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The NKare Bag guides you through the folding process, allowing you to 
concertina pack the wing with each rod on top of the other and then fold 
the wing as required. This folding system ensures that both the fabric and 
the reinforcements of the internal structure are kept in perfect condition.

4. IN FLIGHT

We recommend that you read the certification test report. 

The report contains all the necessary information on how the X-ONE 
reacts during each of the tested manoeuvres. 

It is important to point out that the appropriate response to each adverse 
manoeuvre can vary from size to size; even within the same size at 
maximum or minimum load the behaviour and reactions of the wing may 
vary. 

Having the knowledge that the testing house provides through the test 
report is fundamental to learning how to deal with possible situations.

To become familiar with the manoeuvres described below, we 
recommend practising within the auspices of a licensed training outfit.

4.1 FLYING IN TURBULENCE

The X-ONE has an excellent profile to deal with incidents; it is very 
stable in all conditions and has a high degree of passive safety, even in 
turbulent conditions.

All paragliders must be piloted for the prevailing conditions and the pilot 
is the ultimate safety factor.

We recommend active flying in turbulent conditions, always taking 
measures to maintain control of the wing, preventing it from collapsing 
and restoring the speed required by the wing after each correction.

Do not correct the glider (braking) for too long in case this provokes a 
stall. Whenever necessary, control a situation, react to it and then re-
establish the required speed.

4.2 POSSIBLE CONFIGURATIONS

In spite of the X-ONE’s profile stability, strong turbulent air may cause 
the wing to collapse asymmetrically in very strong turbulence, especially 
if the pilot is unable to fly actively and prevent the collapse. In this case 
the glider conveys a loss of pressure through the brake lines and the 
harness. To prevent the collapse from happening, pull the brake handle 
corresponding to the affected side of the wing. It will increase the 
incidence of the wing (angle of attack). If the collapse does happen, the 
X-ONE will not react violently, the turning tendency is gradual and easily 
controlled. Weight-shift toward the open, flying side (the opposite side of 
the collapse) to keep the wing flying straight, while applying light brake 
pressure to that side if necessary. Normally, the collapsed side of the 
wing should then recover and reopen by itself. If it does not, then pull 
the brake handle on the collapsed side decisively and quickly all the way 
(100%) down. You may have to repeat this pumping action to provoke the 
re-opening of the deflated glider side. Do not over-brake or slow down the 
flying side of the wing (control the turn). Once the collapsed side is open 
make sure you return to the default flying speed.

Frontal collapse
Due to the X-ONE’s design, in normal flying conditions frontal collapses 
are extremely unlikely. The wing’s profile has great buffering abilities when 
dealing with extreme incidence changes. A frontal collapse may occur in 
strong turbulent conditions, entering or exiting powerful thermals or when 
lacking experience using the accelerator/ speed-bar without adapting 
to the prevailing conditions. Frontal collapses usually re-inflate without 
the glider turning, but a symmetrically applied quick braking action 
with a quick deep pump of both brakes will accelerate the re-inflation if 
necessary. Release the brake lines immediately to return to default glider 
air speed.

Summary of Contents for ICEPEAK X-ONE

Page 1: ...ICEPEAK X ONE User s manual...

Page 2: ...tails This is the user manual and we recommend you read it carefully USER MANUAL This manual provides you with the necessary information on the main characteristics of your new paraglider Whilst it pr...

Page 3: ...9 3 3 PRE FLIGHT CHECK 9 3 4 WING INFLATION CONTROL AND TAKEOFF 9 3 5 LANDING 9 3 6 PACKING 9 4 IN FLIGHT 10 4 1 FLYING IN TURBULENCE 10 4 2 POSSIBLE CONFIGURATIONS 10 4 3 ACCELERATED FLIGHT 12 4 4 FL...

Page 4: ...ents of the test pilot The report contains all the necessary information on how the paraglider reacts during each of the tested manoeuvres It is important to point out that the appropriate response to...

Page 5: ...es included in this new model RAM Air Intake this system is characterised by the arrangement of the air inlets to ensure optimal maintenance of internal pressure Thanks to this design we were able to...

Page 6: ...eter has been calculated depending on the workload and aims to achieve the required best performance with the least drag The lines are semi automatically cut to length and all the sewing is completed...

Page 7: ...back and a risk of twisting in the case of a violent asymmetric collapse 2 5 CONNECTING THE SPEED BAR The speed bar is a means of temporary acceleration by changing the flow over the profile The speed...

Page 8: ...bar cords directly to the speed system on the risers This last option makes the connection disconnection more laborious but means the cord has maximum travel without obstructions or restrictions whic...

Page 9: ...to overfly the pilot It is a straight forward exercise leaving enough time for the pilot to decide whether to accelerate and take off or not If the wind permits we recommend a reverse launch as this...

Page 10: ...the X ONE s profile stability strong turbulent air may cause the wing to collapse asymmetrically in very strong turbulence especially if the pilot is unable to fly actively and prevent the collapse In...

Page 11: ...he brake lines until reaching the half way point of the total the brake travel The wing will then surge violently forward and could reach a point below the pilot It is most important to maintain brake...

Page 12: ...this causes a stall or negative spin The wing must be flown at full speed during the landing approach and the C risers will have to be pulled symmetrically all the way down shortly before contact with...

Page 13: ...dge turbulence In addition with the length of the chord and the arc of the wing the ears have a tendency to flap increasing the turbulence and causing the paraglider to lose too much airspeed making i...

Page 14: ...erience an asymmetrical acceleration and dive depending on how the manoeuvre was carried out Practise these manoeuvres at sufficient altitude and with moderation 5 4 SLOW DESCENT TECHNIQUE This techni...

Page 15: ...properly and stow it away in its backpack If flying in a sandy environment and sand has accumulated inside the wing remove it before packing it away The apertures at the wing tips facilitate easy rem...

Page 16: ...ecialised personnel 7 4 REPAIRS We recommend any inspection or repair is performed by a Niviuk professional in our official workshop https niviuk com en niviuk service form Any modification of the gli...

Page 17: ...1 1 1 3 1 1 1 3 2 2 A A A B A A A B A A A B A A A B A A A B mm 140 140 140 140 140 kg 80 95 90 105 98 112 108 120 118 133 kg 88 91 100 101 108 109 117 119 128 130 kg 5 9 6 06 6 32 6 65 6 91 CCC CCC CC...

Page 18: ...DE SUPPLIER MATERIAL 3455 COUSIN FRANCE COLOR INDICATOR 210D TECNI SANGLES FRANCE THREAD V138 COATS ENGLAND MAILLONS 3 5 ANSUNG PRECISION KOREA PULLEYS RF25109 RONSTAN AUSTRALIA MIDDLE CASCADES A 8000...

Page 19: ...19 10 3 RISER PLAN...

Page 20: ...12 c11 c10 c9 a13 a12 a11 a10 a9 a8 a14 c13 c14 b8 b9 br1 br11 br10 br9 br8 br7 br6 br5 br4 br3 br2 br13 br12 A1 A2 A 4 A3 A5 A6 A7 A8 A9 2a5 2 a 6 3a3 s t a b 4A1 2a1 2a2 3a1 2a3 2a4 3a2 2c5 2c6 3c3...

Page 21: ...niviuk com...

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