Niviuk SKIN User manual

USER’S
MANUAL
SKIN

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NIVIUK GLIDERS & AIR GAMES SL C/ DEL TER 6, NAVE D 17165 LA CELLERA DE TER - GIRONA - SPAIN
TEL. [phone] FAX [phone]
[email protected] www.niviuk.com
SKIN
Flying freely
WELCOME
We want to welcome you to our team and thank you for the condence
you gave to our glider product line.
We would like to share the Niviuk R&D team’s commitment, passion and
emotions, which resulted in the creation of the new SKIN. Our company
is proud of the new carefully designed glider, bringing maximum pleasure
during the pilot progression.
Can a single surface glider offer the same features as a normal glider? Can
it be as easy to handle, versatile and a fun mini-wing at the same time?
Could it be the springboard for a new type of ying? The versatility of the
Skin and its new design are going to surprise you.
We are condent that you will enjoy ying this wing and will soon
understand the meaning of our slogan: “The importance of small details”
This is the user’s manual we recommend you to comprehensively read.
The NIVIUK Gliders Team.
USER’S MANUAL
NIVIUK Gliders SKIN
This manual includes all the necessary information pertaining to the SKIN’s
characteristics but can not be viewed as an instructional handbook and
does not offer the instruction required to pilot this type of wing. Training
can only be obtained at a certied paragliding school.
Please review and read the comprehensive content of the SKIN manual.
Misuse of this equipment could lead to sever injuries or death.

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SUMMARY
WELCOME 2
USER’S MANUAL 2
1. CHARACTERISTICS 4
1.1 WHO IS IT DESIGNED FOR? 4
1.2 CERTIFICATION 4
1.3 IN-FLIGHT BEHAVIOUR 4
1.4 ASSEMBLY, MATERIALS 4
1.5 ELEMENTS, COMPONENTS 5
2. UNPACKING AND ASSEMBLY 5
2.1 CHOOSING THE RIGHT LOCATION 5
2.2 PROCEDURE 5
2.3 HARNESS SETUP 6
2.4 TYPE OF HARNESS 6
2.5 ACCELERATOR ASSEMBLY 6
2.6 INSPECTION AND WING
INFLATION ON THE GROUND 6
2.7 ADJUSTING THE BRAKE LINES
AND TOGGLES 6
3. THE FIRST FLIGHT 7
3.1 CHOOSE THE RIGHT PLACE 7
3.2 PREPARATION 7
3.3 FLIGHT PLAN 7
3.4 PRE-FLIGHT CHECK LIST 7
3.5 WING INFLATION, CONTROL
AND TAKE-OFF 7
3.6 LANDING 7
3.7 FOLDING INSTRUCTIONS 7
4. IN FLIGHT 7
4.1 FLYING IN TURBULENCE 7
4.2 POSSIBLE CONFIGURATIONS 8
4.3 USING THE ACCELERATOR 8
4.4 FLYING WITHOUT BRAKE LINES 8
4.5 LINE TANGLES IN FLIGHT 8
5. LOSING HEIGHT 9
5.1 EARS 9
5.2 SPIRAL DIVE 9
5.3 SLOW DESCENT TECHNIQUE 9
6. SPECIAL METHODS 10
6.1 TOWING 10
6.2 ACROBATIC FLIGHT 10
7. CARE AND MAINTENANCE 10
7.1 MAINTENANCE 10
7.2 STORAGE 10
7.3 CHECKS AND CONTROLS 11
7.4 REPAIRS 11
8. SAFETY AND RESPONSIBILITY 11
9. GUARANTEE 11
10. TECHNICAL DATA 12
10.1 TECHNICAL DATA 12
10.2 MATERIALS DESCRIPTION 13
10.3 RISERS LAYOUT 14
10.4 LINE PLAN 15
10.5 LENGTHS SKIN 16 16
10.6 LENGTHS SKIN 18 16
10.7 LENGTHS SKIN 20 17

