Aeropilot-SRO Legend 600 Installation guide

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
1
Callsign: N54SK
Serial no 1646 Dated 23 June 2017
Jeníkovská 1815
286 01 Čáslav
Phone [phone]
Fax [phone]
www.aeropilotcz.com
CIN: 27108431 TIN: CZ27108431
Pilot Operating Handbook and
Flight Training Supplement
AEROPILOT SRO

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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Airplane model: Legend 600
Manufacturer: Aeropilot-SRO, Czech Republic
Airplane Serial Number: 1646
Date of Construction: 06/16/2016
Registration: N54SK
Airworthiness Category: Special Light Sport Aircraft (S-LSA)
Issue Date of POH: 06/23/2017
This airplane must be operated in
compliance with information and
limitations contained herein. This
pilot operating handbook and Flight
Training Supplement must be
available on board of the airplane at
all times.

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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Record of Revisions
Any revisions to the handbook must be recorded in the following table. The responsible airworthiness
authority must endorse it where applicable.
Revision
#
Section
Pages
Date of
Issue
Approval
Date of
Approval
Date
Entered
Signature

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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INTRODUCTION ............................................................................................................................................... 5
GENERAL INFORMATION.............................................................................................................................. 7
LIMITATIONS................................................................................................................................................. 15
EMERGENCY PROCEDURES ....................................................................................................................... 19
NORMAL PROCEDURES .............................................................................................................................. 23
PERFORMANCE ............................................................................................................................................. 30
WEIGHT AND BALANCE, AND EQUIPMENT LIST ............................................................................... 33
DESCRIPTION OF AIRPLANE AND SYSTEMS ....................................................................................... 36
HANDLING AND SERVICING...................................................................................................................... 41
PERIODICINSPECTIONS ............................................................................................................................. 43
SUPPLEMENTS .............................................................................................................................................. 44
FLIGHT TRAINING SUPPLEMENT ........................................................................................................... 44

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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INTRODUCTION
Instructions for use
 This Manual is issued by aircraft manufacturer and must be kept on board of the aircraft during
each flight.
 Records shall be made legibly and indelibly; no page may be torn out of the Manual.
 Manual with complete records form a part of the aircraft technical documentation.
 This manual provides the reference material for a pilots training in the aircraft’s safe operation
 Total number of landings and operating time shall be recorded and transferred from old
into new logbook, along with the information about latest service bulletin performed.
 The aircraft’s owner is responsible for correctness of operation records.
Importantinformation
Changes and Amendments to this Manual
Any changes to applicable regulations or to this aircraft's construction will be published in the
form of a bulletin. It is the responsibility of each aircraft owner to implement the change (or to
have it implemented) and to record the change in the respective part of this Manual.
Any damage to the aircraft shall be reported to applicable inspector-technician. The inspector-
technician will recommend the method of repair, supervise the repair and will make a
technical inspection after the repair has been completed. A record shall be entered into the
aircraft documentation. Any damage which potentially compromises the airworthiness of the
aircraft must be reported as per FAA regulations.

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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Advisory Notice
THIS MANUAL IS WRITTEN FOR THE STANDARD 912 ULS
POWERED LEGEND 600 S-LSA, AS MANUFACTURED ON
PREMISES BY THE AEROPILOT SRO.
AIRCRAFT THAT DIFFER FROM THE PRODUCTION
STANDARD, IN WHATEVER WAY, ARE NOT ADDRESSED IN
THIS MANUAL, EXCEPT TO THE EXTENT SAID AIRCRAFT
CORRESPOND WITH THE PRODUCTION STANDARD.
THIS EDITION OF THIS MANUAL IS APPLICABLE TO
AIRCRAFT REGISTERED IN THE UNITED STATES OF
AMERICA.

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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GENERAL INFORMATION
Introduction to Airplane
The Legend 600 LSA aircraft is a two-seat, strut high-wing monoplane of all-composite structure
designed for sport, recreational or tourist flying. Favorable flight characteristics make the aircraft
suitable for flight training. The aircraft features spacious crew and baggage compartments. Large
doors provide for comfortable boarding of crew and loading of baggage. Adjustable seats allow the
pilots of all heights to find comfortable position. A stiff Kevlar cabin, four-point seat harnesses and
rocket assisted rescue system provide maximum safety of crew in emergency situations.
Cautionary Notes
This aircraft is not subject to the certification in the ‘Standard Category’ by the
Civil Aviation Authority of the Czech Republic and it is operated entirely on the
user’s own risk.
Deliberate spins and aerobatics are prohibited.
Owner of the aircraft and every operator of the aircraft shall read this
Manual carefully and familiarize themselves with its contents.

