Niviuk QUBIK 19 User Manual Download Page 15

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4.5 LINE KNOT(S) IN FLIGHT

The best way to avoid knots and tangles is to thoroughly inspect the lines 
as part of a systematic pre-flight check. If a knot is spotted during the 
take off phase, immediately abort the launch sequence and stop.

If inadvertently taking off with a knotted line, the glider drift will need to 
be compensated by weight-shifting to the opposite side  and applying a 
slight brake pull to that side. Gently pull the brake line to see if the knot 
can be undone or try to locate the problem line. Try pulling it to see if the 
knot can be undone. Beware of trying to clear a knotted line or untangle 
a line in flight when close to the terrain. If the knot is too tight and cannot 
be undone, carefully and safely fly to the nearest landing zone. Be 
careful: do not pull too hard on the brake handles because there will be 
an increased risk of stalling the wing or entering a negative spin. Before 
attempting to clear a knot, make sure there are no other pilots flying in 
the vicinity.

5. LOSING ALTITUDE

Knowledge of different 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 by 3 to 5 km/h. The angle 
of attack and effective wing-loading will also increase due to the smaller 
surface area of the wing.

Standard technique

To perform the ‘Big ears’ manoeuvre, take the outermost line on each 
A-riser and simultaneously, smoothly pull them outward and downward. 
The wingtips will fold in.

To re-establish forward speed and the correct angle of attack, accelerate 
once the ears are pulled. 

Keep the ears pulled in until you have lost the desired altitude.
Let go of the lines to re-inflate the tips automatically. If they do not, try 
progressively pulling one brake then the other. We recommend inflating 
the wing tips asymmetrically, without major change to the angle of 
attack, especially when flying near the ground or flying in turbulence. 

Beware of the risk of stalling!

The action of reaching for the outermost A-lines to make ears, can 
inadvertently mean pulling the brakes. The same can happen when we 
are holding the tips down with the outermost A-lines, it is possible to 
accidentally affect the brakes. This can obviously lead to a significant 
speed decrease. 
 
In paragliders with a very pronounced arc, pulling big ears means an 
increase in drag. On a very arched wing, the ears do not fold, they just 
hang. The increase of drag is more pronounced than on wings with a less 
pronounced arc. 

The QUBIK is designed with little chord, which is good in normal flight 
conditions. However, this same damping is what can cause us to have 
problems to regain normal flying speed after a high increase of the angle 
of attack and the added drag of the ears. These particularities, together 
with turbulent thermic conditions, could cause an unintentional stall. 
 

The solution:

  big ears may still be applied but you must be fully aware 

of the above-mentioned points and act accordingly. To avoid the stall, 
simply use half speed-bar (this is sufficient) to increase the speed  and 
decrease the angle of incidence. This should allow you to maintain 

Summary of Contents for QUBIK 19

Page 1: ...QUBIK User s manual...

Page 2: ...ing 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 t...

Page 3: ...IGHT 12 4 1 DOUBLE STEERING SYSTEM 12 4 2 FLYING IN TURBULENCE 13 4 3 POSSIBLE CONFIGURATIONS 13 4 4 ACCELERATED FLIGHT 15 4 5 FLYING WITHOUT BRAKE LINES 15 4 6 LINE KNOT S IN FLIGHT 15 5 LOSING ALTIT...

Page 4: ...nse 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 experi...

Page 5: ...give you many hours of peaceful flying 1 4 CONSTRUCTION MATERIALS The QUBIK has all the technological innovations used on other Niviuk gliders and is built with the most careful selection of current...

Page 6: ...ven a millimetre of error The cutting of each wing component is performed by a rigorous extremely meticulous automated computer laser cutting robotic arm This program also paints the guideline markers...

Page 7: ...facturer instructions and set the trimmers to the neutral position Check the engine manufacturer s specification on attachment points The QUBIK risers are colour coded Right green Left red This colour...

Page 8: ...talled The standard connection of the speed bar to the speed system is via Brummel hooks where two slots in the hooks are interlocked making their connection disconnection easy However any connection...