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1. CHARACTERISTICS
1.1 WHO IS IT DESIGNED FOR?
The SKIN targets adventurous hike&y passionate mountaineer pilots,
and chose challenging distance crossings as their option. The glider’s
great ying ability does not compromise safety, and will let the pilot
explore the landscape either from a bird’s point of view or on foot while
carrying very light and low volume gear.
We want to emphasize the fact that the Skin is not just a descent
paraglider. Its excellent features enable it to thermal, glide and accelerate
(12 cm accelerator). It is an easy and accessible glider for all pilots with
a minimal amount of ying experience.
Only regional qualied schools can certied pilots.
1.2 CERTIFICATION
The SKIN’s load test conducted by the laboratory Air-Turquoise in
Switzerland, exceeded 8 G of force.
1.3 IN-FLIGHT BEHAIVOR
Niviuk developed the Skin by adopting very dened guidelines: the
objective was to seek utmost performance while minimizing gear weight
and volume for easy transportation, harmonize sensations, facilitate
piloting, and above all, maintain a very high wing safety level.
The glider prole was optimized to transmit maximum information in
a very understandable and convenient way, helping the pilot focus on
synchronizing feelings and technique.
The SKIN’s prole is solid. No unwanted surprises with sudden up
or down motions even when pushing the speed-bar full-out during
acceleration. The glide remains high and stable. The turn is accurate,
less physical and easy to activate without much needed amplitude. Each
ination is easily made, wind or not, and the glider has a great ability to
takeoff from tight mountainous rough terrains. The landing is smooth and
precise.
Flying the SKIN quickly becomes very intuitive, with plenty of nuances
and clear references to the state of the air mass. The glider will react to
pilot input effectively even in turbulent conditions, and remain solid.
The wing reads the air mass effectively and cores thermal progressively.
Easy to control in all ying conditions, passive by nature, it will further the
pleasure of soaring and convey a blissful sense of pure freedom
It is light in ight, easy to handle, well behaved in turbulence and has a
surprising speed range added to a superb glide.
1.4 ASSEMBLY, MATERIALS
The SKIN has all the technological innovations used and found in other
Niviuk gliders. The SLE, DRS and TNT technologies are part of its design
and greatly enhance its performance level.
SLE.- The use of the SLE (Structured Leading Edge) allows reinforcement
of the leading edge, preventing any deformation in turbulence. The
airow is also vastly improved over the entire leading edge of the glider.
DRS.-The trailing edge was reinforced with small ribs to atten it and
distribute the pressure out evenly for better air-ow and less drag on this
important part of the glider. Using the ribs gives exceptional handling
abilities for precise more efcient turns.
TNT.- A revolutionary technique developed using Nitinol to build the
internal structure of the glider, brings a more uniform prole, and hence
reduces the overall wing weight to gain efciency in ight. The Nitinol

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provides the highest level of resistance against deformation, heat or
breaks.
Using this technological advance, the glider is able to maintain its original
features for a longer period of time.
The SKIN’S line cascade layout uses Aramid Edelrid for the upper lines,
and TNL Cousin for the middle and lower lines. This tested and proven
layout combination is the same used with other Niviuk models.
The Aramid lines are not sheathed and thus more exposed to abrasive
materials often found in mountainous terrains. This particularity demands
a specic maintenance schedule as a result. A glider inspection must
be conducted at a certied facility, to check the integrity of the trailing
edge every 100 ying hours. In spite of using high quality technologically
advanced materials, rigorous regular control must be performed before
each ight.
The fabric used to manufacture the glider is light, resistant and durable
and will not experience colour loss.
From Olivier’s computer to fabric cutting, the operation is a zero
tolerance process. An automated computer laser-cutting robotic
arm creates each of the many sections needed to complete the wing
assembly. This program also paints the guideline markers and numbers
each individual fabric piece.
The lines are semi-automatically cut to length and all the sewing is
completed under the supervision of our specialists. The jigsaw puzzle
assembly is rendered easier using this method and minimizes the
operation while making the quality control more efcient.
All NIVIUK Gliders go through an extremely thorough and efcient nal
inspection. Every line is checked and measured once the nal assembly
is concluded. Each wing is then individually inated for the last visual
check.
Each glider is packaged following specic maintenance instructions
recommended by the fabric manufacturer.
NIVIUK Gliders are made of rst materials Information about the various
materials used to manufacture the wing can be reviewed on the last
pages of this manual.
1.5 ELEMENTS, COMPONENTS
The SKIN is delivered with a small fabric repair kit including self adhesive
ripstop matching the wing’s colour scheme, and maillon blocker
replacements.
2. UNPACKING AND ASSEMBLY
2.1 CHOOSING THE RIGHT LOCATION
We recommend unpacking and assembling the wing on a training hill
or a at clear area without too much wind and obstacle free. Meeting
those conditions will help with the necessary steps required to check and
inate the SKIN.
We recommend for a qualied instructor to be present and supervise the
entire procedure.
2.2 PROCEDURE
Take the paraglider out of the rucksack, open and unfold it on the ground
with the lines positioned atop the underside facing the sky. Display the
wing in a crescent shape with the cells intakes pointing upwind as if
you were to inate it. Check the condition of the fabric and the lines for
abnormalities. The maillons, attaching the lines to the risers must be fully
closed. Untangle all the lines if necessary as they must be visible and
obstruction free.

