Description Of Airplane And Systems; General; Airframe - Skyleader 200 Pilot Operating Handbook

7.

DESCRIPTION OF AIRPLANE AND SYSTEMS

7.1.

General

This section provides the general descriptions of the ULL 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 fully
provided by the ULL aircraft Maintenance Manual.
7.2.

Airframe

The airframe is made of duralumin materials, which allows for an aerodynamic shape and excellent flight
characteristics while archieving a minimal ULL 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 ULL aircraft is not complex, it may be only done by qualified personnel.
The holder of a mechanic certificate with airframe or power plant rating(s), or both, or an Repairman maintenance
that has received additional task specific training for the function to be performed is generally considered the
minimum level of certification to perform heavy maintenance on the SKYLEADER 200.
JIHLAVAN airplanes authorizes the holder of a mechanic certificate with airframe or power plant rating(s), or both,
or an Repairman maintenance that has received additional task specific training for the function to be performed to
perform heavy maintenance on the SKYLEADER 200 as described in the Basic principles for repair and maintenance
of the ULL aircraft document..
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KP 2U POH 05/2022