Air Creation SKYPPER evo 912 IS Owner's manual

GDMUSKevo912IS-2G Version 0010 1
Pilot’s Operating Handbook
Trike Type :
S
SK KY YP PP PE ER R e ev vo o
9
91 12 2 I IS S
615 Route de l’Aérodrome, 07200 Lanas, France
Telephone: [phone] • Fax: [phone]
[email protected] • http://www.aircreation.fr

GDMUSKevo912IS-2G Version 0010 2
1 Table of Contents
1Table of Contents................................................................... 2
2Amendment Record Sheet .................................................... 4
2.1 Table of Amendments.......................................................................... 4
2.2 Amendments........................................................................................ 4
3General.................................................................................... 5
3.1 About this Document............................................................................ 5
3.2 Drawings.............................................................................................. 6
Figure 3-1: Skypper evo 912 IS in 3 Perspectives ...................................................................6
4Technical specifications –Performance .............................. 7
4.1 Performance......................................................................................... 7
5Instructions for use................................................................ 8
5.1 Adapting Wings & Trikes...................................................................... 8
5.2 Assembling........................................................................................... 8
5.3 Setting & Function of Controls.............................................................. 8
5.3.1 Master Switch.........................................................................................................8
5.3.2 Instrumentation power switch.................................................................................8
5.3.3 Ignition Switches.....................................................................................................9
5.3.4 Starter buttons........................................................................................................9
5.3.5 Battery Backup switch............................................................................................9
5.3.6 Throttle ...................................................................................................................9
5.3.7 Ground steering......................................................................................................9
5.3.8 Brake......................................................................................................................9
5.3.9 Parking Brake.........................................................................................................9
5.3.10 Fuel Cock ...............................................................................................................9
5.3.11 Fuel Pumps ..........................................................................................................10
5.4 Ergonomics........................................................................................ 10
5.4.1 Pedal Set..............................................................................................................10
5.4.2 Passenger Footrest..............................................................................................10
5.4.3 Harnesses ............................................................................................................10
5.4.4 Baggage Storage .................................................................................................10
5.5 Preflight check.................................................................................... 11
5.6 Boarding............................................................................................. 12
5.6.1 General.................................................................................................................12
5.6.2 Pilot in the Front Seat...........................................................................................12
5.6.3 Passenger ............................................................................................................12

GDMUSKevo912IS-2G Version 0010 3
5.7 Start-up .............................................................................................. 12
5.8 Flight .................................................................................................. 13
5.8.1 Prior to Take-Off...................................................................................................13
5.8.2 Take-Off................................................................................................................14
5.8.3 Cruising ................................................................................................................14
5.8.4 Landing.................................................................................................................14
5.8.5 Parking .................................................................................................................15
5.9 Emergency procedures...................................................................... 15
5.9.1 Power failure on take-off ......................................................................................15
5.9.2 Power failure at altitude........................................................................................15
5.9.3 Restart the engine in flight....................................................................................15
5.9.4 Engine fire ............................................................................................................15
5.10 Options............................................................................................... 16
5.10.1 Cockpit fairing.......................................................................................................16
5.10.2 Parachute.............................................................................................................16
5.10.3 Dual Control for Instruction...................................................................................16
5.10.4 Skis.......................................................................................................................17
5.10.5 HP (Cross Country)..............................................................................................17
5.10.6 Bush .....................................................................................................................17
5.10.7 Strobes.................................................................................................................17
5.10.8 Oil Thermostat......................................................................................................17
5.10.9 4-points harness...................................................................................................17
5.10.10 Flight instrument MGL Explorer+SP6+FF............................................................17
5.10.11 Flight instrument MGL Xtrem+SP6+FF................................................................17
5.10.12 Flight instrument MGL MX1+SP6+FF..................................................................18
5.10.13 Flight instrument MGL EMS2...............................................................................18
5.10.14 Flight instrument MGL ASV 2...............................................................................18
5.10.15 Magnetic Compass Ø57.......................................................................................18
5.10.16 Radio Icom A25 + antenna...................................................................................18
5.10.17 Radio Dittel KRT 2 Radio + antenna.................................................................18
5.10.18 ICA 12 or ICA 13 Intercom .................................................................................18
5.10.19 Dittel KTX 2 Transponder ..................................................................................18
5.10.20 Propeller...............................................................................................................18
5.11 Specific Use / Safety Instructions....................................................... 19
5.11.1 Towing..................................................................................................................19
5.11.2 Load Carriage, Survey Material, Data Transmission, Photography, Video
&c. ........................................................................................................................19
5.11.3 Sky jumpers..........................................................................................................19
5.11.4 Skis.......................................................................................................................19
6Appendix............................................................................... 21
6.1 Trike –Quality Form........................................................................... 21