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2.3 HARNESS SETUP
Correctly connect the risers to the harness’s carabiners. The risers and
lines should not have any twists and be displayed in the right order.
Check for the harness buckles to be fully locked and secured in place.
2.4 TYPE OF HARNESS
The SKIN can be own with most of the harnesses found on the market
today, including the cocoon style models.
We strongly recommend adjusting the distance between the chest
strap carabiners according to the settings used during the certication
procedure. The distance will vary according to the size of the chosen
harness model.
Incorrect chest strap adjustments can greatly affect glider behaviour. Too
wide a distance between the carabiners will provide greater feedback from
the wing but less glider stability. Too narrow a distance will not bring as
much feedback in addition to increasing the risk of experiencing a riser
twist during a collapse.
2.5 ACCELERATOR ASSEMBLY
The speed-bar is included with the wing. On delivery the accelerator is
not attached to the glider but most harnesses are speed-bar ready. It
must be installed and correctly adjusted. When setting up any type of
speed-bar to the wing, check rst for the harness to be compatible and
equipped with all the necessary hardware to complete the installation as
recommended by the manufacturer. After completion, the speed-bar lines
must be adjusted to the correct distance for a full acceleration relative to
the pilot’s leg length.
We recommend testing the speed-bar adjustment and functionality in a
hang-test device which most schools are equipped with. To accelerate
the SKIN, the pilot must extend his legs and push on the speed-bar with
his feet.
2.6 INSPECTION AND WING INFLATION ON THE GROUND
Once all the gear is checked and deemed safe to use, inate the SKIN,
and ground handle it as much as possible to become familiar with the
wing’s behaviour. Aggressive inations are not necessary as the wing will
climb overhead with minimum tension on the risers. Gently holding the
“A” risers upward while moving upwind is all that is needed for a smooth
progressive climb of the wing. Once positioned and ying overhead, use
the toggles to apply the appropriate tension on the brake lines to keep
the SKIN stationary.
2.7 ADJUSTING THE BRAKE LINES AND TOGGLES
The lower brake lines length is pre-adjusted at the factory and identical
to the ones used during the glider certication procedure. However, that
length can be modied to the pilot’s personal preference. We nevertheless,
recommend keeping the default factory settings as is, and adapt yourself
to the SKIN’s behaviour instead.
If you decide to change the length of the brake lines, untie the knot, slide
the line through the brake link to the desired length, and strongly re-tie the
knot. Qualied personnel should carry out this adjustment. Ensure that the
adjustment does not slow down the glider without any pilot input. Both
brake lines should be symmetrical and have the same lengths. The most
recommended knots are the clove hitch knot or bowline knot.
When changing the brakes line lengths, make sure they do not gain
tension while the accelerator/speed-bar is pushed. During the acceleration
the wing pitches down over the “D” risers axis, and the trailing edge goes
up. The brake lines length must be carefully adjusted taking the extra
length into account during acceleration.

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3. THE FIRST FLIGHT
3.1 CHOOSE THE RIGHT PLACE
The rst ights with the SKIN should be made in low wind speeds,
on a training hill or obstacle free area. We recommend for a qualied
instructor to be present and supervise the entire procedure.
3.2 PREPARATION
Repeat the procedures detailed in chapter 2 UNPACKING AND
ASSEMBLY to prepare your equipment.
3.3 FLIGHT PLAN
Planning a ight before taking off to avoid possible problems later, is
always a good idea.
3.4 PRE-FLIGHT CHECK LIST
Once ready, but before taking off, conduct another equipment inspection.
Give a thorough visual check to your gear to ensure that all is in working
order as it should, with the wig fully open, the lines untangled and properly
laid out on the ground. Be certain the weather conditions are suited for
your ying skill level.
3.5 WING INFLATION, CONTROL AND TAKE-OFF
Smoothly and progressively inate the wing (chapter 2.6 INSPECTION
AND WING INFLATION ON THE GROUND). The SKIN comes up easily,
without excessive handling energy and does not overy the pilot. It is
a straight forward exercise leaving enough time for the pilot to decide
whether to accelerate and take off or not.
Whenever the wind speed permits it, we recommend using a reverse
launch technique more conducive to carry out a better visual check of
the wing. The SKIN is especially easy to control during reversed inations
in windier conditions. However, wind speeds up to 25 to 30 km/h are
considered strong and extra consideration should be given as whether or
not to y.
Setting up the wing on the ground before takeoff is especially important.
Choose an appropriate location pointing into the wind. Position the
paraglider in a crescent conguration to facilitate ination. A clean wing
layout will ensure a trouble free take-off.
3.6 LANDING
The SKIN lands easily with a faire amount of ground effect on demand by
wrapping one’s hands a few times for greater braking efciency.
3.7 FOLDING INSTRUCTIONS
The SKIN has a complex leading and trailing edge manufactured using a
variety of different materials. A correct folding method is very important to
follow to extend the useful life of your paraglider. It should be arranged in
an accordion-like shape, with the leading edge reinforcements at and the
Nitinol exible rods stacked up atop one another. This method will keep
the prole in its original shape and protect the integrity of the wing over
time.
The wing should then be folded in three sections while taking care of not
bending or twisting the SLE. There is no need for compression during the
procedure; doing so may damage the fabric, including the risers and lines.
4. IN FLIGHT
4.1 FLYING IN TURBULENCE

