Skyleader 600 - Description of Airplane and Systems; General; Airframe

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7. DESCRIPTION OF AIRPLANE AND SYSTEMS
7.1. General
This section provides the general descriptions of the aircraft airframe and systems. This section does not provide any
maintenance information, and may not be used as maintenance input. The purpose is to provide an understanding
of the way the systems are installed and operate. When maintenance information is needed, it is fy provided by the
Aircraft Maintenance Manual.
7.2. Airframe
The airframe is made of duralumin materials, which allows for an aerodynamic shape and excellent ight
characteristics while archieving a minimal aircraft weight.
All outside surfaces are protected with high performance 2 component white paint. Interior surfaces are protected
with a high quality 2 component paint.
The airframe consists of two major components. These are the fuselage (including engine mounts, cockpit,
centroplan, landing gear, horizontal and vertical tail units), and wing (each one is connected by three bolts to the
centroplan part).
Althrough assembly and disassembly of the aircraft is not complex, it may be only done by qualied personnel.
The holder of a mechanic certicate with airframe or power plant rating(s), or both, or an LSA Repairman
maintenance that has received additional task specic training for the function to be performed is generally
considered the minimum level of certication to perform heavy maintenance on the SKYLEADER 600.
JIHLAVAN airplanes authorizes the holder of a mechanic certicate with airframe or power plant rating(s), or
both, or an LSA Repairman maintenance that has received additional task specic training for the function to be
performed to perform heavy maintenance on the SKYLEADER 600 as described in the Basic principles for repair and
maintenance of the aircraft document..