GDMUSKevo912IS-2G Version 0010 4
2 Amendment Record Sheet
2.1 Table of Amendments
Review
Date
Comment
Section
0010
09-2021
Reference document
2.2 Amendments
The information in this manual is based on the data that was available at the time of its
publication. The latest amendments to this manual will be issued on the Air Création
website (http://www.aircreation.fr) in PDF format. This should be printed out and added
to the manual. The amendment table should at that time be updated with the appropriate
details and date. Therefore it is important for operators to check the website regularly for
any amendments that have been made. If any errors or omissions are found in this manual
please advise the factory.

GDMUSKevo912IS-2G Version 0010 5
3 General
3.1 About this Document
This manual is a legal document which is approved for use with Air Creation SKYPPER
trikes.
It must be used in conjunction with the particular wing’s operating handbook and the
Rotax 912 IS Owner’s Manual.
It must remain with the aircraft, and not be amended or altered without authority from Air
Creation.
All pilots should read this manual before flying as pilot in command of the aircraft to
which it refers.
This manual is not intended to teach you how to fly the aircraft. Learning to fly should be
accomplished under the supervision of a suitably qualified flight instructor experienced in
flying this type of aircraft.
What this manual will do is provide the information necessary to a qualified pilot for the
safe flight of this weight-shift aircraft.

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3.2 Drawings
Figure 3-1: Skypper evo 912 IS in 3 Perspectives

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4 Technical specifications –Performance
4.1 Performance
Engine
912 IS
Propeller
Helix
H50F 1,75 L-CS-
12-3/A1
Neuform
TXL3-65-
47-101.6
Neuform
CL3 -65-(IP)-
47-101,6
Duc Flash
2MFSH-3-L
Empty weight (standard)
183,5 kg
405 lbs
186 kg
410 lbs
185,5 kg
409 lbs
185 kg
408 lbs
Maximum weight without wing
417 kg
919 lbs
417 kg
919 lbs
417 kg
919 lbs
417 kg
919 lbs
Ultimate load factors at max
weight
+6g -3g
+6g -3g
+6g -3g
+6g -3g
Limit load factors
+ 4g - 2g
+ 4g - 2g
+ 4g - 2g
+ 4g - 2g
Fuel tank capacity
55 Liters
14.5 US Gal
55 Liters
14.5 US Gal
55 Liters
14.5 US Gal
55 Liters
14.5 US Gal
Maximum power
73.5 kW
73.5 kW
73.5 kW
73.5 kW
Maximum rpm
5800 rpm
5800 rpm
5800 rpm
5800 rpm
Maximum continuous power
69 kW
69 kW
69 kW
69 kW
Rpm
5600 rpm
5600 rpm
5600 rpm
5600 rpm
Reduction drive
Mechanical
Mechanical
Mechanical
Mechanical
Ratio
1:2.43
1:2.43
1:2.43
1:2.43
Maximum propeller rpm
3400 rpm
2600 rpm
2600 rpm
3400 rpm
Minimum height for a noise
level on ground less than 65dB
at maximum power
415 m
1362 ft
280 m
919 ft
330 m
1083 ft
375 m
1230 ft

