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We recommend that you try the correct fitting of the acceleration system 
on equipment designed to do this, most paragliding schools have this sort 
of equipment. 

2.6 INSPECTION AND WING INFLATION ON THE GROUND

Once all the equipment has been thoroughly checked and the wind 
conditions are favourable, inflate your LINK as many times as necessary 
in order to become acquainted with the wings behaviour. The LINK 
inflates easily and smoothly. An excess of energy is not necessary and the 
wing will inflate with minimum pressure on the harness when you move 
forward. This may be assisted by using the A lines. Do not pull; merely 
support them as they rise naturally with the movement of the wing. Once 
the wing is in the 12 o’clock position, simply apply correct pressure on the 
brake lines and the LINK will sit over your head.
We recommend placing the wing on the ground in a horseshoe shape 
which in most conditions will facilitate a smooth and easy inflation.

2.7 TRIMMERS

Take off
Thanks to the profile of the LINK, all aspects of take off can be controlled 
using the trimmers.
The SLE system pre-positions the open cells of the leading edge in 
the best possible way assuring a rapid formation the wing profile. This 
contribution is in itself already a huge advantage when attempting to 
take off in nil wind conditions but the correct use of the trimmers at this 
time with further enhance an easy take-off. In nil wind and without the 
application of trimmers the LINK inflates easily and effortlessly. However 
by adjusting the trimmers we can control both the inflation and the speed 
at which the wing rises. We should not confuse the speed of the inflation 
with the speed of the forward run required. It is important to remember 
that the minimum take-off speed is achieved with the trimmers closed and 
as the trimmers are opened more speed will be required.
Therefore every 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 precisely adjustable allowing 
the pilot to either increase speed by opening the trimmers or conversely 
decrease speed by closing them. Each trimmer is equipped with a scale 
clearly numbered so allowing the pilot to easily check and confirm the 
exact setting of each. Each trimmer may be set to compensate for the 
torque effect of the engine allowing fine tuning to ensure the wing remains 
in symmetrical flight. The pilot will very quickly become familiar with 
the scale and after just a few flights be able to optimise every flight by 
adjusting the trimmers to their most efficient setting.  
With the trimmers closed and using just the full range of brake travel the 
LINK is a precise, light to handle and a fun machine to fly.

Landing
The LINK offers the comfort of ending the flight with the perfect landing; 
large areas and long runs are no longer required.
It must be remember that in wind nil conditions the forward ground speed 
encountered may be significantly higher and during landing that speed 
must be decreased as safely as possible. This can be achieved by fully 
closing the trimmers and proportionately applying the brakes. If necessary 
as the pilot reaches the ground a longer run off should also be carried out. 
When landing in moderate wind conditions, the ground speed is reduced 
so a simple and progressive application of the brakes will be enough for a 
perfect landing. 
Landing with open or half open trimmers is possible, but it will be 
necessary to balance the application of the brakes to the position of the 
trimmers and the forward ground speed being experienced. Of course 
open trimmers and an increase in forward ground speed when landing 
may require a larger landing area as opposed to when the trimmers are 
closed.  The LINK very efficiently transforms forward speed into lift and 
inherently allows a wide margin for error either with or without wind. 

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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