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The SKIN has a sturdy prole able to withstand various aerological
conditions under pilot’s command. It reacts admirably in passive ights,
and brings a high level of safety in turbulent conditions. Nonetheless,
the pilot must always handle the wing according to the conditions of the
moment. Active piloting is the ultimate safety factor.
Necessary ne braking adjustments to keep the wing under control must
constently be made to let the glider y at the required air speed.
Do not maintain any correction longer than necessary (brake input) which
could cause the wing to enter an unwanted and possibly dangerous
ying conguration. Always remain in control and re-establish the
required air speed when necessary.
4.2 POSSIBLE CONFIGURATIONS
Training to master these manoeuvres must be learned in a school
environment.
Asymmetrical collapse
In spite of having a very stable prole, heavy turbulent conditions may
cause part of the wing to deate asymmetrically with the brake lines
and the harness transmitting a tension lose to the pilot. To prevent the
collapse from happening, pulling the brake line on the compromised
side of the wing will increase the angle of incidence. If the collapse does
happen the SKIN does not react violently; its turning motion becomes
gradual and easy to control. Weight shift toward the opposite side of
the compromised half wing, and keep a straight ight path as soon as
possible. If necessary slightly slow the ying side down by braking lightly.
The collapse will normally reopen by itself. If that does not happen, rmly
pump the brake line on the collapsed side using the brake toggle. Repeat
the motion until the deation fully reopens. Do not over brake on the
pressurized remaining ying side while correcting the compromised half
of the wing.
Symmetrical collapse
During normal ying conditions, the SKIN design makes symmetrical
collapses quite improbable. The wing’s prole was designed to handle
wide variations of the angle of attack. A collapse could take place in
heavy turbulent conditions, entering/exiting strong thermals or misusing
the accelerator. Symmetrical collapses usually re-inate without the glider
turning; even pressure applied onto both brake lines with a rapid deep
pumping action of the toggles will also quicken the re-ination. Release
the brake lines tension (hands up) immediately to return to the default
glider air speed and ying conguration.
Negative spin
This conguration goes beyond the SKIN’s normal ight behaviour.
Unusual circumstances can however provoke this conguration such as
trying to turn when ying at close to minimum air speed (heavy into the
brakes). It is not easy to give any recommendations about this situation
as it varies depending on the circumstances of the moment. Remember
to restore the relative air speed over the wing by progressively reducing
brake lines tension and let the wing regain its default wind speed. The
wing’s natural reaction would be to surge laterally with a turning radius no
greater than 360º before returning to normal ight conditions.
Parachutal stall
Close to be an impossibility with the SKIN
Deep stall
The possibility of the SKIN falling into this conguration during normal
ight is very unlikely. It could only happen if you are ying at a very
low air speed, whilst over steering, entering dangerous manoeuvres in
turbulent air. To provoke a deep stall, the wing has to be slowed down to
its minimum air speed by symmetrically pulling the brake lines all the way