GDMUSKevo912IS-2G Version 0010 8
5 Instructions for use
5.1 Adapting Wings & Trikes
In our current production, the two-seater wings Fun 450, iFun 16-16SP-XL, Kiss 450,
iXess, NuviX and BioniX may equip SKYPPER trikes.
5.2 Assembling
1. Assemble the wing as indicated in the Pilot’s Operating Handbook of the wing, rest it on its nose
faced into the wind.
2. Wheel the trike behind the wing, in the keel axis, remove the windshield, pull the upper beam
down and take the front strut out.
3. Raise the upper beam, push the hang point into the hang bracket, position the Ø10 hang bolt,
install the butterfly nut, tilt the lever back in order to tighten the plates, and secure with the safety
ring.
4. Slip the backup fastening cable through the belt loop at the kingpost level, make one turn around
it. Slip it through the belt loop again and fasten it to the trike upper beam. The backup fastening
cable should pass under the tensioning cables and between the keel and the fine cord of the
CORSET for the NuviX and BioniX wings. This operation secures both the trike to the wing and
the wing crossbar tensioning system.
5. Raise the wing nose by pulling the trike back or by slipping the control bar until the keel meets the
upper arch.
6. Attach the front strut between the plates at the top of the upper beam using the bolt, the butterfly
nut and the safety ring.
7. Hold the control bar and lift the wing. The front tube base is fixed to the frame at windshield level.
8. Set the safety bolt of the upper beam (above the passenger seat), screw the butterfly nuts, then slip
the safety rings into the drilling of the bolt.
9. Set the bolt connecting the front tube with the lower beam; screw the butterfly nut, and secure
with the split ring.
10. Assemble the windshield using the ¼ turn plastic screws.
11. To disassemble, reverse the assembly operations.
5.3 Setting & Function of Controls
5.3.1 Master Switch
The key switch located on the lower right side of the dashboard allows the circuit board
to be supplied by the battery. A green light confirms that the circuit is activated.
5.3.2 Instrumentation power switch
The switch located on the upper right part of the dashboard allows the power supply of
the electronic instruments by the battery.

GDMUSKevo912IS-2G Version 0010 9
5.3.3 Ignition Switches
Each ignition line has its own switch, positioned to the lower right of the dashboard,
which makes it possible to operate them simultaneously or to select one of them. Line A
is controlled by the left switch, line B by the right switch.
5.3.4 Starter buttons
The engine start is activated by two push buttons located in the lower part of the
dashboard. The one on the right is the start power switch. It allows the momentary power
supply of the engine by the battery and activates the fault detection system. The one on
the left activates the starter.
5.3.5 Battery Backup switch
In the event of a malfunction of the two ignition lines, the engine may be restarted by
switching the emergency switch located at the bottom of the instrument panel to the "on"
position. This activates the permanent power supply of the engine by the battery to allow
to extend the flight to an emergency landing place.
5.3.6 Throttle
The primary throttle control is a foot throttle which is connected to the right foot pedal.
This is activated by pressing the foot pedal. There is also an additional hand throttle
which is located on the right side of the instrument panel. Both throttles work in the
conventional manner, i.e. forwards to increase power. An addition foot throttle may be
fitted for the rear seat occupant/instructor (in option).
5.3.7 Ground steering
The nose wheel is steered by the foot pedals via cables. They work in the normal weight
shift aircraft manner –i.e. push right to go left.
Rear seat steering is also an option and operates in the same manner via a rear steering
bar and linking cables (in option).
5.3.8 Brake
Push the left pedal forward to apply the hydraulic disc brakes upon the wheels.
5.3.9 Parking Brake
Push the brake pedal (brake action), lift the parking brake rack located on the right of the
left pedal and slowly release the brake pedal. The rack is blocked. The parking brake is
spring loaded and automatically returns to the off position when the brake pedal is
pressed again.
5.3.10 Fuel Cock
The fuel supply valve is located near the right articulation of the upper beam, in front of
the fuel tank. The tap is positioned so that it is open when the tap is in line with the fuel
line and shut off when the tap is perpendicular to the fuel line.

