Shark 600 Technical specifications

FLIGHT MANUAL
Airplane Type
SHARK 600
Model / Version:
Serial Number:
Registration:
Document Number:
Shark600_MA_075 Rev.E
Date of Issue:
Approval Number and Date:
This airplane must be operated according to the information and
limitations presented in this Flight Manual.
This manual must be available to the Pilot at any time during flight.

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FLIGHT MANUAL
SHARK 600
Section 0
Foreword
2024-02-25
Rev. E
Doc. No.: SHARK600_MA_075
0-1
0Foreword
0.1 Record of Revisions
Rev.
Number of
the document
- bulletin
It concerns
pages No.
Date of
issue
Signature
IR
-
New document
A
-
Sections 0, 1, 4, 7
B
-
Sections 0, 2, 3, 4, 5, 7
21.3.2023
C
-
Sections 0, 3, 5
26.7.2023
D
-
Sections 0, 5
18.9.2023
E
-
All sections
25.2.2024
NOTE
It is the responsibility of the owner to keep this manual up to date. Check
www.shark.aero for the latest updates.

Section 0
Foreword
FLIGHT MANUAL
SHARK 600
0-2
Doc. No.: SHARK600_MA_075
2024-02-25
Rev. E
0.2 Table of Contents
Section
Content
Rev.
0
Foreword
E
1
General
B
2
Limitations
B
3
Emergency Procedures
B
4
Normal Procedures
C
5
Performance
D
6
Weight and Balance
A
7
Airplane Description
C
8
Handling, Servicing and Maintenance
A
9
Supplements
B

FLIGHT MANUAL
SHARK 600
Section 1
General
2024-02-25
Rev. B
Doc. No.: SHARK600_MA_075
1-1
TABLE OF CONTENTS
1General
1.1 Introduction ...................................................................................1-3
1.2 Certification Bases..........................................................................1-3
1.3 Warnings, Cautions and Notes.......................................................1-4
1.4 Three View Drawing.......................................................................1-5
1.5 Dimensions.....................................................................................1-6
1.6 Engine.............................................................................................1-7
1.7 Propeller.........................................................................................1-7
1.8 Fuel.................................................................................................1-8
1.9 Lubricant and Oil ............................................................................1-8
1.10 Cooling............................................................................................1-9
1.11 Weights ..........................................................................................1-9
1.12 Wing Loading..................................................................................1-9
1.13 List of Abbreviations.....................................................................1-10

Section 1
General
FLIGHT MANUAL
SHARK 600
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2024-02-25
Rev. B
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FLIGHT MANUAL
SHARK 600
Section 1
General
2024-02-25
Rev. B
Doc. No.: SHARK600_MA_075
1-3
1.1 Introduction
This flight manual is provided with your airplane to allow you to
obtain as much knowledge as possible for safe operation.
Additionally, this section contains definitions or explanations of
symbols, abbreviations, and terminology used in this manual. It
also includes supplementary information which can be helpful to
the pilot.
Read this manual before your first flight and make sure you
understand all the information presented here. This manual does
not replace a Flight Instructor!
1.2 Certification Basis
The following standards were used for approval and testing:
UL-2 Requirements of LAA –Light Aircraft Association of
Czech Republic.
LTF UL Ultralight aircraft requirements applicable in Germany.
ASTM Standard Requirements for Light Sport Aircraft (LSA)
valid in US and used as a background for European light
airplane standards.

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General
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SHARK 600
1-4
Doc. No.: SHARK600_MA_075
2024-02-25
Rev. B
1.3 Warnings, Cautions and Notes
The following definitions applied to Warnings, Cautions and Notes
are used in this manual:
WARNING
NON-OBSERVATION OF THE CORRESPONDING PROCEDURE CAN
IMMEDIATELY LEAD TO A SIGNIFICANT REDUCTION OF FLIGHT
SAFETY.
CAUTION
Non-observation of the corresponding procedure can lead to
equipment damage and reduction of flight safety in a short or longer
time interval.
NOTE
Information not directly related to the safety of the flight.

