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4.2 POSSIBLE CONFIGURATIONS

To become familiar with the possible incidents described below, we 
recommend practising within the environment of a licensed training outfit. 
You must adapt your use of the brakes depending on the wing-loading 
and avoid over-steering.

It is important to note that the type the reaction to an incident can vary 
from one size of wing to another, and even within the same size the 
behaviour and reactions may be different depending on the wing-loading.

In the test report, you will find all the necessary information on how to 
handle your new wing during each of the tested manoeuvres. Having this 
information is crucial to know how to react during these incidents in real 
flight, so you can deal with these situations as safely as possible.

Asymmetric collapse

In spite of the ARTIK 6 ’s profile stability, strong turbulent air may cause 
the wing to collapse asymmetrically, especially in very strong turbulence, 
especially if you do not 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 
on the affected side of the wing. It will increase the incidence of the wing 
(angle of attack). If the collapse does happen, the ARTIK 6 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, try to weight-shift towards the 
collapsed side. If this does not resolve the issue, pull the brake handle 
on the collapsed side decisively and quickly all the way (100%) down 
and release it back up immediately. You may have to repeat this action 
to provoke the re-opening of the collapsed 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 normal flying speed.

Frontal collapse

Due to the ARTIK 6 ‘s design, in normal flying conditions frontal collapses 
are unlikely to take place. 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. 
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.

Negative spin

A negative spin does not conform to the ARTIK 6’s normal flight 
behaviour. Certain circumstances however, may provoke a negative spin 
(such as trying to turn when flying at very low air speed whilst applying 
a lot of brake). It is not easy to give any specific recommendation about 
this situation other than quickly restoring the wing’s default air speed 
and angle of attack by progressively reducing the tension on the brake 
lines. The normal wing reaction will be to have a lateral surge on the re-
accelerated side with a rotation not greater than 360º before returning to 
default air speed and a straight flight path trajectory.

Parachutal stall

The possibility of entering or remaining in a parachutal stall have been 
eliminated from the ARTIK 6.
A parachutal stall is virtually impossible with this wing.  If it did enter into 
a parachutal stall, the wing loses forward motion, becomes unstable 
and there is a lack of pressure on the brake lines, although the canopy 
appears to be fully inflated. To regain normal air speed, release brake line 
tension symmetrically and manually push on the A-lines or weight-shift 
your body to any side WITHOUT PULLING ON THE BRAKE LINES.

Deep Stall

The possibility of the ARTIK 6 stalling during normal flight is very unlikely. 
It could only happen if you are flying at a very low air speed, whilst over-
steering or performing dangerous manoeuvres in turbulent air.

Содержание ARTIK 6

Страница 1: ...ARTIK 6 User s manual...

Страница 2: ...on discover the meaning of our motto The importance of small details This is the user manual and we recommend you read it carefully The Niviuk Team USER S MANUAL This manual provides you with the nece...

Страница 3: ...TAKE OFF 9 3 6 LANDING 9 3 7 PACKING 9 4 IN FLIGHT 10 4 1 FLYING IN TURBULENCE 10 4 2 POSSIBLE CONFIGURATIONS 11 4 3 ACCELERATED FLIGHT 12 4 4 FLYING WITHOUT BRAKE LINES 12 4 5 KNOT S IN FLIGHT 12 5 L...

Страница 4: ...commend pilots read the flight test report carefully especially the comments of the test pilot The report contains all the necessary information on how the paraglider reacts during each of the tested...

Страница 5: ...ely related properties It has shape memory and enormous elasticity This means that the rods maintain their optimum shape even after ultra compact or bad folding so that the wing does not suffer from d...

Страница 6: ...reduces the cohesion of the wing and therefore aerodynamic efficiency The use of these technologies is a big technological leap forward in building wings and a big improvement in flight comfort For t...

Страница 7: ...rresponding risers Make sure that there are no knots 2 3 CONNECTING THE HARNESS The ARTIK 6 risers are colour coded Right green Left red This colour coding makes it easier to connect the wing to the c...

