Shark UL User Manual

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Flight manual UL aircraft
1.4. AIRPLANE BASIC DESCRIPTION
SHARK is an all-composite low-wing ultralight airplane with retractable
undercarriage, tandem seats configuration, designed for fast
cross-country flights.
Airplane is equipped with 100HP Rotax 912 ULS engine and one of
propellers acc. paragraph 7.8.
Wing span
7,9 m
Length
6,85 m
Height
2,3 m
Wing area
9,5 m
2
MAC length
1,237 m
Swept wing angles
3,53° / 13,8° / 39,8°
Existing version of the airplane, approved by calculations and tests,
cover installation of engines Rotax 912ULS with optional equipment.
All versions are calculated and tested for MTOW 600kg, but this specific Flight
manual has defined limits, valid for UL category in Czech Republic under LAA
CZ.
Marking of a specific airplane version is defined in introduction of
this flight manual. Deviations from the basic version are
described in the following box:

Shark UL Specifications

General

Brand	Shark
Model	UL
Category	Aircrafts
Language	English