The Pegasus PAL 95 is a twin cylinder, horizontally opposed aircraft engine that was developed by Pegasus Aviation (NZ) Ltd of New Zealand for use in ultralight aircraft. The engine is no longer available.[1]
Designed to fill a similar market segment as the similar configuration and output HKS 700E, the PAL 95 produces 65 hp (48 kW) at 5200 rpm.[1]
The PAL 95 has a computer-controlled engine management system that controls both the fuel injection system and the ignition timing, giving automatic altitude-compensated mixture control. The pistons are forged and ceramic coated. The intake valves are made from nickel-steel and the exhaust valves from stainless steel. The engine was supplied with an electric starter and an exhaust system by the factory as standard equipment.[1]
Speed reduction is via a standard twin cog-belt system, with harmonic dampening on the crankshaft pulley. The initial TBO was estimated by the manufacturer as 1500 hours.[1]
Data from Cliche[1]