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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Aircraft Drawing
Measurement in Inches and Millimeters

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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Legend 600 Aircraft Data
Aircraft data
Model
Airframe LSA 600
Engine
Propeller
Rescue System
Manufacturer
AEROPILOT SRO
Rotax 912 ULS
Klassic 1700/3
GALAXY6/600SD
Serial No.
1646
6.786.936
17013683R
8202
Place & Year of
Manufacture
2016-Čáslav (Czech Republic)
2016
2016
2016
Other Data
Data Summary for Legend 600 S-LSA
Wing
Wing span 29.84 feet
Length 23.13 feet
Height, total 9.59 feet
Wing surface 116.7 ft2
Wing aspect ratio 7.64
Depth of MAC (mean aerodynamic chord) 3.93 feet
Wing profile MS 313 B
At root 4,27 feet
At tip 3,15 feet
Wing flaps surface 11.83ft2
Flaps deflections 15° / 30° / 40°
Tail
Horizontal tail plane span 9.19 feet
Horizontal tail plane surface 24.1ft2
Vertical tail plane surface 11.2ft
2
Weights
Empty weight 766 lbs
Take-off weight, maximum 1320 lbs
Engine
Type (brief description): Rotax 912ULS 100HP –four-stroke, four-cylinder engine, air-cooled cylinders with water-
cooled heads, integrated reduction gearbox, dual electronic ignition and tuned inlet manifold.
Engine Displacement 1400ccm
Take-off power, max. 98.99kW@5800rpm
Cruising power, max. 93.81kW@5500rpm
Dry weight 123 lbs
(Includingaccessories) 159 lbs

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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Fuel (See Rotax Manual) MOGAS 91 Octane min, 100LL AVGAS
Oil (type) SHELL HELIX H x 7 AV 10 W - 40
Oil capacity 3L
Reduction gear (gear ratio) 2.43:1
Fuel tank volume –main tank 34 Gallons (130L)
Propeller
Diameter / pitch at 75% Woodcomp ‘Klassic’ ground adjustable
Weight 11 lbs ( 5kg)
Material Wood/Composite
Performance Summary
SUMMARY OF PERFORMANCE SPECIFICATIONS
Call Sign: N54SK
Type/Name
LEGEND 600
Serial No./Year of manufacture
1646/2016
Empty weight
766 lbs
Max. Take-off weight
1320 lbs
Useful Load
554 lbs
VY (Best Rate of Climb)
65KT
Vso (Stall Speed, Full Flaps)
38KT
VFE (Max Flap Extension Speed)
72KT
VA (Maneuvering Speed)
97KT
VNO (Max Struc. Cruising Speed)
108KT
VNE (Never Exceed Speed)
120KT
VH(Max Speed @ 5800rpm for 5 minutes)
120KT
Fuel tank capacity –34 Gal
Useable 34 Gal
Take-off power, (Max.)
98.99kW@5800rpm
Cruising power, (Max.)
93.81kW@5500rpm

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Date of Issue: 23 June 2017 Revision - Original
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Terminology
Aviation Acronym
Description
A/C / ACFT
Aircraft
A/P
Autopilot
AC
Alternating Current
ACP
Audio Control Panel
AFIS
Airborne Flight Information System
AFM
Aircraft Flight Manual
AGL
Above Ground Level
AHRS
Attitude Heading Reference System
AMP / Amp / amp
Ampere
ANN
Annunciator
ANT
Antenna
AOA
Angle of Attack
AP
Autopilot
AS
Airspeed
ASL
Above Sea Level
ASSY
Assembly
AT
Antenna
ATC
Air Traffic Control
ATIS
Automatic Terminal Information Service
B/A
Bank Angle
B/CU
Battery/Charger Unit
BIT
Built-In-Test
CAS
Calibrated Air Speed
CFI
Certified Flight Instructor
CFII
Certified Flight Instructor/Instrument
CFR
Code of Federal Regulations (FAA)
CG
Center-of-Gravity
DIST
Distance
ECU
Electronic Control Unit
EFIS
Electronic Flight Instrument System
EGT
Exhaust Gas Temperature
ELT
Emergency Locator Transmitter
EXT
Extinguisher
FAA
Federal Aviation Administration
FCU
Fuel Control Unit
GPS
Global Positioning System
IAS
Indicated Airspeed
ISA
International Standard Atmosphere
KIAS
Knots Indicated Airspeed
KTAS
Knots True Airspeed
Kts
Knots
L/D
Lift-To-Drag (Ratio)
MAINT
Maintenance
MFD
Multi Function Display
OAT
Outside Air Temperature
OBS
Omni Bearing Selector
RCVR
Receiver
STBY
Standby
TAS
TRUE Air Speed