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down until the stall point is reached and held there for a few seconds. The
glider will rst pitch rearward and then reposition itself overhead, rocking
slightly, depending on how the manoeuvre was done. When entering a
stall, remain clear minded and ease off the brake lines upon reaching the
half-way point during the downward pulling motion. The wing will then
surge violently forward and could reach a point below the horizontal line. It
is most important to maintain brake pressure until the glider has returned
to its default overhead ying location.
To resume normal ight conditions, progressively and symmetrically
release the brake lines tension to regain air speed. When the wing reaches
the overhead position, the brakes must be fully released. The wing will
then surge forward to regain full air speed. Do not brake excessively as
the wing needs to accelerate to pull away from the stall conguration. If
you have to control a possible symmetrical front stall (frontal collapse),
briey pull both toggles down to bring the wing back up and release
them immediately while the glider is still in transition to reposition itself
overhead.
Wing tangle
Beware when attempting to untangle a wing while ying near a
mountainside or near other paragliders as you may lose control of the
ight path trajectory and a collision could occur as a result.
Over handling
Most ying incidents are caused by incorrect pilot impute, which could
cascade into abnormal ying congurations. Over handling could lead a
wing to violently react. The SKIN was designed to return to a normal ight
conguration by itself, do not try to over handle it.
Generally speaking, the following reactions of the wing are neither due
to the input given nor its intensity, but rather by the length of time it is
applied. The aircraft’s should regain its default ying conguration and air
speed without excessive corrections.
4.3 USING THE ACCELERATOR
The SKIN was designed to sturdily y through its entire speed range. It is
useful to accelerate when ying in strong winds or in extreme katabatic
air. When increasing the glider’s air speed, its prole becomes more
sensitive to turbulence and closer to a possible frontal collapse. A feeling
of weakening internal cell pressure should be taken as a warning, and be
counteracted by releasing the tension on the foot accelerator (speed-bar)
in addition to braking slightly, pulling the brakes/toggles down, to increase
the angle of attack while letting the glider regain its default air speed.
It is NOT recommended to accelerate near obstacles or in highly turbulent
air. If necessary to accelerate, ying actively while moderating the
accelerator pressure and monitoring brake pressure will be the wisest
course of action to take.
4.4 FLYING WITHOUT BRAKE LINES
If for any particular reason the SKIN’s brakes/toggles become disable
and prevent steering, using the D-risers and body weight shifting will
be the only recourse to reach the nearest LZ (Landing Zone) as soon as
possible. Steering with the D-risers is easily done for not being under too
much tension, however, one must be mindful not to over handle them to
the point of causing a stall or negative turn. To land, the wing will come
in at full air speed (hands up), then both “D” risers will be pulled down
evenly and symmetrically before touch down. This braking method is not
as effective as when using the brake line toggles, and hence the wing will
experience a higher than normal air speed, forcing the pilot to run faster
upon touching down.
4.5 LINE TANGLES IN FLIGHT
The best way to avoid knotted lines and tangles is to inspect them before
inating the wing for take-off. If a problem is spotted in the line cascades

10
overhead during the running phase, an immediate stop must take place
to abort launch.
If the problem is discovered after takeoff, a possible drift of the wing
could take place on the knotted side of the wing. The drift will have to be
compensate by leaning toward the opposite side glider while applying
a slight amount of brake to keep a straight ight path. A gentle pull of
the brake line can be made in an attempt to loosen the tangle. If located
elsewhere under the wing, and if the line(s) can be reached, gently pull
a few times on it to see if the problem can be solved. Beware not to
exert too much tension on the the line(s), and risk stalling or initiating a
negative turn as a result.
Before trying to remove a knot or line tangle while ying, always mind
the possible presence of other pilots in the vicinity, and do not make the
attempt to work on the problem while ying near obstacles. If the knot is
too tight it will not be possible to loosen it; carefully y to the nearest LZ
(Landing Zone).
5. LOSING HEIGHT
Knowledge of different descent techniques could become vital in certain
situations. The most adequate descent method will depend on the
particular situation.
It is well advised to learn the particularities of these manoeuvre under the
supervision of a knowledgeable certied instructor.
5.1 EARS
Big ears is a moderate descent technique, able to increase the sink
rate to –3 or –4 m/s, and reduce the ground speed down to 3 to 5 km/.
Effective piloting then becomes limited. The angle of attack and load will
also increase due to the smaller surface area of the wing. Pushing on the
accelerator/speed-bar will partially restore the wing’s horizontal speed
and angle of attack.
To activate the “Big ears” manoeuvre, pull the outer lines 3A3
connected to both “A” risers outward, then downward, evenly,
smoothly and simultaneously. The wingtips will fold in. Let go of the
lines to reinate them automatically. If they do not, gently pump them
open asymmetrically and sequentially, not to alter the angle of attack,
especially when ying near obstacles or ying in turbulent air.
5.2 SPIRAL DIVE
A more effective way to rapidly loose altitude. A wing can loose altitude
quite rapidly during a spiral dive. As a result, the (G force) can increase
to the point of causing the pilot to consciousness (blackout). These are
the reasons why it is best to enter this manoeuvre gradually. It is possible
to eventually build the capacity to resist a certain amount of G force and
fully appreciate and understand a spiral dive. Always and only practice at
high altitude and with enough ground clearance.
To start the manoeuvre, rst weight shift and pull the brake/toggle
located on the inner side of the turn. The intensity of the turn can be
controlled by braking slightly on the outer and upper toggle.
A paraglider ying at its maximum rotating speed can reach –20 m/s, or
the equivalency of a 70 km/h vertical descent, and stabilize in a spiral
dive from 15 m/s onwards. Good enough reasons to familiarize yourself
with the manoeuvre and understand how to exit it.
To exit this manoeuvre, progressively release the brake/toggle located
on the inside of the turn, and momentarily apply a slight amount of brake
on the upper outer toggle. Weight shifting toward the outside of the turn
must be performed at the same time, smoothly and gradually, while
moderating and controlling any glider surge. Always to be practiced at
high altitude and with enough ground clearance.