Страница 8: ...the bar that the pilot pushes with their feet as well as the two chords that connect it to the speed system components on the risers Once you have chosen the type of speed bar you prefer you must inst...

Страница 9: ...ffect the trailing edge and slow the glider down without pilot input Both brake lines should be symmetrical and the same length We recommend using a clove hitch or bowline knot When changing the brake...

Страница 10: ...n perfect condition 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 syst...

Страница 11: ...ver brake or slow down the flying side of the wing control the turn Once the collapsed side is open make sure you return to normal flying speed Frontal collapse Due to the ARTIK 6 s design in normal f...

Страница 12: ...apped between the other lines This line has a different colour and is located on the outside position of the B riser Pull this line until it is taut This action will help to release the cravat If inef...

Страница 13: ...brake handles because there will be an increased risk of stalling the wing or entering a negative spin Before attempting to clear a knot make sure there are no other pilots flying in the vicinity 5 LO...

Страница 14: ...deformed After this the physical effort is less Continue to hold the risers in position Once the wing is deformed its horizontal speed will drop to 0 km h vertical descending speed increases to 6 to 8...

Страница 15: ...le the certified equipment to carry out this operation The wing must be inflated similarly as during a normal take off It is important to use the brakes to correct the flight path alignment especially...

Страница 16: ...sed to the sun Pack it properly and stow it away in its backpack If your wing is wet from contact with salt water immerse it in fresh water and dry it away from direct sunlight 7 2 STORAGE It is impor...

Страница 17: ...iuk com content service Any modification of the glider made in an external workshop will invalidate the guarantee of the product Niviuk cannot be held responsible for any issues or damage resulting fr...

Страница 18: ...4 2 2 1 4 2 2 1 4 2 2 1 4 2 3 1 A A B C A A B C A A B C A A B C mm 160 200 200 200 Kg 58 75 70 90 85 105 100 122 Kg 4 3 4 5 4 7 5 C C C C 10 TECHNICAL DATA 10 1 TECHNICAL DATA 20 CELLS Number ASPECT R...

Страница 19: ...PLIER UPPER CASCADES DC 60 LIROS GMHB GERMANY UPPER CASCADES DC 40 LIROS GMHB GERMANY MIDDLE CASCADES DC 60 LIROS GMHB GERMANY MIDDLE CASCADES DC 40 LIROS GMHB GERMANY MIDDLE CASCADES A 8000 U 70 EDEL...

Страница 20: ...10 3 RISERS PLAN 22...

Страница 21: ...10 4 SUSPENSION PLAN 23...

Страница 22: ...0 330 355 385 500 A B C D BR 1 7189 7137 7210 7280 7474 2 7153 7100 7170 7242 7213 3 7112 7058 7131 7201 7063 4 7121 7067 7145 7212 7055 5 7048 6981 7110 7176 6912 6 7011 6945 7054 7120 6775 7 6950 68...

Страница 23: ...0 330 355 385 500 A B C D BR 1 7988 7918 8000 8078 8336 2 7949 7880 7957 8037 8048 3 7907 7837 7917 7995 7884 4 7918 7849 7934 8009 7877 5 7831 7769 7901 7974 7716 6 7791 7729 7840 7913 7566 7 7726 76...

Страница 24: ...um weight in flight kg 70 Speed range using brakes km h 14 Glider s weight kg 4 5 Total speed range with accessories km h 29 Number of risers 3 Range of trimmers cm 0 Projected area m2 19 61 Harness u...

Страница 25: ...9 A 10 C 11 A 12 A 13 B 14 B 15 A 16 A 17 A 18 A 19 A 20 A 21 B 22 A 23 0 ARTIK 6 25 ARTIK 6 27 Classification C In accordance with standards EN 926 1 2015 EN 926 2 2013 and LTF NFL II 91 09 PG_1750 2...

Страница 26: ...niviuk com...

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