FLIGHT MANUAL
SHARK 600
Section 1
General
2024-02-25
Rev. B
Doc. No.: SHARK600_MA_075
1-5
1.4 Three View Drawing
Figure 1-1 Three View Drawing

Section 1
General
FLIGHT MANUAL
SHARK 600
1-6
Doc. No.: SHARK600_MA_075
2024-02-25
Rev. B
1.5 Dimensions
Overall Dimensions
Wing Span: .............................................7.9 m
Length:....................................................6.85 m
Height: ...................................................2.5 m
Wings
Airfoil:.....................................................JS20 –JS80
Wing Area:..............................................9.5 m2
Mean Aerodynamic Chord (MAC):.........1.237 m
Aspect Ratio: ..........................................6.671
Dihedral:.................................................6°
Sweep of Leading Edge: .........................3.53° / 13.8° / 38°
Aileron
Area:.......................................................0.281 m2each aileron
Flaps
Area:.......................................................0.922 m2each flap
Horizontal Stabilizer
Area:.......................................................2.154 m2
Elevator Area:.........................................0.662 m2
Angle of Incidence:.................................-1.5°

FLIGHT MANUAL
SHARK 600
Section 1
General
2024-02-25
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1-7
Vertical Stabilizer
Area:.......................................................1.062 m2
Rudder Area: ..........................................0.335 m2
Landing Gear
Track:......................................................1.694 m
Wheel Base:............................................1.48 m
1.6 Engine
Rotax 912 ULS Engine, 4 Cylinder, 4-Stroke, Horizontally Opposed,
Liquid Cooled Cylinder Heads, Air Cooled Cylinders.
Propeller is driven via an integrated Reduction Gear.
Reduction Ratio:.....................................2.43 : 1
Displacement;.........................................1.352 liters
Output Power:........................................73.5 kW / 100hp @ 5800
rpm
1.7 Propeller
Two-bladed Variable Pitch Propeller, manufactured by Woodcomp
and Neuform:
•In-flight electrically adjustable (Woodcomp SR 3000 2WN)
•In-flight hydraulically adjustable (Woodcomp KW20W)
•In-flight electrically adjustable (Neuform TXR2-V-70)

Section 1
General
FLIGHT MANUAL
SHARK 600
1-8
Doc. No.: SHARK600_MA_075
2024-02-25
Rev. B
1.8 Fuel
Approved fuel grades are:
•MOGAS EN 228 Super/Super plus (minimum 95 octane).
•MOGAS ASTM D4814.
•AVGAS 100LL (ASTM D910) *see restrictions in 2.12.
Total Capacity:
•100 liters ( 26,4 US gallons) or optional 150 liters ( 39.6 US
gallons), in both configurations 1 liter (0.26 gal) is unusable.
1.9 Lubricant and Oil
Lubrication system is “forced feed type” with an external reservoir.
Type:
•for MOGAS: API SL
•for AVGAS / 100L: API SL
Oil capacity:
•3 liter maximum ( 0.79 gal)
•2 liter minimum ( 0.53 gal)

FLIGHT MANUAL
SHARK 600
Section 1
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2024-02-25
Rev. B
Doc. No.: SHARK600_MA_075
1-9
1.10 Cooling
The Cooling System consists of a combination of forced air and a
pressurized closed liquid system.
Type:
•Conventional cooling liquid mixed with water 50% + 50%
For example: BASF Glysantin Antikorrosion 50% / water 50%
Capacity:
•Minimum: 2.4 Litres ( 0.63 gal)
•Maximum: 2.5 Litres ( 0.66 gal)
1.11 Weights
See section: 2.6
1.12 Wing Loading
Maximum take-off weight 600 kg
Wing Loading
63.2 kg/m²
Power Loading
6.0 kg/hp

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General
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Doc. No.: SHARK600_MA_075
2024-02-25
Rev. B
1.13 List of Abbreviations
Abbreviation
Definition
CAS
Calibrated airspeed; Indicated speed corrected
for installation and instrument errors. CAS is
equal to TAS at standard atmospheric
conditions at MSL
Center of
Gravity
Point of equilibrium for the airplane mass
(weight)
CG
Centre of Gravity
CG Arm
Distance from the reference datum to the CG,
it is determined by dividing the total moment
(sum of the individual moments) by the total
mass (weight)
CG Limits
The CG range which an airplane with a given
mass must be operated within
Demonstrated
crosswind
component
The max. speed of the crosswind component
at which the maneuverability of the airplane
during take-off and landing has been
demonstrated during test flights
EW
Empty Mass (Weight) of the airplane including
unusable fuel, all operating fluids and
maximum oil amount. Movable ballast is not
included in Empty Weight
GS
Ground Speed. Speed of the airplane relative
to the ground
hp
Horsepower

