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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 manoeuvres in 
real flight, so you can deal with these situations as safely as possible.

Asymmetric collapse

In spite of the LINK 2’s profile stability, strong turbulent air may cause 
the wing to collapse asymmetrically 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 LINK 2 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 normal flying speed.

Frontal collapse

Due to the LINK 2’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 LINK 2’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 LINK 2. 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 LINK 2 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.

To provoke a deep stall, the wing has to be slowed down to its minimum 
air speed by symmetrically pulling the brake lines all the way (100%) 
down until the stall point is reached and held there. The glider will first 
pitch rearward and then reposition itself overhead, rocking slightly, 
depending on how the manoeuvre is done. 

When entering a stall, remain clear-headed and ease off the brake lines 

Summary of Contents for LINK 2

Page 1: ...LINK 2 User s manual ...

Page 2: ...oment in the air The perfect LINK 2 your passion and pleasure We are confident you will enjoy flying this glider and will soon 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 MANUAL This manual provides you with the necessary information on the main characteristics of your new paraglider Whilst it...

Page 3: ... AND TAKE OFF 10 3 6 LANDING 10 3 7 PACKING 11 4 IN FLIGHT 11 4 1 FLYING IN TURBULENCE 11 4 2 POSSIBLE CONFIGURATIONS 11 4 3 ACCELERATED FLIGHT 13 4 4 FLYING WITHOUT BRAKE LINES 13 4 5 LINE KNOT S IN FLIGHT 14 5 LOSING ALTITUDE 14 5 1 BIG EARS 14 5 2 B LINE STALL 15 5 3 SPIRAL DIVE 15 6 SPECIAL METHODS 16 6 1 TOWING 16 6 2 ACROBATIC FLIGHT 16 7 CARE AND MAINTENANCE 16 7 1 MAINTENANCE 16 7 2 STORAG...

Page 4: ...then tested in all types of flight conditions This intense development work supported by the combined experience of the whole team has resulted in a wing with unbeatable flight behaviour This intense development work was underpinned by the combined experience of the whole team and has resulted in a wing with incredible flight behaviour Thanks to the leading edge reinforcements and the SLE Structur...

Page 5: ...ill give you many hours of peaceful flying 1 4 CONSTRUCTION MATERIALS The LINK 2 has all the technological innovations used on other Niviuk gliders and is built with the most careful selection of current materials It has all the current technology and accessories available to improve pilot comfort whilst increasing safety and performance In the design of all Niviuk products the team aims to ensure...

Page 6: ...piece thus avoiding errors during this delicate process The jigsaw puzzle assembly is made easier using this method and optimises the operation while making the quality control more efficient All Niviuk gliders go through an extremely thorough and detailed final inspection The canopy is cut and assembled under strict quality control conditions facilitated by the automation of this process Every wi...

Page 7: ... errors Correctly connect the risers to the attachment points so that the risers and lines are correctly ordered and free of twists Check that the IKS and carabiners are properly fastened and securely locked 2 4 HARNESS TYPE Check the engine manufacturer s specification on attachment points Before any flight commences it is strongly recommended that the pilot checks the connection of the wing to t...

Page 8: ...y However any connection system that is safe may be used Image 1 Connecting the speed bar using a Brummel hook 2 5 2 Changing the riser cords In spite of the speed system having pulleys with bearings to reduce friction to a minimum the frequency with which the speed bar is used causes the cord to wear and you may need to replace them In all Niviuk gliders the speed system cords on the risers are c...

Page 9: ...ery 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 2 offers the comfort of ending the flight with the perfect landing large areas and long runs are no longer required Please note that in wind nil conditions the forward ground speed...

Page 10: ...ed in section 2 UNPACKING AND ASSEMBLY to prepare your equipment 3 3 FLIGHT PLAN Planning a flight before taking off to avoid possible problems later is always a good idea 3 4 PRE FLIGHT CHECK Once ready but before taking off conduct another equipment inspection Conduct a thorough visual check of your gear with the wing fully open the lines untangled and properly laid out on the ground to ensure t...

Page 11: ...to assist you with rapid packing which helps maintain the integrity of the leading edge and its internal structures in 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 system ensures that both the fabric and the reinforcements of the internal structure ar...

Page 12: ...ng 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 LINK 2 s normal flight behaviour Certain ci...

Page 13: ...in or other paragliders it may not be possible to continue on the intended flight path Over controlling Most flying problems are caused by wrong pilot input which then escalates into a cascade of unwanted and unpredicted incidents We should note that the wrong inputs can lead to loss of control of the glider The LINK 2 was designed to recover by itself in most cases Do not try to over correct it G...