GDMUSKevo912IS-2G Version 0010 10
5.3.11 Fuel Pumps
The two fuel pumps are controlled by switches positioned on the lower left side of the
dashboard. The left switch acts on the main pump, the one on the right on the auxiliary
pump.
5.4 Ergonomics
5.4.1 Pedal Set
The position of the foot pedals can be adjusted to provide the most comfortable and
efficient piloting position.
The range of adjustment of the rudder pedal is up to 2 inches (5 cm) with 2 horizontal
positions.
The rudder pedal is moved by pulling back the fork axel and setting it in the desired
position.
5.4.2 Passenger Footrest
The footrest can be adjusted by rotation on its axis on the bottom strut. Two positions
1.5 in (4 cm) apart may be set according to the size of the passenger.
5.4.3 Harnesses
The Skypper is fitted with lap straps which utilize conventional airline-type buckles.
There are also additional inertia reel shoulder harnesses for the pilot and passenger which
attach to the lap strap buckles.
5.4.4 Baggage Storage
Baggage can be stowed in the following areas:
A storage basket is located in the cockpit fairing under the pilots’legs. Maximum load for is 22
lbs (10 Kg).
In the stowage area under rear seat. Maximum load in this area 33 lbs (15 Kg).
Rear seat stowage bag. This can be fitted when flying solo and is secured by webbing straps. Max
load 65 lbs (30 Kg).
Document pocket behind the back of the front seat. Max load 2 lbs (1 Kg).
Loads carried in these areas must be accounted for when working out the takeoff weight
of the aircraft.

GDMUSKevo912IS-2G Version 0010 11
5.5 Preflight check
The following is a brief summary of the minimum pre-flight inspection, which assumes
that the scheduled maintenance checks outlined in the maintenance manual has been
performed.
If you are unsure, it does no harm to increase the number of items in your inspection in
accordance with the recommendations of the maintenance manual.
1. Check the wing as indicated in the user’s manual.
2. Ignition switches and master switch OFF
3. Check the trike-to-wing fastenings and every safety device (bolt, nut and split ring).
4. Check that the pylon backup cable is correctly positioned and fastened.
5. Check the lower and upper fixing of front strut and every safety device (bolts, nuts and split rings).
6. Pylon fixation bolts secure and pinned.
7. Engine fairing secured
8. Engine mount, rubber mounts, security and condition
9. Check the propeller, the exhaust, its fastening springs and rubber mounts.
10. Check the fuel tank, sight gauge and cap, the fuel filter, the fuel valve and the fuel hose for
security, integrity, and leaks.
11. Check the coolant level in the expansion tank located behind the passenger seat and any leakage
from hoses. Make sure the water cooler box is unobstructed.
12. Check the oil level with the gauge placed in the bottle located on the engine’s left side, behind the
rear strut’s shock absorber, in accordance with the recommendations given in the Rotax engine
manual (rotation of the propeller).
13. Check that the radiator's lower air inlet is not obstructed.
14. If there may be water in the fuel tank (due to condensation, fuel quality) eliminate it with the help
of the drain system located on the right side, behind the passenger seat. To drain, open the door of
the luggage container, take the draining tube out and press the button. Fix the draining tube back
into place after use. Also drain the fuel prefilter located behind the rear seat on the right side of the
trike.
15. Lock check of steering, brake lines, position and fixing of pedals, tires condition and inflation.
16. Rear wheels, brake lines and wheel spats security and conditions, tire and suspension units
condition and inflation.
17. Seat cushions and backrests, position and security
18. Condition of seat belts and function of buckles
19. Check the storage bags and the bag placed on the passenger seat while flying solo.
20. Check the operation and friction of the hand and foot throttles to detect possible jamming of the
throttle cables. Starting the engine under these conditions may cause loss of control of the aircraft
and cause a serious accident, or even death, due to the strong push after starting.
21. Brake pedal operation
22. Security of windscreen
23. Loose item check in cockpit fairing (if installed).

