The Learjet 24E is an enhanced derivative of the Learjet 24 series, developed by Learjet as part of its ongoing improvements to the pioneering Model 23 and 24 light business jets. Introduced in the early 1970s, the 24E featured aerodynamic refinements and avionics updates aimed at improving performance and operational capability while retaining the sleek, high-speed profile that defined the brand.
The Learjet 24E first flew in 1976, with production spanning until 1977. It maintained the series’ hallmark of twin General Electric CJ610 turbojet engines, each producing 2,950 pounds of thrust, delivering a maximum cruise speed of approximately 514 knots. The 24E offered a maximum range of around 1,430 nautical miles, an MTOW of 13,500 pounds, and a takeoff distance of about 4,250 feet.
The cabin, configured for typical business use, seated up to six passengers. While compact compared to later light jets, the Learjet 24E’s interior provided executive seating and basic amenities suited to short- to medium-range corporate missions. Cabin volume measured about 123 cubic feet, with dimensions designed for quick point-to-point travel rather than extended comfort.
Operationally, the 24E maintained the Learjet reputation for high cruise speeds and direct routing capability. The aircraft’s improvements over earlier 24 models enhanced both climb performance and runway flexibility, making it a practical choice for business operators prioritizing speed and efficiency over large cabin space.
