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all aspects of flight.
The LINK has the same advantages when landing as it does on take-off. 
With a low speed approach, a short final glide and with the pilot always 
in total control the LINK can land in the smallest of areas with precision 
and ease.
It is worthwhile remembering that the best paraglider in the hands of a 
bad pilot does not guarantee a happy ending. The LINK’s passive safety 
measures should also be accompanied by the passive safety offered 
by the rest of the flying equipment, the harness, helmet the emergency 
parachute etc. The extraordinary behaviour of the LINK and common-
sense piloting will give you many hours of peaceful flying.

1.4 ASSEMBLY, MATERIALS

The LINK does not only introduce new design methods but also new 
manufacturing technologies. Not a single millimetre of error is possible in 
the manufacturing process from Olivier’s computer to the cutting of the 
fabric. The cutting is done section by section in an extremely meticulous 
manner. The numbering and marking of the guideline marks is also done 
in the same meticulous way so avoiding errors in this critical process.

The lines are semi-automatically manufactured and all the sewing is 
finished under the supervision of our specialists.  The jigsaw puzzle of 
the assembly process is made easier using this method. We economise 
on resources while making the quality control more efficient. All the 
different parts of the canopy are cut and assembled under the strict 
conditions induced by the automation of the whole process.  All NIVIUK 
Gliders go through an extremely thorough and efficient final inspection. 
Every single line of each glider is measured individually once the final 
assembly has concluded. 
Each wing is thoroughly inspected at the end of it assembly. Each glider 
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, and 
homologation requirements of the present-day market. 

Information about construction materials is given on the last pages of this 
manual.

1.5 ELEMENTS, COMPONENTS

The LINK is delivered to its owner together with a series of components 
that, although not fundamental do take an important part in the use, 
transport and storage of the paraglider. 
The glider is delivered together with a rucksack large enough for all of 
the equipment to fit inside once appropriately packed. The rucksack is 
designed to make transport on foot as pleasant as possible. The internal 
bag intended to protect the LINK from possible damage during storage 
is also supplied. The glider strap allows the folded wing to be held in 
position. Furthermore you will find an accelerator bar that can be used 
with the LINK, a small fabric repair kit made of auto-adhesive ripstop and 
an instruction booklet with all the basic information about your LINK. You 
will also find a USB pen drive.

1.6 PROFILE

The LINK project demanded a profile which would achieve PPG efficiency 
above traditional profiles taking powered flight forward and into the future. 
The new profile not only advances the understanding of aerodynamics 
and efficiency but also allows the reduction of surface area and the 
materials used:
• The SLE on the leading edge allows an easy inflation even in nil wind 
conditions.
• The LINK inflates easily and immediately ensuring only short low speed 
runs are necessary to take off.
• Once airborne the trim system allows easy and precise adjustment to 
achieve cruising speeds substantially higher than the average in the PPG 
category.
• The trim system has easy read metric markers to allow accurate and 
symmetrical adjustments. 
• The new and efficient profile of the LINK enables the wing to glide 

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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