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11

Wing tangle
Of all the possible situations, which you may encounter while flying the 
LINK, this is the least probable one of all. The well-proportioned ratio and 
well calculated positioning of the line cascades ratify this fact.

A wing tangle may happen after an asymmetric collapse, the end of the 
wing is trapped between the lines (Cravat). This situation could rapidly 
cause the wing to turn, although it depends on the nature of the tangle. 
The correction manoeuvres are the same as those applied in the case 
of an asymmetrical collapse, control the turn tendency by applying the 
opposite brake and lean your body against the turn. Then locate the line 
that reaches the stabilizer that is trapped between the other lines. This line 
has a different colour and belongs to the external lines of the C riser.
Pull on this line until it is tense, this should help to undo the wing tangle. 
If you cannot undo the tangle, fly to the nearest possible landing spot, 
control the flying course with your body movements and a little pressure 
on the opposite brake. Be careful when attempting to undo a tangle if you 
are flying near a mountainside or near to other paragliders you may lose 
control of the flying course and a collision may occur.

Over handling
Most flying incidents are caused by incorrect actions of the pilot, which 
in turn creates abnormal flying configurations, usually a cascade of 
incidents. You must to remember that over handling the wing will lead to 
critical levels of functioning. The LINK is designed always to try to recover 
normal flight by itself, do not try to over handle it.
Generally speaking the reactions of the wing which follow over handling 
are neither due to the input made or the intensity but the length of time 
the pilot continues to over handle. You have to allow the profile to re-
establish normal flight speed after any type of handling. 

4.3 USING THE ACCELERATOR

The profile of the LINK has been designed to fly stable through its entire 
speed range. It is useful to accelerate when flying in strong winds or 

in extreme descending air. When you accelerate the wing, the profile 
becomes more sensitive to possible turbulence and closer to a possible 
frontal collapse. If you feel a pressure loss, you should release the 
pressure on the accelerator and pull slightly on the brake lines to increase 
the angle of incidence. Remember that you have to re-establish the flight 
speed after correcting the incidence.
It is NOT recommended to accelerate near to the mountainside or in very 
turbulent conditions. If necessary you will have to constantly adjust the 
movements and pressure on the accelerator whilst constantly adjusting 
the pressure applied to the brake lines. This balance is considered to be 
“active piloting.”
If we choose to fly with the trimmers opened while using the accelerator 
you must fly actively.
 
4.4 FLYING WITHOUT BRAKE LINES

If, for any reason at all, you cannot use the brake lines of your LINK you 
will have to pilot the wing using the D-risers and your body weight to 
fly towards the nearest landing. The D-lines steer easily because they 
are not under pressure; you have to be careful not to over handle them 
causing a stall or negative turn. To land you have to let the wing fly at full 
speed and before reaching the ground you will have to pull symmetrically 
on both the D-risers. This braking method is not as effective as using the 
brake lines so you will land at a higher speed. 

4.5 KNOTS IN FLIGHT

The best way to avoid these knots and tangles is to inspect the lines 
before you inflate the wing for take-off. If you notice a knot before 
takeoff, immediately stop running and do not takeoff.
If you have taken-off with a knot you will have to correct the drift by 
leaning on the opposite side of the knot and apply the brake line on 
that side too. You can gently try to pull on the brake line to see if the 
knot becomes unfastened or try to identify the line with the knot in it. 
Try to pull the identified line to see if the knot undoes. Be very careful 

Summary of Contents for LINK 23

Page 1: ...USER S MANUAL LINK...

Page 2: ...gression the LINK will adapt with your experience We are sure that you will enjoy flying this wing and that you will soon discover the true meaning of our slogan Give importance to the small details t...

Page 3: ...ING INFLATION CONTROL AND TAKE OFF 8 3 6 LANDING 9 4 IN FLIGHT 9 4 1 FLYING IN TURBULENCE 9 4 2 POSSIBLE CONFIGURATIONS 10 4 3 USING THE ACCELERATOR 11 4 4 LYING WITHOUT BRAKE LINES 11 4 5 KNOTS IN FL...

Page 4: ...l freedom The addition of SLE technology with its light weight and structured cells ensures that every inflation and take off remains simple and uneventful Thanks to the LINK s controlled and progress...