11
5.3 SLOW DESCENT TECHNIQUE
During a normal slow circling descent versus spiraling down at great
speed, the stress exerted on the gear and the pilot will be kept at a
minimum. The low speed turning technique is similar to climbing in a
gentle thermal but circling downward instead to gradually loose altitude.
Keeping the glider in calm katabatic air will promote an easy low speed
descent and give time to the pilot to make a safe landing approach.
6. SPECIAL METHODS
6.1 TOWING
The SKIN does not experience any problem whilst being towed. Only
a qualied towing operator should be in charge of operating a certied
paragliding winch. The towed wing is inated the same way used during a
mountain ight takeoff.
Any corrections should be made softly to stay away from a high angle of
attack and prevent a possible spin or stall while under tow.
6.2 ACROBATIC FLIGHT
Although the SKIN was tested by expert acrobatic pilots in extreme
situations, it WAS NOT been designed for acrobatic ight manoeuvres.
DO NOT USE THIS GLIDER for aerobatic manoeuvres. We consider
aerobatic ight, any form of piloting reaching beyond the realm of
standard easy going ight. To learn safely how to master aerobatic
manoeuvres, instruction must be taken at a certied school, and under
the guidance of a qualied instructor in a safe environment.
A complete wing and line inspection should be done every six months,
including repairs if necessary to guaranty the integrity of the equipment.
Extreme manoeuvres take you and your wing to centrifugal forces that
can reach 4 to 5g.
7. CARE AND MAINTENANCE
7.1 MAINTENANCE
Regular scheduled gear maintenance will ensure its continued
performance.
Thorough pre-ight checks before taking off are not optional but rather
mandatory.
If in doubt about the gear’s integrity, frayed line, damaged ripstop, loose
stitches, etc..., do not takeoff and have the wing inspected and repaired
at a certied outt if necessary and as soon as possible.
If the wing lands leading edge rst and impacts the ground while still fully
or even partially inated, fabric damage could ensue as a result.
The combination of sheathed and unsheathed suspension lines demands
great care and attention to maintain the glider state at its highest degree
of functionality.
The fabric and the lines do not need to be washed. If cleaning is needed,
use a damp wet cloth. Do not use any caustic cleaning agents.
If the wing was in contact with salt water, wash it with fresh water and
dry it away from harmful direct sunlight. Exposure to UV. will prematurely
age the gear. After landing, never keep the glider exposed to the sun’s
UV rays. It should be stowed away or covered immediately for protection.
If the wing is own in a sandy environment and sand enters the caissons,
dump it out before packing the glider away.
7.2 STORAGE

