TL Ultralight TL-3000 Sirius, Руководство по эксплуатации и полетам

Страница: 49 / 64

Flight and operational manual
TL 3000 SIRIUS
Page 48
7.6 Seats and safety belts
The seats are removable and composed of an upholstered composite seat and
backrest. The safety belts are four ‐ point central buckle.
7.7 Luggage compartment
The luggage compartment is located behind the pilot seats and designed to
accommodate maximum 25 kg of luggage. It is accessible from the pilot cockpit.
In order to prevent a possible luggage intrusion into the cockpit, the luggage
compartment is equipped with a removable net.
7.8 Cabin door
The cabin door opens upwards. To remain in the closed position, the cabin door
is equipped with a latch mechanism and secured with an independent
espagnolette mechanism. To remain in the open position, they are supported
by gas operated springs.
7.9 Power plant
The aircraft is powered with Rotax 912 ULS engine. It is a four ‐ cylinder, four ‐
stroke opposite cylinders engine with a central camshaft and OHV distribution.
Cooling is combined; the heads of cylinders are liquid ‐ cooled and the cylinders
are air ‐ cooled. Lubrication is a dry box type. Ignition is dual non ‐ contact
condenser with a magneto. The engine is equipped with an electric starter,
alternative current generator and mechanical fuel pump. The propeller is
powered through an integrated reducer with mechanical vibration silencer.
The propeller with the propeller cone cover is attached to the engine.
7.10 Fuel system
The fuel system is composed of two composite fuel tanks with the total volume
of 130 litres that are installed in the wing, fuel piping, fuel content gauge and
fuel filter. Each fuel tank is equipped with a sludge system. If required by a
customer, a fuel pump is included in the system in some cases.