Page 9: ...ry flight by adjusting the trimmers to their most efficient setting With the trimmers closed and using just the full range of brake travel the QUBIK is a precise light to handle and a fun machine to f...

Page 10: ...of moving the brake pulleys to a variety of positions to ensure pilot comfort The pulley is fastened to the riser loop that can be adjusted easily The riser has 2 possible fixing points distributed a...

Page 11: ...a variety of different materials and it must be packed carefully A correct folding method is very important to extend the useful life of your paraglider It should be concertina packed with the leadin...

Page 12: ...e to deal with incidents it is very stable in all conditions and has a high degree of passive safety even in turbulent conditions All paragliders must be piloted for the prevailing conditions and the...

Page 13: ...Negative spin A negative spin does not conform to the QUBIK s normal flight behaviour Certain circumstances however may provoke a negative spin such as trying to turn when flying at very low air spee...

Page 14: ...can lead to loss of control of the glider The QUBIK was designed to recover by itself in most cases Do not try to over correct it Generally speaking the reactions of the wing which are caused by too...

Page 15: ...rform the Big ears manoeuvre take the outermost line on each A riser and simultaneously smoothly pull them outward and downward The wingtips will fold in To re establish forward speed and the correct...

Page 16: ...During this manoeuvre the first sensation is a decrease in relative wind and a slight backwards inclination of the wing as if going backwards To exit the manoeuvre release the lines as you would with...

Page 17: ...r will briefly experience an asymmetrical acceleration and dive depending on how the manoeuvre was carried out Practise these manoeuvres at sufficient altitude and with moderation 6 SPECIAL METHODS 6...

Page 18: ...the wing to be correctly folded when stored Keep it in the in a cool dry place away from solvents fuels oils Do not leave your gear inside a car boot as cars left in the sun can become very hot A ruc...

Page 19: ...included in the repair kit as long as no stitching is required to mend the fabric Any other tears or repairs should be done in a specialist repair shop by qualified personnel Damaged lines must be rep...

Page 20: ...all the correct licences Be modest when you evaluate your skill level in terms of meteorology Niviuk s liability for damages covers only its own products Niviuk can take no responsibility for your act...

Page 21: ...21...

Page 22: ...3 2 A A B C D mm 140 140 140 140 140 mm 80 80 80 80 80 km h TRIM 40 56 MAX 65 kg 60 100 70 120 80 140 100 160 110 180 kg 4 7 5 1 5 4 5 9 6 3 DGAC 10 TECHNICAL DATA 10 1 TECHNICAL DATA CELLS NUMBER ASP...

Page 23: ...CODE SUPPLIER UPPER CASCADES TNL 80 TEIJIM LIMITED JAPAN UPPER CASCADES TNL 140 TEIJIM LIMITED JAPAN MIDDLE CASCADES TNL 80 TEIJIM LIMITED JAPAN MIDDLE CASCADES TNL 140 TEIJIM LIMITED JAPAN MIDDLE CA...

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

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

Page 26: ...625 770 A B C D br 1 5660 5576 5612 5714 6760 2 5617 5534 5561 5656 6367 3 5580 5500 5526 5624 6188 4 5603 5523 5559 5666 6030 5 5563 5490 5519 5677 5929 6 5532 5461 5482 5618 5882 7 5518 5460 5483 55...

Page 27: ...625 770 A B C D br 1 6265 6173 6212 6326 7354 2 6219 6128 6156 6262 6936 3 6182 6094 6122 6231 6757 4 6208 6122 6160 6278 6603 5 6169 6090 6121 6295 6492 6 6136 6059 6081 6231 6441 7 6124 6061 6085 61...

Page 28: ...7 6747 6677 6704 6792 7149 8 6782 6715 6752 6824 6953 9 6728 6671 6753 6828 6804 10 6650 6600 6641 6906 6539 11 6598 6556 6573 6620 6345 12 6534 6505 6507 6550 6370 13 6548 6529 6542 6580 14 6293 625...

Page 29: ...29 QUBIK 19 QUBIK 21...

Page 30: ...30 QUBIK 23 QUBIK 25...

Page 31: ...31 QUBIK 27...

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