The F-30 is equipped with a dual
capacitor discharge ignition system and is free-air-cooled, with optional fan cooling. The cylinder walls are electrochemically coated with
Nikasil. Standard starting is electric start and
recoil start is not an option. The reduction drive system available is the G-40 gearbox with optional reduction ratios of 2.03:1, 2.25:1, 2.64:1, 2.96:1 and 3.33:1. A centrifugal clutch is also available as optional equipment.[1][2][3]
Four-cylinder horizontally opposed, two-stroke, aircraft engine with a dual 38 mm diaphragm carburetors. Produces 85 hp (63 kW) at 5,500 rpm if free-air-cooled or 80 hp (60 kW) at 5,500 rpm if fan cooled. It has a factory rated
time between overhaul (TBO) of 1,200 hours. Currently in production.[3]
F-30E
Four-cylinder horizontally opposed, two-stroke, aircraft engine with fuel injection. Produces 90 hp (67 kW) at 5,500 rpm if free-air-cooled or 85 hp (63 kW) at 5,500 rpm if fan cooled. It has a factory rated TBO of 1,200 hours. Currently in production.[3]
F-30S
Four-cylinder horizontally opposed, two-stroke, aircraft engine with dual integral pumper carburetors. Produces 100 hp (75 kW) at 6200 rpm if free-air-cooled or 95 hp (71 kW) at 6,200 rpm if fan-cooled. It has a factory rated TBO of 1,000 hours. Currently in production.[2]
F-30ES
Four-cylinder horizontally opposed, two-stroke, aircraft engine with fuel injection. Produces 110 hp (82 kW) at 6,200 rpm if free-air-cooled or 105 hp (78 kW) at 6,200 rpm if fan-cooled. It has a factory rated TBO of 1,000 hours. Currently in production.[2]
Dry weight: 105 lb (47.6 kg), including starter and exhaust system, 129 lb (58.5 kg) with gearbox, exhaust system and electric start. Fan cooling adds 8.5 lb (3.9 kg)