Page 5: ...is packaged following the maintenance and conservation instructions recommended for the advanced materials NIVIUK Gliders are made of first class materials as demanded by the performance durability a...

Page 6: ...maillons which attach the lines to the risers are properly closed Identify and if necessary disentangle the lines from A B and C risers the brake lines and the corresponding risers Make sure that ther...

Page 7: ...ry pilot should be aware of the trimmer settings and make any necessary adjustments appropriate to the conditions the terrain and pilot ability In flight The trimmers on the LINK are highly and precis...

Page 8: ...ach the lines to the risers are fully closed Identify and if necessary disentangle the lines from A B and C risers the brake lines and the corresponding risers Check for no ties or knots The correct p...

Page 9: ...ers are closed The LINK very efficiently transforms forward speed into lift and inherently allows a wide margin for error either with or without wind 4 IN FLIGHT We recommend that you read very carefu...

Page 10: ...o recover optimum flight speed Negative spin This configuration is out of the normal flight behaviour of the LINK Certain circumstances however may provoke this configuration such as trying to turn wh...

Page 11: ...le of the LINK has been designed to fly stable through its entire speed range It is useful to accelerate when flying in strong winds or in extreme descending air When you accelerate the wing the profi...

Page 12: ...e which should be avoided more so if you are flying near the ground or flying in turbulence 5 2 B LINE STALL When you carry out this manoeuvre the wing stops flying it loses all horizontal speed and y...

Page 13: ...f piloting that is different to normal flight To learn safely how to master acrobatic manoeuvres you should attend lessons which are carried out and supervised by a qualified instructor over water Ext...

Page 14: ...d checked at your local repair centre every 100 hours of use or every 12 months whichever happens first This will guarantee that your LINK will continue to function properly and therefore continue ful...

Page 15: ...82 3 82 3 82 FLATTENING 15 15 15 15 CORD MAXIMUM 2 56 2 67 2 77 2 9 MINIMUM 0 6 0 62 0 65 0 69 AVERAGE 2 08 2 17 2 25 2 34 LINES TOTAL METERS M 276 294 306 317 HEIGHT M 6 87 7 11 7 41 7 72 NUMBER 218...

Page 16: ...HREAD SERAFIL 60 AMAN GERMANY SUSPENSION LINES FABRIC CODE SUPPLIER UPPER CASCADES TNL 080 EDELRID GERMANY MIDDLE CASCADES TNL 080 TEIJIM LIMITED JAPAN MIDDLE CASCADES TNL 140 TEIJIM LIMITED JAPAN MAI...

Page 17: ...17 11 3 RISER ARRANGEMENT...

Page 18: ...18 11 4 LINE PLAN...

Page 19: ...ENGHT m m A B C D 480 480 480 480 STANDARD 480 480 525 570 TRIMMER OPENED 380 410 440 480 ACCELERATED 11 5 LENGTHS LINK 23 NIVIUK LINK 23 LINES HEIGHT m m A B C D br 1 6380 6300 6320 6430 7000 2 6340...

Page 20: ...ENGHT m m A B C D 480 480 480 480 STANDARD 480 480 525 570 TRIMMER OPENED 380 410 440 480 ACCELERATED 11 8 LENGTHS LINK 29 NIVIUK LINK 29 LINES HEIGHT m m A B C D br 1 7245 7151 7182 7309 7900 2 7199...

Page 21: ...A 8 A 9 B 10 A 11 A 12 A 13 A 14 B 15 A 16 A 17 A 18 A 19 A 20 A 21 B 22 A 23 A 24 0 Class B In accordance with EN standards 926 2 2005 926 1 2006 PG_0451 2011 Date of issue DMY 03 01 2012 Manufacture...

Page 22: ...A 4 A 5 A 6 A 7 A 8 A 9 B 10 A 11 A 12 A 13 A 14 B 15 A 16 A 17 A 18 A 19 A 20 B 21 B 22 A 23 A 24 0 Class B In accordance with EN standards 926 2 2005 926 1 2006 PG_0491 2011 Date of issue DMY 03 01...

Page 23: ...23...

Page 24: ...The importance of small details niviuk com...

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