The Learjet 25 was originally powered by a pair of General Electric CJ610-4 turbojets engines rated at 2,850lbs of thrust each. Later variants included the 25D and 25G, powered by the CJ610-8A engine rated at 2,950lbs. of thrust each. Inspection interval on the -8A engines is 5,000 hours. The Learjet 25D is normally configured for six passengers in a seating arrangement consisting of four individual forward facing seats, and a full-width bench seat aft of these.
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The Learjet 25D has a range of 1,014 nautical miles. Type in your city or airport identifier for a visual representation of the NBAA IFR Range (NM) for this aircraft.