Page 14: ...ferent descent techniques could become vital in certain situations The most suitable descent method will depend on the particular situation To become familiar with the manoeuvres described below we recommend practising within the environment of a licensed training outfit 5 1 BIG EARS Big ears is a moderate descent technique able to increase the sink rate to 3 or 4 m s and reduces the ground speed ...

Page 15: ...to pull the risers down until the wing is 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 m s depending on the conditions and how the manoeuvre is performed To exit the manoeuvre simultaneously release both risers The wing will then slightly surge...

Page 16: ...esigned for it We do not recommend using this glider for acrobatic flying We consider acrobatic flights to be any form of piloting different than standard flights Learning acrobatic manoeuvres should be conducted under the supervision of qualified instructors within a school environment and over water with all safety rescue elements in place Centrifugal forces as high as 4 to 5 g can be exerted on...

Page 17: ...acked In case of long term storage it is advisable if possible that the wing is not compressed and it should be stored loosely without direct contact with the ground Humidity and heating can have an adverse effect on the equipment 7 3CHECKS AND INSPECTION Inspections The LINK 2 must be periodically serviced An inspection must be scheduled every 100 flying hours or every two years whichever comes f...

Page 18: ...t any informal training from anyone who is not properly qualified as a flight instructor 9 GARANTEE The equipment and components are covered by a 2 year warranty against any manufacturing defect The warranty does not cover misuse of the equipment DISCLAIMER Paragliding is an activity that requires concentration specific knowledge and common sense Take care You should learn to paraglide under the a...

Page 19: ...mm 170 170 170 170 mm 85 85 85 85 km h TRIM 38 47 MAX 55 kg 55 100 70 120 90 145 105 170 kg 4 8 5 1 5 5 6 0 DGAC EN 926 1 10 TECHNICAL DATA 10 1 TECHNICAL DATA LINK 2 CELLS NUMBER ASPECT RATIO FLAT AREA FLAT PROJECTED CORD MAXIMUM LINES TOTAL MAIN RISERS NUMBER TRIMS ACCELERATOR SPEED RANGE TOTAL WEIGHT IN FLY MIN MAX GLIDER WEIGHT CERTIFICATION ...

Page 20: ...TICK SPORTWARE CO CHINA THREAD SERAFIL 60 AMAN GERMANY SUSPENSION LINES FABRIC CODE SUPPLIER UPPER CASCADES TNL 80 TEIJIM LIMITED JAPAN MIDDLE CASCADES TNL 80 TEIJIM LIMITED JAPAN MIDDLE CASCADES TNL 140 TEIJIM LIMITED JAPAN MAIN TNL 140 TEIJIM LIMITED JAPAN MAIN TNL 220 TEIJIM LIMITED JAPAN MAIN TNL 280 TEIJIM LIMITED JAPAN MAIN BREAK TNL 280 TEIJIM LIMITED JAPAN THREAD SERAFIL 60 AMAN GERMANY RI...

Page 21: ...24 10 3 RISERS PLAN ...

Page 22: ...25 10 4 SUSPENSION PLAN ...

Page 23: ...13 5751 5723 5804 5857 14 5491 5470 5535 15 5447 5454 5535 A B C D br 1 5737 5654 5693 5811 6633 2 5701 5619 5648 5758 6385 3 5682 5602 5631 5742 6275 4 5702 5623 5664 5784 6117 5 5680 5609 5648 5820 6028 6 5659 5591 5620 5767 5996 7 5651 5596 5627 5723 6033 8 5678 5622 5664 5742 5895 9 5634 5571 5619 5736 5791 10 5561 5506 5538 5803 5597 11 5512 5466 5494 5553 5455 12 5454 5419 5460 5519 13 5469 ...

Page 24: ...13 6345 6316 6405 6464 14 6060 6038 6108 15 6013 6020 6108 A B C D br 1 6360 6268 6313 6442 7332 2 6322 6231 6265 6384 7070 3 6303 6216 6250 6371 6962 4 6327 6241 6287 6419 6809 5 6309 6230 6272 6463 6712 6 6287 6211 6243 6405 6676 7 6280 6219 6254 6358 6716 8 6310 6249 6295 6380 6546 9 6266 6197 6250 6377 6417 10 6187 6126 6161 6452 6184 11 6133 6083 6114 6181 6006 12 6069 6032 6078 6144 13 6087 ...

Page 25: ...28 LINK 2 21 LINK 2 23 10 9 CERTIFICATION ...

Page 26: ...29 LINK 2 25 LINK 2 27 ...

Page 27: ......

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