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.
[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 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.