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It is important for the wing to be correctly folded when stored. Stow
the gear away in a cool, dry place, away from harmful agents. It is not
advisable to store any ying equipment in the trunk of a vehicle left to
bake in the sun, when temperatures inside a backpack possibly reaching
60ºC. Weight should not be applied atop the equipment.
If the ying gear is stowed away in direct contact with organic materials
(such as leaves or insects), a chemical reaction could take place and
cause irreparable damage.
7.3 CHECKS AND CONTROLS
The SKIN must be periodically serviced. An inspection must be
scheduled every 100 ying hours or every twenty four months (whichever
comes rst). Regular maintenance is the only way to guarantee the
SKIN’s integrity and keep it functioning as it should while still conforming
with the certication criteria.
The SKIN is partly built with unsheathed lines. Their durability falls within
the load standards in that category. Their resistance against UV damage
is among the highest for this type of material.
The combination of sheathed and unsheathed lines requires great
attention in use and maintenance to keep the integrity of the SKIN
by following scheduled inspections. Even minute line length and
strength variations, sheathed or not, will have a direct effect on glider
performance.
7.4 REPAIRS
If the wing is damaged, you can temporarily repair it by using the ripstop
material found in the repair kit, so long as no stitches are involved in the
tear, otherwise the damaged area must be repaired in a specialized repair
shop and qualied personnel. Do not accept a home repair.
8. SAFETY AND RESPONSIBILITY
It is well known that paragliding is considered a high-risk sport, where
safety depends on the person who is practicing it.
Wrong use of this equipment may cause severe injuries to the pilot,
and even death. Manufacturers, dealers and representatives can not be
rendered responsible for any act or accident that may result out of of
practicing this sport.
This equipment cannot be used without prior training. Do not take advice
or accept any informal training from anyone who is not properly qualied
or certied as a ight instructor.
9. GUARANTEE
The entire equipment and components are covered by a 2-year
guarantee against any manufacturing defect.
The guarantee does not cover misuse or abnormal use of the materials.
DISCLAIMER:
Paragliding is an activity requiring attention, specic knowledge and
sound judgment. Beware! Learn your skills under the supervision and
guidance of a certied approved school. Contract a personal insurance,
become a licensed pilot. Be humble when evaluating your prociency
level in respect to weather conditions before deciding on whether or not
to y. NIVIUK’s liability coverage is for its product line only. NIVIUK can
not be rendered responsible for your own actions. Fly at your risk!

10. TECHNICAL DATA
10.1 TECHNICAL DATA
SKIN 16 18 20
CELLS NUMBER 39 39 39
BOX 39 39 39
FLAT AREA m216 18 20
SPAN m 9,38 9,95 10,5
ASPECT RATIO 5,5 5,5 5,5
PROJECTED AREA m213,5 15,2 16,9
SPAN m 7,46 7,92 8,34
ASPECT RATIO 4,13 4,13 4,13
FLATTENING % 15 15 15
CORD MAXIMUM m 2,11 2,24 2,37
MINIMUM m 0,44 0,46 0,49
AVERAGE m 1,71 1,81 1,9
LINES TOTAL METERS m 356 378 399
HEIGHT m 5,9 6,3 6,6
NUMBER 388 388 388
MAIN 3/3/4/2 3/3/4/2 3/3/4/2
RISERS NUMBER 4 A/B/C/D A/B/C/D A/B/C/D
TRIMS NO NO NO
ACCELERATOR m/m 120 120 120
TOTAL WEIGHT MINIMUM kg 60 70 85
IN FLIGHT MAXIMUM kg 85 95 110
GLIDER WEIGHT kg 2,3 2,6 2,9
CERTIFICATION EN 926-1 926-1 926-1
12

10.2 MATERIALS DESCRIPTION
CANOPY FABRIC CODE SUPPLIER
UPPER SURFACE 9017 E25 PORCHER IND (FRANCE)
BOTTOM SURFACE 9017 E25 PORCHER IND (FRANCE)
RIBS 9017 E29 PORCHER IND (FRANCE)
LOOPS LKI - 10 KOLON IND. (KOREA)
REINFORCEMENT LOOPS 9017 PORCHER IND (FRANCE)
TRAILING EDGE REIFORCEMENT MYLAR 20 D-P (GERMANY)
REINFORCEMENT RIBS LTN-0.8 STICK SPORTWARE CO.CHINA
THREAD SERAFIL 60 AMAN (GERMANY)
SUSPENSION LINES FABRIC CODE SUPPLIER
UPPER CASCADES DC - 40 LIROS GMHB (GERMANY)
UPPER CASCADES 8000/U - 50 EDELRID (GERMANY)
MIDDLE CASCADES DC - 40 LIROS GMHB (GERMANY)
MIDDLE CASCADES 8000/U - 70 EDELRID (GERMANY)
MIDDLE CASCADES 8000/U - 90 EDELRID (GERMANY)
MIDDLE CASCADES TNL-80 TEIJIM LIMITED (JAPAN)
MIDDLE CASCADES TNL-140 TEIJIM LIMITED (JAPAN)
MAIN TNL-140 TEIJIM LIMITED (JAPAN)
MAIN TNL-220 TEIJIM LIMITED (JAPAN)
MAIN BREAK TNL-280 TEIJIM LIMITED (JAPAN)
THREAD SERAFIL 60 AMAN (GERMANY)
RISERS FABRIC CODE SUPPLIER
MATERIAL WD103 COUSIN (FRANCE)
COLOR INDICATOR PAD TECNI SANGLES (FRANCE)
THREAD V138 COATS (ENGLAND)
MAILLONS MRI4 ANSUNG PRECISION (KOREA)
PULLEYS PY - 1304-2 ANSUNG PRECISION (KOREA)
13

