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1. CHARACTERISTICS

1.1 WHO IS IT DESIGNED FOR?

The LINK is a glider designed for all kind of powered flight and is designed 
for all kind of pilots.
For the student or established pilots the LINK is the PPG glider of choice 
for those who want to enjoy the relaxed powered flight with a safety and 
performance in mind.
Powered flight is a relatively new activity which continuously evolves. It’s 
essential that to get the top performance of the wing the motor, propeller 
and harness are matched suitably.

1.2 CERTIFICATION

The LINK has successfully achieved the European EN certification in the 
B category. 
These outstanding levels of certification confirm top safety, precise 
handling and ease of use.
On the essential load test as well on the in-flight behaviour test the 
results were extremely good.
Check the homologation results and figures on the last pages of this 
manual.

1.3 IN-FLIGHT BEHAVIOUR

The NIVIUK Team has carried out extensive and meticulous design work. 
As a consequence of several prototypes and many hours of test flights 
numerous adjustments were made. These prototypes were then tested in 
all types of flight conditions. This intense development work supported 
by the combined experience of the whole team has achieved a wing with 
unbeatable behaviour. 
Light handling, precise response, manoeuvrability, safety and a high 
stability achieved thanks to the leading edge reinforcements, the SLE 
(Structured Leading Edge). These are some of the qualities of this wing 

which is perfectly adapted to the powered flight needs. 
Its inflation behaviour is the first step to appreciate its obedient 
disposition. Its lightness of weight and controls determine all the actions 
during the flight with total 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 progressive inflation rate the pilot 
remains in complete control of the wing throughout all stages of take 
off. This allows extra time to position the wing in the perfect pre-launch 
position directly above the head. 
 The running phase is perhaps one of the most critical when taking off 
with a powered wing, so any technological assistance is an advantage 
to take off easily and safely. On takeoff in order to create sufficient lift 
traditional profiles demand high forward speed, in other words, a long 
and fast run. The new technological features on the LINK facilitate early 
lift and take-off therefore reducing the amount of time and physical effort 
required when running. 

Once airborne, the LINK remains precise and balanced to every pilot 
input thanks to the addition of finely evolved SLE (Structured Leading 
Edge), the same innovative structure technology as used on our highly 
successful competition wings is now applied to this PPG glider for all the 
pilots to experience and enjoy.
It will very quickly become apparent to the pilot that the handling and 
manoeuvrability of the LINK remains light and efficient during all aspects 
of flight and even in the most adverse conditions every pilot input is met 
with an immediate and precise response.
At each release of the trimmers the wings profile changes and 
accelerates, penetrating without any problems. The brake is usable in all 
the trimmer positions, even accelerated.
The performance on this new wing is above the average on this kind of 
wings. The power required of the engine is on the low to medium range. 
Its consumption is much less than most wings due to the effectiveness of 
a glider perfectly designed to ensure the top stability and performance in 

Содержание LINK 23

Страница 1: ...USER S MANUAL LINK...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 17: ...17 11 3 RISER ARRANGEMENT...

Страница 18: ...18 11 4 LINE PLAN...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 23: ...23...

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

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