EVEKTOR-AEROTECHNIK Harmony LSA User manual

EVEKTOR - AEROTECHNIK a.s.
Letecka 1384 Tel.: [phone]
686 04 Kunovice Fax: [phone]
CZECH REPUBLIC email: [e-mail]
www.evektoraircraft.com
Copyright © 2011
EVEKTOR - AEROTECHNIK, a.s.
AIRCRAFT OPERATING INSTRUCTIONS
FOR
LIGHT SPORT AIRCRAFT
Serial number:
Registration mark:
Document number: HARMAOIUS
Date of issue: June 01, 2011
This manual must be on the airplane board during operation. This manual
contains information which must be provided to the pilot
and also contains supplementary information provided by the airplane
manufacturer - Evektor - Aerotechnik a.s.
This aircraft must be operated in compliance with the information
and limitations stated in this manual.

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CONTENTS
0. TECHNICAL INFORMATION
0.1 Log of Revisions ............................................................0-3
0.2 List of Effective Pages...................................................0-5
0.3 AOI Sections...................................................................0-8

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0.1 Log of Revisions
All revisions or supplements to this manual, except actual weighing data,
are issued in form of revisions, which will have new or changed pages as
appendix and the list of which is shown in the Log of Revisions table.
The new or changed text in the revised pages will be marked by means of
black vertical line on the margin of page and the revision number and date
will be shown on the bottom margin of page.
Rev.
No. Affected
Section Affected Pages Date Appro- ved Date
Date of
Insertion
Sign.

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0.2 List of Effective Pages
Section Page Date Section Page Date
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0.3 AOI Sections
Section
GENERAL ..............................................................................1
LIMITATIONS ........................................................................2
EMERGENCY PROCEDURES ...............................................3
NORMAL PROCEDURES ......................................................4
PERFORMANCE ...................................................................5
WEIGHT AND BALANCE ......................................................6
AIRPLANE AND SYSTEM DESCRIPTION ............................7
AIRPLANE HANDLING, SERVICING
AND MAINTENANCE .............................................................8
SUPPLEMENTS......................................................................9

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SECTION 1
1. GENERAL
1.1 Introduction ....................................................................1-3
1.2 Certification basis ..........................................................1-3
1.2.1 Data location.....................................................................1-4
1.3 Warnings, cautions, notes.............................................1-4
1.4 Descriptive data .............................................................1-5
1.4.1 Airplane description...........................................................1-5
1.4.2 Powerplant........................................................................1-5
1.4.3 Main technical data...........................................................1-6
1.4.4 Three-view drawing...........................................................1-7
1.5 Definitions and abbreviations .......................................1-8

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1.1 Introduction
PARTICIPANT’S RESPONSIBILITY
There are inherent risks in participating in aviation activities, these
risks are significant, up to and potentially including death. Operators
and passengers of recreational aviation aircraft, by participation,
accept the risks inherent in such participation of which the ordinary
prudent person is or should be aware. Pilots and passengers have
a duty to exercise good judgment and act in a responsible manner
while using the aircraft and to obey all oral or written warnings, or
both, prior to and/or during use of the aircraft.
This Aircraft Operating Instructions has been prepared to provide
pilots and instructors with information for safe and efficient
operation of the HARMONY LSA airplane. It also contains
supplementary information considered to be important by the
airplane manufacturer.
1.2 Certification basis
HARMONY LSA complies with the ASTM F2245-09a
Standard Specification for Design and Performance of a Light Sport
Airplane, issued by ASTM International Committee F37.
IFR version complies with FAR 91.205 requirements, as well as
with F2245 Annex A3 Additional Requirements for Light Sport
Airplanes Operated under Instrument Flight Rules, as known till
1.1.2009.