10.3 RISERS LAYOUT
14

10.4 LINE PLAN
15

10.5 LENGTHS SKIN 16 10.6 LENGTHS SKIN 18
LINES HEIGHT m/m
A B C D E F br
1 5470 5435 5391 5402 5441 5512 5770
2 5408 5374 5323 5335 5363 5397 5602
3 5394 5361 5314 5321 5342 5390 5573
4 5365 5332 5283 5283 5324 5368 5507
5 5367 5336 5282 5281 5318 5350 5418
6 5411 5381 5332 5325 5363 5431 5425
7 5346 5314 5275 5274 5321 5392 5359
8 5271 5242 5195 5199 5243 5275 5290
9 5246 5220 5174 5179 5226 5266 5251
10 5224 5198 5154 5158 5206 5242 5278
11 5208 5187 5141 5146 5198 5220
12 5228 5210 5172 5172 5232 5283
13 5151 5125 5094 5089 5109 5171
14 5063 5043 5007 5016 5034 5067
15 5006 4992 4957 4973 4993 5033
16 4947 4933 4900 4917 4932 4968
17 4895 4888 4855 4868 4883 4914
18 4878 4877 4842 4846 4860 4885
19 4715 4685 4697 4714 4740
20 4654 4668 4681 4717
RISERS LENGHT m/m
A B C D
480 480 480 480 STANDARD
360 390 435 480 ACCELERATED
120 90 45 0 TRAVEL
LINES HEIGHT m/m
A B C D E F br
1 5831 5794 5746 5758 5801 5875 6152
2 5766 5730 5676 5688 5718 5754 5975
3 5753 5718 5667 5674 5698 5748 5946
4 5723 5688 5636 5636 5680 5726 5878
5 5726 5693 5636 5634 5673 5707 5785
6 5773 5742 5690 5681 5723 5794 5793
7 5705 5671 5630 5629 5679 5754 5725
8 5627 5596 5546 5551 5597 5630 5653
9 5601 5573 5525 5530 5579 5622 5613
10 5578 5551 5504 5508 5559 5597 5642
11 5562 5539 5491 5496 5550 5574
12 5584 5564 5525 5524 5587 5640
13 5502 5474 5442 5436 5458 5523
14 5409 5387 5350 5359 5378 5413
15 5349 5334 5296 5314 5335 5377
16 5285 5271 5236 5255 5270 5308
17 5231 5223 5189 5203 5219 5252
18 5212 5212 5175 5180 5194 5221
19 5041 5008 5020 5038 5066
20 4975 4990 5004 5042
RISERS LENGHT m/m
A B C D
480 480 480 480 STANDARD
360 390 435 480 ACCELERATED
120 90 45 0 TRAVEL
16

10.7 LENGTHS SKIN 20
LINES HEIGHT m/m
A B C D E F br
1 6172 6133 6082 6094 6141 6220 6514
2 6104 6066 6009 6022 6055 6093 6329
3 6092 6054 6001 6008 6034 6087 6300
4 6061 6024 5969 5969 6016 6065 6229
5 6065 6031 5970 5968 6010 6046 6132
6 6116 6083 6028 6019 6063 6138 6142
7 6046 6010 5966 5965 6018 6097 6065
8 5964 5931 5878 5883 5932 5967 5994
9 5936 5907 5856 5861 5913 5958 5952
10 5913 5884 5835 5839 5892 5932 5984
11 5897 5872 5822 5827 5883 5908
12 5920 5900 5858 5858 5923 5979
13 5835 5805 5772 5767 5790 5860
14 5735 5711 5671 5679 5695 5729
15 5672 5656 5617 5636 5657 5701
16 5606 5590 5555 5574 5590 5630
17 5549 5541 5504 5519 5537 5572
18 5529 5528 5490 5496 5511 5539
19 5348 5314 5327 5346 5375
20 5279 5295 5309 5349
RISERS LENGHT m/m
A B C D
480 480 480 480 STANDARD
360 390 435 480 ACCELERATED
120 90 45 0 TRAVEL
17

The importance of small details
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