EVEKTOR-AEROTECHNIK SportStar plus Technical specifications

EVEKTOR - AEROTECHNIK a.s.
Letecka 1384 Tel.: [phone]
686 04 Kunovice Fax: [phone]
CZECH REPUBLIC email: [e-mail]
Copyright © 2006
EVEKTOR - AEROTECHNIK, a.s.
FLIGHT MANUAL
FOR
LIGHT SPORT AIRPLANE
Serial number:
Registration mark:
Document number: SP2006FMENKT
Date of issue: December 20, 2006
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.........................................3
0.1 Log of Revisions ...............................................................3
0.2 List of Effective Pages......................................................5
0.3 FM Sections.......................................................................8

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0. TECHNICAL INFORMATION
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 Revisons 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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Rev.
No. Affected
Section Affected Pages Date
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0.2 List of Effective Pages
Section Page Date Section Page Date
- Title page - 2 2-1 Dec 20/06
2-2 Dec 20/06
0 0-1 Dec 20/06 2-3 Dec 20/06
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Section Page Date Section Page Date
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0.3 FM 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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December 20, 2006 1 - 1
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General
CONTENTS
1. GENERAL ......................................................................3
1.1 Introduction .......................................................................3
1.2 Certification basis .............................................................3
1.3 Warnings, cautions, notes................................................3
1.4 Descriptive data ................................................................4
1.4.1 Airplane description.............................................................. 4
1.4.2 Powerplant........................................................................... 4
1.4.3 Main technical data.............................................................. 4
1.4.4 Three-view drawing.............................................................. 6
1.5 Definitions and abbreviations ..........................................7

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1. GENERAL
1.1 Introduction
This Flight manual has been prepared to provide pilots and
instructors with information for safe and efficient operation of the
SPORTSTARPLUS airplane. It also contains supplementary
information considered to be important by the airplane
manufacturer.
1.2 Certification basis
The aircraft described herein complies with the Standard
Specification for Design and Performance of a Light Sport Airplane,
Designation F 2245-04, issued by ASTM International Committee
F37.
This type of aircraft complies with the Czech UL-2 airworthiness
requirements, it has been type certified by the Light Aircraft
Association of the Czech Republic and the type certificate
ULL 07/2003 supplement was issued in December 19th, 2006.
1.3 Warnings, cautions, notes
The following informations apply to warnings, cautions and notes
used in the Flight manual:
WARNING
MEANS THAT NON-OBSERVATIONS OF THE
CORRESPONDING PROCEDURE LEADS TO
AN IMMEADIATE OR IMPORTANT
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.

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NOTE
Draws the attention to any special item not
directly related to safety but which is important or
unusual.
1.4 Descriptive data
1.4.1 Airplane description
SPORTSTARPLUS airplane is an all-metal low-wing of
semimonocoque structure with two side by side seats and 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 WOODCOMP KLASSIC 170/3/R propeller.
For further description see Section 7 - Airplane and system
description.
For concrete engine and propeller type - see Section 9 -
Supplements - Airplane description.
1.4.3 Main technical data
Wing
Span 28.37 ft 8.646 m
Area 112.7 sq.ft 10.47 sq.m
MAC depth 4.1 ft 1.25 m
Wing loading 10.76 lbs/sq.ft 52.53 kg/sq.m
Aileron - area 2.62 sq.ft 0.25 sq.m
Flap - area 5.60 sq.ft 0.52 sq.m
Fuselage
length 19.62 ft 5.980 m
width 3.55 ft 1.082 m
height 7.66 ft 2.335 m
cockpit canopy max. width 3.87 ft 1.180 m

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Horizontal tail unit
Span 8.20 ft 2.50 m
HTU Area 20.88 sq.ft 1.94 sq.m
Elevator area 8.40 sq.ft 0.78 sq.m
Vertical tail unit
Height 4.07 ft 1.24 m
VTU Area 10.76 sq.ft 1.00 sq.m
Rudder area 4.31 sq.ft 0.40 sq.m
Landing gear
Wheel track 6.12 ft 1.865 m
Wheel base 4.43 ft 1.350 m
Main and nose landing gear
wheel diameter 14 in 350 mm

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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 indicatedair speed 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 milimeter
m/s meter per second
OAT outside air temperature

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General
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
VAmanoeuvring 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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Limitations
CONTENTS
2. LIMITATIONS .................................................................3
2.1 Introduction .......................................................................3
2.2 Airspeed ............................................................................3
2.3 Airspeed indicator marking..............................................4
2.4 Powerplant.........................................................................5
2.5 Powerplant instrument marking.......................................6
2.6 Miscellaneous instrument marking..................................6
2.7 Weight................................................................................6
2.8 Centre of gravity................................................................7
2.9 Approved manoeuvres .....................................................7
2.10 Manoeuvring load factors.................................................7
2.11 Flight crew.........................................................................7
2.12 Kinds of operation ............................................................8
2.13 Fuel ....................................................................................9
2.14 Oil.....................................................................................10
2.15 Maximum number of passengers ..................................10
2.16 Other limitations..............................................................10
2.17 Limitation placards .........................................................10

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Limitations
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