Zlin Aviation
Section 1
Maintenance Manual Aircraft Maintenance Manual
Issued: 01/02/2006
QAP-AMM-Rev02
Date of latest Revision: 23/01/2013
Page Number: 1-2
1.1.1 SPECIFICATIONS AND DATA
Technical Description
The Savage is a single engine, high wing, two seat tandem Light Sport Aircraft of classical design.
It is built in the Czech Republic (Zlin Aviation sro) and in Italy (Zlin Aviation Italia srl) in full
compliance with the regulations in force in both Countries, and to the requirements of the ASTM
Consensus Standards for Light Sport Aircraft. The manufacturing organization between the two
companies if fully covered in the company’s QAP and explained and described in the company’s
QAM.
Weights (ULM-VDS)
CLASSIC/BOBBER
CRUISER
CUB
Max take-off weight
600kg (992 lbs)
600 kg (992 lbs)
600 kg (992 lbs)
Empty weight
288 kg (633.6 lbs)
291 kg (640 lbs)
296 kg (652 lbs)
Payload
162 kg (356.4 lbs)
159 kg (349.8 lbs)
154 kg (339.5 lbs)
Max wing loading
39,4 kg (86.9 lbs)
39,4 kg (86.9 lbs)
39,4 kg (86.9 lbs)
Load factor, limit
+4 -2
+4 -2
+4 -2
NOTE:
Performance specifications are outlined in the POH.
Difference between Classic, Cub, Cruiser, Bobber
Aesthetic differences in the cowling design (CUB has a metal sheet cowling instead of
composite);
Different panel housing;
Slightly different instrument panel;
Bending angle of the front lexan varies
Different shape of landing gear
Design of the bottom fuselage part
Different window design
Different wing tips design
NOTE: wings and profile, fuselage, controls, main constructive aspects etc. are the same for all models.
There are no maintenance aspects that make one model different from the other (others than the materials of
the cowling which need different processes for minor repairs.
