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

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Flight and operational manual
TL 3000 SIRIUS
Page 45
7.1 Introduction
Section 7 describes aircraft systems and operations
7.2 Airframe
TL – 3000 Sirius aircraft is a two ‐ seat, strut type high ‐ wing, single ‐ engine
monoplane with the nose type undercarriage. TL – 3000 Sirius airframe is an all
composite shell structure.
7.2.1 Fuselage
The fuselage is made as a pure sandwich shell structure with the struts.
The power plant is placed in the front fuselage portion, and the
cockpit with the seats next to each other is situated behind the engine
wall. The luggage compartment is located behind the pilot seats.
7.2.2 Wing
The wing is all composite with a single strut consisting of a metal tube
and composite coating. It is designed as a two ‐ spar sandwich shell
structure with a root rib and another rib at the strut attachment point.
The wing is equipped with the ailerons and simple flap. The fuel tank is
located in the front root portion of the wing.
7.2.3 Horizontal tail plane (VOP)
Stabilizer is an all composite two ‐ spar concept. The divided elevator is
a single spar shell structure.
7.2.4. Vertical tail plane (SOP)
The aircraft keel is an integrated part of the fuselage shell structure
and is reinforced with the struts. The rudder is a single ‐ spar shell
structure.