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5.6 Boarding
5.6.1 General
When flown solo, the aircraft must be flown from the front seat only !
A protective helmet must always be worn, fit correctly and secured. A positive lock must be fitted
to the visor and be engaged during flight.
Check that neither pilot nor passenger has any objects that can fall out of their pockets.
Ensure articles of clothing, such as gloves, scarves, glasses/sun-glasses, as well as cameras, maps,
knee boards, portable navigation instruments etc. are secured, no loose objects in the cockpit !
Any loose object is likely to pass through the propeller arc, destroy the propeller or/and throw
debris through the sail and seriously threaten the safety of the aircraft and its occupants.
Occupants with long hair, particularly in the back seat, must have it tied up to ensure that it cannot
reach moving or hot parts of the engine.
5.6.2 Pilot in the Front Seat
When flying solo, the aircraft may only be piloted from the front seat!
Get on board from the left-hand side of the trike. The pilot should step over the lower
strut while holding the front strut with the left hand. The reverse operation is
recommended to exit the trike.
5.6.3 Passenger
Once the back of the pilot seat has been pulled down, the passenger embarks from the left
of the trike by placing his left foot on the rear gear strut and holding the upper strut with
the right hand.
Passenger minimum briefing:
Do not touch instructor foot throttle or ignition switch, if fitted.
Do not touch the control frame and cables.
Fold arms, or rest them on knees.
Do not under any circumstances, touch the hot and/or rotating engine parts directly behind.
5.7 Start-up
Rotating propellers are almost invisible and can cause injury or death. Ensure that
all spectators/children/pets are kept well clear of the propeller arc. On certain
surfaces, stones can bounce into the propeller blades and become projectiles. Do
not start an engine if any loose stones are in the vicinity of the aircraft with any
spectators present at all.
1. The ultralight has to be in a secure zone; make sure it is facing an unobstructed place while taking
into account the effect of the blast of the propeller upon the surroundings.
2. Fill the fuel tank (please refer to the engine user’s manual for fuel details). The gauge is located on
the right at the front of the tank.
3. Make sure the fuel valve is open.

GDMUSKevo912IS-2G Version 0010 13
4. Sit in the trike, pilot in the front seat, parking brake engaged, safety belt fastened. Pull the buckle
to release the winding system of the shoulder straps and fix it on the locating lug provided for this
purpose, on the belt’s side.
Safety belts should be placed at hip level and tightened correctly. Safety belts
fastened at abdominal level may cause internal injury in the event of a violent shock.
5. Rotate the battery ignition key to the "On" position (the green battery indicator light on the
dashboard will illuminate).
6. Turn on the electronic instruments using the switch on the top right of the dashboard.
7. Set the switch off the main fuel pump to "On".
8. Set the two switches of the ignition lines to "On".
9. Press the Start Power Switch. Keep it pressed during steps 9 to 12.
10. Check that the two red lights below the ignition line switches turn on and off after about 3
seconds. If not, consult the Rotax engine manual to identify the problem.
11. Check that the fuel pressure reaches 3 bar (43.5 psi).
12. Depress the accelerator pedal by 1 to 2 cm from the "idle" position (refer to the Rotax manual for
precise information on this operation depending on the temperature).
13. Make sure no one is standing close to the propeller and say aloud: “Clear prop”, then pause.
Engage the starter by pressing the starter button. Release the pressure on both pushers as soon as
the engine starts and runs at 1500 rpm minimum. Activate starter for max 10 seconds only,
followed by a cooling period of 2 minutes.
Be prepared to cut the engine immediately in case of runaway due to a
blocked throttle mechanism.
14. Check the extinction of the warning lights and the engine parameters. The oil pressure should rise
within 10 seconds after starting.
15. Adjust the throttle for more than 2500 rpm for 5 seconds (generator B switches to A) if the oil
pressure is stable and above 3 bar (43.5 psi).
If a warning light comes on or flashes after starting, perform a line and ignition test.
After this test, both warning lights must be off, otherwise a problem exists and no
takeoff must be undertaken.
16. Set the auxiliary fuel pump switch to "On".
17. Start taxing only after the engine has reached its operating temperature parameters. Release the
parking brake by a short push on the brake pedal.
If the parking brake has been engaged with little pressure and has not been
released, the pilot may not feel his action when taxing, but the take-off distance will
be much longer.
5.8 Flight
5.8.1 Prior to Take-Off
Your ultralight must be in good flight condition, that is to say maintained and used as
prescribed by Air Creation.
1. Harnesses and helmets secure.