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Date of Issue: 23 June 2017 Revision - Original
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TEMP
Temperature
TOC
Top-of-Climb
TOD
Top-of-Descent
VFR
Visual Flight Rules
VMO
Maximum Allowable Airspeed
VOR
Very High Frequency Omni directional Range Radio
VORTAC
Collocated VOR and TACAN Stations
VS
Vertical Speed
VSI
Vertical Speed Indicator
WT
Weight
XMIT
Transmit
XMTR
Transmitter
XPDR
Transponder
Z
Zulu Time (GMT) or Zero

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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Crosswind / Headwind Determination
The crosswind and headwind component chart allows for figuring the headwind and crosswind
component for any given wind direction and velocity.
Sample Problem
Runway..........................................................................17
Wind........................................................140° at 25 knots
First, determine how many degrees difference there is between the runway and the wind direction. It
is known that runway 17 means a direction of 170°; from that subtract the wind direction of 140°. This
gives a 30° angular difference or wind angle. Next, locate the 30° mark and draw a line from there
until it intersects the correct wind velocity of 25 knots. From there, draw a line straight down and a
line straight across. The headwind component is 22 knots and the crosswind component is 13 knots
Figure 1Crosswind Calculation Chart (Source ---FAA Pilot Handbook Of Aeronautical Knowledge)
Supporting Documentation

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Date of Issue: 23 June 2017 Revision - Original
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The following documents are regarded as supporting documents to this
Pilot Operating Handbook:
For aircraft fitted with 912 ULS engines: latest revision / edition of the
Operators Manual For Rotax® Engine Type 912 Series, Ref No.: OM-912.
Latest revision / edition of Rotax, SD-912-064UL, as applicable (to type of
engine fitted).
Operator manual for GPS, Flight and Engine Instruments, COM radio,
transponder and GPS:
SkyView SVHDX –Version 15.0
SkyView SVD700 –Version 15.0 (Document 101321-016, Revision Q - For
use with firmware version 10.0)
Reference should be made to these documents for operational guidelines and
instructions. These should be incorporated into the normal and emergency
procedures for the aircraft as applicable.

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Date of Issue: 23 June 2017 Revision - Original
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Limitations
Introduction
This section includes operating limitations, instrument markings and basic placards
necessary for the safe operation of the Aeropilot Legend 600, its engine, systems and
equipment
Warning decal visible to the passenger containing the following words is required:
Registrationdecal
OPERATING DATA AND
LIMITATIONS
Call Sign
N54SK
Type/Name
LEGEND 600
Manufacturer
AEROPILOT SRO
Serial No./Year of manuf.
1646/2017
Empty weight
766LBS
Max. Take-off weight
1320LBS
Payload
554LBS
Stall Speed
38 KT
Never Exceed Speed VNE
130 KT
Max. Speed In Turbulent
Air - VNO
108 KT
Max Speed With Flaps -
VFE
72KT
Fuel Tank Capacity
34 Gal.
Location: Left part of instrument panel
THIS AIRCRAFT IS MANUFACTURED IN ACCORDANCE WITH THE
LIGHT SPORT AIRCRAFT AIRWORTHINESS STANDARD AND DOES
NOT CONFORM TO STANDARDCATEGORYAIRWORTHINESS
REQUIREMENTS
Location: right part of instrument panel, above center.

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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USA REGISTRATION DECAL
Call Sign
N54SK
Type/Name
LEGEND 600
Manufacturer
AEROPILOT SRO
Serial No./Year of manuf.
1646/2015
Empty weight
766 LBS
Max. Take-off weight
1320 LBS
Payload
554 LBS
Location: center tunnel, in front of central control.

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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Airspeed Limits
VY (Best Rate of Climb)
65KT
Vso (Stall Speed, No Flaps)
33KT
Vso (Stall Speed, Full Flaps)
28KT
VFE (Max Flap Extension Speed)
72KT
VA (Maneuvering Speed)
97KT
VNO (Max Struc. Cruising Speed)
108KT
VH(Max Speed @ 5800rpm for 5 minutes)
103KT
VNE (Never Exceed Speed)
130KT
Wind speed limits
Maximum allowed headwind speed 20kn
Maximum allowed crosswind speed: 8kn (inexperienced pilot)
15kn (Experienced pilot/Instructor)
Power plantlimits
Maximumallowed speed: 5800rpm for 5 minutes
Maximumcontinuous speed: 5500rpm
Idling speed, approximately: 1400rpm
Maximumcylinder head temperature: 266 deg F
Maximumoil temperature: 275deg F
Minimum air temperature at starting: 13deg F
Maximum air temperature at starting: 122deg F
Oil pressure: 16.7psi
Weights
Minimum crew weight: 132 lbs
Maximumtake-off weight: 1320 lbs
Empty weight (typical) 766 lbs
Maximum COG locations from front edge of wing:
Forward limit 26% MAC
Aft limit: 34% MAC
Max. Baggage weight 33 lbs
Tailwind take-off and landing should be avoided.
VA- Do not apply full deflections above this speed
The VNE speed must not be exceeded under any circumstances!
All speeds stated in this Manual are Indicated Air Speeds IAS!