FLIGHT MANUAL
SHARK 600
Section 1
General
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Abbreviation
Definition
IAS
Indicated airspeed as shown on the airspeed
indicator
ISA
International Standard Atmosphere
KCAS
Calibrated airspeed on knots
KIAS
Indicated airspeed in knots
KTAS
True airspeed in knots
Lever Arm
The horizontal distance from the reference
datum to the center of gravity (of a
component)
MAC
Mean Aerodynamic Chord
MAP
Manifold (intake) Pressure
MCPMaximum permissible
continuous engine output power
during flight
MLW
Maximum mass (weight) permissible for
landing
Moment
The mass (weight) of a component multiplied
by its lever arm
MPG
Miles (nautical) per US gallon
MSL
Mean Sea Level
MTOW
Maximum Take-off Mass (Weight), the
maximum mass (weight) permissible for take-
off
OAT
Outside Air Temperature

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2024-02-25
Rev. B
Abbreviation
Definition
RD
Reference datum (RD)/ Reference plane. An
imaginary vertical plane from which all
horizontal distances for the center of gravity
calculations are measured. It is the plane
through the leading edge of the wing root rib,
perpendicular to the longitudinal axis of the
airplane.
rpm
Revolutions per minute
Station
A defined point along the longitudinal axis
which is generally presented as a specific
distance from the reference datum
Take-off Power
Maximum engine power for take-off
TAS
True airspeed. Speed of the airplane relative to
air. TAS is CAS corrected for altitude and
temperature error
TFUEL
Temperature (Fuel) (at a specific critical point
under the engine cowling)
TMOT
Temperature (Motor) (at a specific critical
point under the engine cowling)
Unusable Fuel
The amount of fuel remaining in the tank
which cannot be used
Usable Fuel
The amount of fuel available for the flight plan
calculation
Useful Load
The difference between take-off mass (weight)
and empty mass (weight)

FLIGHT MANUAL
SHARK 600
Section 1
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Doc. No.: SHARK600_MA_075
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Abbreviation
Definition
VA*, VA
Maneuvering speed. Maximum speed at which
the airplane is not overstressed at full
deflection of control surfaces
VFE, VFE
Maximum speed with flaps extended
VLE, VLE
Maximum speed with the gear extended
VLO, VLO
Maximum speed of gear extending or
retracting
VNE, VNE
Speed which must never be exceeded in any
operation
VNO, VNO
Maximum structural cruising speed which
should only be exceeded in calm air, and then
only with caution
VS0, VS0
The power-off stall speed with the airplane in
landing configuration
VS1, VS1
The power-off stall speed with the airplane in
its current configuration
VX, Vx
Best angle-of-climb speed
VY, Vy
Best rate-of-climb speed
* - Indexes of characteristic speeds may, in cases of very small type (e.g.,
on placards), be written in the font size of the base type.

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General
FLIGHT MANUAL
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Doc. No.: SHARK600_MA_075
2024-02-25
Rev. B
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FLIGHT MANUAL
SHARK 600
Section 2
Limitations
2024-02-25
Rev. B
Doc. No.: SHARK600_MA_075
2-1
TABLE OF CONTENTS
2Limitations
2.1 Airspeeds........................................................................................2-3
2.2 Airspeed Indicator Markings..........................................................2-4
2.3 Engine.............................................................................................2-5
2.4 Engine Instrument Markings..........................................................2-6
2.5 Weight Limits .................................................................................2-7
2.6 Center of Gravity Limits .................................................................2-8
2.7 Approved Flight Maneuvers...........................................................2-8
2.8 Maneuvering Load Factor ..............................................................2-9
2.9 Flight Crew .....................................................................................2-9
2.10 Type of Operation ........................................................................2-10
2.11 Fuel...............................................................................................2-10
2.11.1 Approved Fuel Types ....................................................... 2-10
2.11.2 Fuel Tank Capacity ........................................................... 2-11
2.12 Other Limitations .........................................................................2-11
2.13 Placards ........................................................................................2-12

Section 2
Limitations
FLIGHT MANUAL
SHARK 600
2-2
Doc. No.: SHARK600_MA_075
2024-02-25
Rev. B
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