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The P-38J was followed by the P-38L, deliveries of which commenced in June, 1944, almost 4,000 were built by the end of hostilities. The P-38L was fitted with F-30 engines, delivering equal or better power to higher altitudes, and slightly larger fuel tanks, with booster pumps in the wings. Detail changes included the first tail warning radar in a fighter.
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The two Allison V-1710F-30 V-12s had a 5.5 in. bore and 6.0 in stroke, providing a compression ratio of 6.5. These drove Curtiss Electric constant speed props via a 2:1 reduction gear, delivering 1,475 HP military and takeoff ratings at 3,000 RPM, or 1,612 HP maximum rating at 3,000 RPM and 60 in. of manifold pressure. Some later engines are described as delivering up to 1,725 HP WEP rating. The engines required 100 octane or higher rated fuel, and had 13 USG oil capacity. The oil was cooled in two outboard chin core radiators, vented via automatically controlled flaps on either side of the nacelle. Fuel consumption was 0.65 lb/HP./hr at 1,100 HP normal rating, at 2,600 RPM.