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2. Clothes, personal effects & accessories attached; pockets empty or closed.
3. Controls full and free.
4. Parking brake disengaged.
5. Red warning light for the correct lock of the upper beam unlit. If the light is on, the upper beam is
not properly locked.
6. Lower and upper fixing of front strut, trike-to-wing fastenings in position and secure.
7. Instruments all serviceable, reading correctly.
8. Fuel on, sufficient for the flight, cock open.
9. Proper operation of both ignition lines. The test is performed at a speed of 4000 rpm by cutting the
ignition line A. The engine speed change must be at most 250 rpm. Reposition the ignition switch
of line A to ON and reproduce the operation with line B. Put both switches back ON after the test.
10. Proper operation of both fuel pumps. The test is performed by cutting off the auxiliary fuel pump
at a speed of 2000 rpm. No loss of power or abnormal operation should be observed. The fuel
pressure limits must not be exceeded. After restarting the auxiliary pump, repeat the operation
with the main pump. Restore both switches to ON after the test.
11. Minimum parameters of engine temperature reached.
12. Corset (if fitted) set to relaxed (slow) position.
13. Wind speed and direction checked, and suitable for safe take-off on selected runway.
14. All Clear, all around the circuit, final clear and runway unobstructed.
15. Power, check full power is achieved early in the take-off run.
5.8.2 Take-Off
Use the foot pedal to progressively attain full throttle when carrying a passenger.
When flying solo, 3/4 throttle will be enough for take-off and climbing. Use full power
only under critical conditions (short take-off runs, obstacles and high altitude flight). In
this case never reduce or cut the engine below the 300 ft (100 m) altitude to avoid
dynamic stalling.
The recommended speed for initial climb is indicated in the wing’s manual.
5.8.3 Cruising
Keep the aircraft level with the throttle between ¼ and full power, depending on given
airspeed and load. Avoid repeated and sudden power climbs and idle dives to prevent
quick engine temperature changes, which could damage the engine by thermal shock. To
avoid permanent pressure on the right foot throttle, push the hand lever on the right of the
control panel until it resists, then release the pedal. To return to pedal control, press the
pedal until it resists, then pull back the lever.
Fuel tank content is easy to check from pilot’s and passenger’s seats as the tank has a side
gauge, or the optional electric gauge. A landing should be considered before tank
contents reach 1.5 US gallons (5 liters). This allows approximately 30 minutes reserve of
flight at economical cruising speed.
5.8.4 Landing
The landing approach is best executed using the foot throttle pedal and both hands on the
control bar. At maximum load, keep the throttle at ¼ of full power when on final to
facilitate flare-out. Throttle back when the wheels touch the ground.
The recommended approach speed is indicated in the instruction and maintenance manual
of the wing.

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5.8.5 Parking
1. Park the aircraft in the crosswind and place the extremity of the half-wing in the wind on the
ground.
2. Turn off electronic instruments.
3. Stop the engine with the ignition switch.
4. Cut the battery power using the key.
5. Block the parking brake.
6. Block the control bar on the front strut of the trike using Velcro strap.
7. Leave the trike, pilot first, then passenger, and always to the left side.
5.9 Emergency procedures
5.9.1 Power failure on take-off
Should the power unit fail after take-off while still at low height, maintain aircraft control
and safety approach speed, and land the aircraft straight ahead without attempting to turn
back to the landing field. If time allows, set ignition switch and fuel cock off.
5.9.2 Power failure at altitude
If the engine fails for any reason, prepare for landing and carry out the emergency
procedures as follows:
1. Immediately establish the best glide angle speed.
2. Check for suitable landing sites. Choose a number of preliminary options if possible.
3. Set ignition, pump and battery switches off. Close the fuel cock if time allows.
4. Check that pilot and passenger seat belts are tight and secure.
5. Check wind direction, either by natural indications such as smoke rising or by judging drift of
aircraft over the ground.
6. Choose the most appropriate landing site.
7. Set up an approach as accurate as possible into wind.
8. Remember that your aircraft cannot be heard. Check that no one is on the landing site.
9. Finalize your approach, deciding upon the best landing free of any obstacles.
10. Use a short landing technique.
11. Evacuate the aircraft as quickly as possible, encouraging the passenger to do the same if there is
damage to the unit that could result in a fire.
5.9.3 Restart the engine in flight
1. Set the ignition switch to ON.
2. Set the main fuel pump switch to the ON position.
3. Operate the starter with the two push buttons (see 5-7 Start)
4. Adjust the throttle.
Restarting in flight may be hazardous. Keep enough altitude and stay close to a
landing field.
5.9.4 Engine fire
Should an engine fire occur during flight:

GDMUSKevo912IS-2G Version 0010 16
1. Maintain your flying speed.
2. Set ignition, pumps and battery switches off.
3. Set fuel cock off.
4. Carry out the emergency landing procedures as above.
5.10 Options
The standard empty weight used as reference to calculate the empty weight of the trike
does not include the options stated hereafter. Thus it is necessary to subtract from the
payload, detailed in particular wing’s Pilot Operating handbook, the weight of each
option installed.
5.10.1 Cockpit fairing
A composite shell can be installed on the nose of the tricycle to better protect the crew
from the relative wind. The behavior of the aircraft is not modified by the presence of the
fairing, but the weight of this option reduces the payload of the aircraft by 5 kg (11 lbs).
5.10.2 Parachute
The Skypper can be equipped with a pyrotechnic rocket parachute, inside the special
container placed under the passenger seat.
The parachute will slow the descent of both aircraft and occupants if a major problem
occurs (collision, flight envelope exceeded, etc.). It is advised to use it only as last
resort to save life or prevent injury.
Before starting the engine, the safety cotter pin placed on the launching handle should be removed.
Then it should be replaced after landing, before disembarking, to avoid unintentional firing. It is
recommended to link the engine key with the safety cotter pin, so its removal while using the trike
cannot be forgotten.
Before firing the parachute it is advised, if altitude allows, switching the engine off to avoid
damaging the main bridle with the rotating propeller.
If you cannot stop the engine, it will be stopped at the same time you pull the handle of the
parachute, due to the switch integrated on the handle fitting.
The activating of the rocket motor is made by pulling the red handle located between the pilot’s
legs, on the seat frame.
A strong pull on the handle is needed, at maximum available length.
Always inspect bridle connection points and activation cables before flying; do not
modify them. When rigging the wing, bridles must be fixed with the link shackle.
The recommendations concerning inspection, activation and unloading of the
rocket, maintenance periods and overall care are stated in the user’s manual
provided with the parachute.
The parachute does not change the flight behavior of the aircraft but its weight reduces
the payload by 22 lbs (10 kg).
5.10.3 Dual Control for Instruction
This option allows for control of the ground steering and the engine power from the rear
seat. It allows full control from the rear seat of the aircraft.

GDMUSKevo912IS-2G Version 0010 17
Its weight reduces the payload of the SKYPPER trike by 2.20 lbs (1 kg).
5.10.4 Skis
This option allows use of the trike on packed snow after removing the wheels. The whole
series of wings supports this option.
The additional weight is up to 21 lbs (9.5 kg) and reduces the payload of the trike by the
same amount.
5.10.5 HP (Cross Country)
The HP option, which increases the possibilities of off-road use, consists of 3 ultra-wide
tires. Its weight is up to 5.5 lbs (2.5 kg) and reduces the payload of the trike by the same
amount.
5.10.6 Bush
The Bush version allows the use of unprepared fields. It includes a hydraulic braking
system on the 3 wheels "Beringer" associated with tires of type Aero Classic TT. This
version is not equipped with rear wheel fairings and has an additional side cooling scoop.
The standard propeller is a rainforced Duc Flash-2 MFSH-3-L. Its weight of 5.5 kg (12
lbs) reduces the payload of the tricycle.
5.10.7 Strobes
This option which improves the visibility of the aircraft consists of 2 flashing lights
placed on the side of the wheel fairings. Its weight of 0.5 kg (1 lbs) reduces the payload
of the tricycle.
5.10.8 Oil Thermostat
This option that allows faster engine warm-up consists of a thermostat and different
outputs straight or bent. It is fitted in the luggage compartment next to the oil tank. Its
weight of 0.5 kg (1 lbs) reduces the payload of the trike.
5.10.9 4-points harness
This option that allows a better hold back of the passenger (child, disabled person)
consists of a harness with two shoulder straps. Its weight of 0.5 kg (1.1 lbs) reduces the
payload of the tricycle.
5.10.10 Flight instrument MGL Explorer+SP6+FF
This option allows to concentrate in a single instrument all the engine and flight
parameters as well as the air map. It is installed in replacement of the analog instruments.
Its weight of 1.1 kg (2.4 lbs) is identical to the weight of all the analog instruments and
therefore does not modify the payload of the tricycle.
5.10.11 Flight instrument MGL Xtrem+SP6+FF
This option allows to concentrate in one instrument all the engine and flight parameters.
It is installed in replacement of the needle instruments. The 0.2 kg (0.4 lbs) lower weight
increases the payload of the tricycle.