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1.2.1 Data location
The certification documentation is available from the US importers
or airplane manufacturer on a request of competent aviation
authority and/or Designated Airworthiness Representative.
Contact address:
Visit www.evektoraircraft.com for US importers.
Airplane Manufacturer:
Evektor - Aerotechnik, a.s.
Letecká 1384
686 04 Kunovice
Czech Republic
tel.:[phone]
fax:[phone]
e-mail:[e-mail]
1.3 Warnings, cautions, notes
The following informations apply to warnings, cautions and notes
used in the Aircraft Operating Instructions:
WARNING
MEANS THAT NON-OBSERVATIONS OF THE
CORRESPONDING PROCEDURE LEADS TO
AN IMMEADIATE OR IMPORTENT
DEGRADATION OF THE FLIGHT SAFETY.
CAUTION
MEANS THAT NON-OBSERVATIONS OF THE
CORRESPONDING PROCEDURE LEADS TO A
MINOR OR TO A MORE OR LESS LONG TERM
DEGRADATION OF THE FLIGHT SAFETY.
NOTE
Draws the attention to any special item not
directly related to safety but which is important or
unusual.

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1.4 Descriptive data
1.4.1 Airplane description
HARMONY LSA airplane is a metal-composite low-wing monoplane
of semimonocoque structure with two side by side seats and
steerable nose wheel landing gear.
For further description see Section 7 - Airplane and system
description.
1.4.2 Powerplant
The standard powerplant consists of ROTAX 912ULS (100 hp)
engine and ground adjustable, 3-bladed, WOODCOMP KLASSIC
170/3/R propeller.
IFR version is fitted with certified ROTAX 912S2 engine and ground
adjustable, 3-bladed, composite Warpdrive CF prop, with Nickel
protection of blade leading edges.
For further description see Section 7 - Airplane and system
description.
For particular engine and propeller type - see Section 9 -
Supplements - Airplane description.

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1.4.3 Main technical data
Wing
Span 30.45 ft
Area 111.47 sq.ft
MAC depth 3.873 ft
Wing loading with vortex generators 11.84 lbs/sq.ft
Wing loading no vortex generators 11.38 lbs/sq.ft
Aileron - area 3.35 sq.ft
Flap - area 5.60 sq.ft
Fuselage
length 20.05 ft
width 3.55 ft
height 8.12 ft
cockpit canopy max. width 3.9 ft
Horizontal tail unit
Span 9.09 ft
HTU Area 20.67 sq.ft
Elevator area 9.06 sq.ft
Vertical tail unit
Height 4.21 ft
VTU Area 11.20 sq.ft
Rudder area 4.63 sq.ft
Landing gear
Wheel track 6.40 ft
Wheel base 4.76 ft
Nose and main landing gear wheel diameter 15 in

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1.4.4 Three-view drawing
Figure 1-1

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1.5 Definitions and abbreviations
NOTE
The abbreviations on placards in the airplane
cockpit are printed in BOLD CAPITAL LETTERS
in the text of this Aircraft Operating Instructions.
ACCU accumulator
ALT ENC encoding altimeter
ATC air traffic control
bar bar 1 bar = 100 kPa
BEACON anti-collision beacon
°C Celsius degree
CAS calibrated airspeed
CLOCK aircraft clock
ft foot 1 ft = 0.305 m
GPS global positioning system
HTU horizontal tail unit
IAS indicated airspeed
IC intercom
IFR instrument flight rules
ISA international standard atmosphere
kg kilogram
KIAS indicated airspeed in knots
KCAS calibrated airspeed in knots
mph mile per hour
mph CAS calibrated airspeed in miles per hour
km/h CAS calibrated airspeed in km/h
kts knots 1 kt = 1.852 km/h
litres litre
lbs pounds 1 lb = 0.45 kg
m meter
MAC mean aerodynamical chord
max. maximum
min. minimum or minute
mm millimeter
m/s meter per second
OAT outside air temperature

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OFF system is switched off or control element is in off-
position
ON system is switched on or control element is in on-
position
Pa pascal 1Pa = 1N/m2
PSI pound per sq.in (1PSI = 6.89 kPa)
RPM revolutions per minute
RWY runway
sq.ft foot squared
sq.m meter squared
VAmaneuvering airspeed
VFE maximum flap extended speed - flaps in 50°
position
VFR visibility flight rules
VLOF airplane lift-off speed
V-METER voltmeter
VNE never exceed speed
VNO maximum structural cruising speed
VSO stall speed with wing flaps in 50° position
VS1 stall speed with wing flaps in 0° position
VTU vertical tail unit
VXbest angle-of-climb speed
VYbest rate-of-climb speed
XPDR transponder

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