several international programs beyond the U.S. Navy. The Indian Tejas MkII fighter aircraft program has selected the F414-INS6 variant, while Saab has developed the F414G single-engine variant for its Gripen E/F platform.