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5.10.12 Flight instrument MGL MX1+SP6+FF
This option allows to concentrate in a single instrument all the parameters of the engine,
the flight and the air map. It is installed in replacement of the analog instruments. Its
weight of 1.1 kg (2.4 lbs) is identical to the weight of all the analog instruments and
therefore does not modify the payload of the tricycle.
5.10.13 Flight instrument MGL EMS2
This option allows to concentrate in one instrument all the engine parameters. It is
installed in place of the analog instruments. The lower weight of 0.8 kg (1.8 lbs)
increases the payload of the tricycle.
5.10.14 Flight instrument MGL ASV 2
This option allows the pilot to know his air speed in flight, his altitude and his vertical
speed. Its weight of 0.3 kg (0.6 lbs) reduces the payload of the tricycle.
5.10.15 Magnetic Compass Ø57
This instrument allows to visualize the magnetic course followed. Its weight of 0.3 kg
(0.6 lbs) reduces the payload of the tricycle.
5.10.16 Radio Icom A25 + antenna
This option allows the pilot to communicate with the outside environment. Its weight of 1
kg (2.2 lbs) reduces the payload of the tricycle.
5.10.17 Radio Dittel KRT 2 Radio + antenna
This option allows the pilot to communicate with the outside environment. Its weight of
0.6 kg (1.3 lbs) reduces the payload of the tricycle.
5.10.18 ICA 12 or ICA 13 Intercom
This option allows the pilot to communicate with his passenger. Its weight of 0.5 kg (1
lbs) reduces the payload of the tricycle.
5.10.19 Dittel KTX 2 Transponder
This option allows the identification of the aircraft by the air traffic control services. Its
weight of 0.5 kg (1 lbs) reduces the payload of the tricycle.
5.10.20 Propeller
This option allows the use of different propellers. The extra weight of these propellers
reduces the payload of the tricycle. Below are the descriptions and payload reductions
according to the optional models proposed:
Neuform TXL 3-65-47-101.6 -2,5 kg (5.5 lbs)
Neuform CL3-65-(IP)-47-101.6 -2,0 kg (4.4 lbs)
Duc Flash-2 MFSH-3-L rainforced -1,5 kg (3.3 lbs)

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5.11 Specific Use / Safety Instructions
5.11.1 Towing
The towline must include a fuse gauged at 80 daN maximum in order to allow an automatic
release in case of over-tensioning.
Release the towline above a fully clear ground before landing.
Test systematically the releasing device of the trike before take-off.
The ideal speed for towing streamers is 47 mph (75 km/h). In the case of a glider, the speed should
be adapted to its performances. The emergency procedures stated in 5.9 remain applicable; the
towing must be launched above a fully clear field prior to landing. Characteristics, listed in the
applicable wing user’s manual, are diminished due to the drag of towing and flying level requires
a higher engine power. Minimum speed and stall speed remain unchanged.
5.11.2 Load Carriage, Survey Material, Data Transmission,
Photography, Video &c.
Install the loads to be carried on the passenger seat. The holding device has to support efforts up to
9 g forward, 3 g upward et 1.5 g laterally.
Limit the dimensions of the loads carried to avoid any contact, stress marks or blocking with the
wing structure and particularly with the inferior longitudinal cables.
Mounting any kind of camera at the tip of the wing is possible up to a maximum weight of 2 kg if
you install a counterweight at the extremity of the opposite wing. The inertia of the wing on its roll
axis will increase.
The emergency procedures stated in chapter 5.9 remain applicable.
5.11.3 Sky jumpers
Training on the ground is absolutely necessary before take-off.
The skydiver always leaps from the back seat, in normal tandem or "sidesaddle" position, body
perpendicular to the trike axis.
The pilot cuts the engine before the preparatory step of the jump. The skydiver may use the wheel
leg gear as a step.
The emergency procedures stated in 5.9 remain applicable. If altitude allows, the sky jumper will
return to normal position before landing.
5.11.4 Skis
Mounting the ski system in place of the wheels reduces performance globally due to the increase
of drag.
The lack of brakes makes perfect speed management necessary and makes stopping possible only
on a flat surface, engine off.
The emergency procedures stated in 5.9 remain applicable.