Serial Number 1646
Date of Issue: 23 June 2017 Revision - Original
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Payload decal
Fuel tank capacity / Max. Payload
Gal
Pilot, Pax and
Baggage -Lbs
Full tanks
33
356
3/4 of tanks
26
398
1/2 of tanks
17
452
1/4 of tanks
8
506
30min. fuel reserve
2
N/A
Location: right part of right instrument panel.
Maneuvers
Turns up to 60° banking angle, climbing and diving up to 30° from horizontal plane.
INTENTIONAL SPINS, AEROBATCIS AND FLIGHT IN IMC PROHIBITED!
Load factors (per UL-2 regulation)
Maximum positive load factor in the centre of gravity: 4.0
Maximum negative load factor in the centre of gravity: -2.0
Types of operation
Light Sport
Only daylight flights are allowed under VFR (ground contact) conditions
Other
Only flight conditions that the aircraft is equipped and the pilot properly certified for.

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Date of Issue: 23 June 2017 Revision - Original
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Emergencyprocedures
This section describes recommended procedures for resolving emergency situations, which could occur during
operation.
Strict adherence to inspection and maintenance schedule prescribed bythe manufacturer reduces the probability of a
failure to absolute minimum.
Engine failure
During take-off run
 Throttle to idle
 Ignition switch off
 Brake according to actual conditions
During take-off (in air)
 Maintain speed 65kts minimum
 Less than 300ft above terrain –land in the direction of flight, maneuvering the aircraft out of obstructions
 Detect wind direction and speed
 Apply flaps as necessary
 Shut off fuel cock
 Shut off the ignition
 Tighten safety harnesses
 Main switch off
In flight
 Dive and glide, maintain speed 65kts minimum
 More than 300ft above terrain –: select suitable landing location
 If cause of engine failure is discovered (e.g. empty fuel tank) and flight altitude allows it, try restarting the
engine according to the procedure below:
 If engine does not restart or if flight altitude drops below safe level, select suitable landing location and
proceed according to previous section.
NOTE: IF A SUCCESSFUL EMERGENCY LANDING IS IN DOUBT
DUE TO OBSTRUCTIONS, LENGTH OF LANDING SITE OR
TERRAIN –USE THE EMERGENCY PARACHUTE
Restarting engine in flight
May be only performed at safe flight altitude to allow safe emergency landing with engine off.
 Fuel cock open, check amount of fuel in selected tank
 Fuel pump switch on
 Ignition switch on
 Throttle up to 1/3 of throttle, not more
 Flight speed 65-75knots
 Press start button

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Date of Issue: 23 June 2017 Revision - Original
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Flying with engine off
If the engine fails, it is necessary to maintain best glide speed - 65knot
Safety landing
Safety landing is generally made in case of loss of orientation, worsening of weather, low fuel, and/or sudden
incapacitation of pilot. Always follow the recommendations listed below:
 Select suitable landing location depending on wind direction and terrain/cover
 If possible, communicate your intention to land
 Fly above right side of selected landing area in the direction of planned landing, maintaining horizon at approx.
150ft altitude.
 Apply “take-off” flaps, maintain speed 65knots
 Carefully check the location.
 Climb a little, maintaining ground visibility if conditions permit, fly small left circuit.
 Perform landing approach and then land.
Check selected area throughout the safety landing procedure.
In case of fire
On ground, during starting
 Release starter button
 Shut off fuel cock
 Switch off ignition
 Main switch off
 Exit the aircraft
 Tryto extinguish the fire
On ground, engine running
 Shut off fuel cock
 Switch off ignition
 Main switch off
 Exit the aircraft
 Tryto extinguish the fire
On ground, during take-off
 Speed 65knots
 Shut off fuel cock
 Switch off heating, if switched on
 Switch off ignition
 Main switch off
 Land and exit the aircraft
 Tryto extinguish the fire