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Tiger 5BTiger 5B

The aircraft is a four-place, low-wing, single-engine airplane, equipped with tricycle landing gear.

This airplane is certificated in the normal and utility category. See the airplaneā€™s P.O.H. for approved maneuvers. The airplane is approved for day and night VFR operations when equipped in accordance with F.A.R. 91 or F.A.R 135.

The airplane is powered by a horizontally opposed, four cylinder, direct drive, normally aspirated, air cooled, carburetor equipped engine. The engine is a Lycoming Model O-360-A4K and is rated at 180 horsepower.

The fuel system consists of two tanks with a total capacity of 52.6 gallons, of which 51 gallons is usable, two sump tanks, independent fuel gauges, and a fuel selector valve. An auxiliary electric fuel pump supplements engine-driven pump.

The electrical system uses a 24-volt, 70-amp alternator and a battery.