background image

10

If you have taken off with a knot you will have to correct the drift by 
leaning on the opposite side of the knot and apply the brake line on 
that side too. You can gently pull on the brake line to see if the knot 
becomes unfastened or try to identify the line with the knot in it. The 
identified line can then be pulled to see if the knot undoes. Be very 
careful when trying to remove a knot. When there are knots in the 
lines or when they are tangled, do not pull too hard on the brake lines 
because there is a greater risk of the wing to stalling or negative turn 
being initiated

Before trying to remove a knot, make sure there are no pilots flying 
nearby and never try these manoeuvres near the mountainside. If the 
knot is too tight and you cannot remove it, carefully and safely fly to the 
nearest landing place. 

5. LOSING HEIGHT

The knowledge of the different descent techniques is an important 
resource to use in certain situations. The most adequate descent method 
will depend on the particular situation.

We recommend that you learn to use these manoeuvres under the tuition 
of a competent school.

5.1 EARS
 
Big ears are a moderate descent method, reaching –3 or –4 m/s, speed  
reduces slightly between 3 and 5 km/h and piloting becomes limited. 
The angle of incidence and the surface wing load also increases. Push 
on the accelerator to restore the wing’s horizontal speed and the angle 
of incidence.
 
To activate big ears take  the outer most line on each a risers (2a3 in 
the line  plan) and simultaneously, smoothly pull them outward and 

downward. The wingtips will fold in. Let go of the lines and the big ears 
re-inflate automatically. If they do not re-inflate, gently pull on one of the 
brake lines and then on the opposite one. We recommend that you re-
inflate asymmetrically, not to alter the angle of incidence, 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 you are not in control of the paraglider. The air 
circulation over the profile is interrupted and the wing enters into a 
situation similar to parachuting.

To carry out this manoeuvre you have to take the B-lines at the maillons 
height leaving them as base in the hand palm avoiding taking the A&B 
together. Pull symmetrically down (approx. 20-30cms) and then hold 
this position. The initial phase is quite physical (hard resistance) which 
means that you will have to pull strongly until the profile of the wing is 
deformed, when this happens the required force will then significantly 
reduce. To maintain this manoeuvre you must continue to hold the B 
Lines in the pulled down position. The wing will then become deformed, 
horizontal speed drops to 0 km/h and vertical speed increases to –6 to 
–8 m/s depending on the conditions and how the manoeuvre has been 
carried out.

To exit the manoeuvre, simultaneously release both risers, the wing will 
then slightly surge forward and then automatically return to normal flight. 
It is better to let go of the lines quickly rather than slowly. This is an easy 
manoeuvre but you must remember that the wing stops flying, it loses 
all horizontal movement and its reactions are very different compared to 
normal flight.

Summary of Contents for HOOK 3

Page 1: ...USER S MANUAL HOOK 3...

Page 2: ...t in flight and efficiency It s the change from the usual to the extraordinary The HOOK 3 does not leave anything else to wish for We are confident that you will enjoy flying this wing and that you wi...

Page 3: ...LANDING 7 4 IN FLIGHT 7 4 1 FLYING IN TURBULENCE 7 4 2 POSSIBLE CONFIGURATIONS 7 4 3 USING THE ACCELERATOR 9 4 4 FLYING WITHOUT BRAKE LINES 9 4 5 KNOTS IN FLIGHT 9 5 LOSING HEIGHT 10 5 1 EARS 10 5 2 B...

Page 4: ...ts numerous adjustments were made These prototypes were then tested in all types of flight conditions HOOK 3 is the result Hook 3 is technology privileged compared to its predecessors the wing feature...

Page 5: ...l find the accelerator bar that completes the acceleration gear of the wing a small fabric repair kit made of auto adhesive rips top a user s manual with the answers all our questions about our new HO...

Page 6: ...nd 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 on them just lift to accompany the natural rising movement of...

Page 7: ...e shape of the canopy in flight All this will assist in a trouble free take off 3 6 LANDING The HOOK 3 lands excellently it transforms the wing speed into lift on the pilot s demand allowing an enormo...

Page 8: ...ing To achieve this progressively reduce the pressure on the brake lines and let the wing gain speed The normal reaction would be a lateral surge with a turn tendency no greater than 360 before restor...

Page 9: ...at follow over handling are neither due to the input made or the intensity but the length of time the pilot continues to over handle You have to allow the profile to re establish normal flight speed a...

Page 10: ...ull them outward and downward The wingtips will fold in Let go of the lines and the big ears re inflate automatically If they do not re inflate gently pull on one of the brake lines and then on the op...

Page 11: ...effect of the exit manoeuvre is that the glider will rock briefly with lateral surge depending on how the manoeuvre has been carried out Practice these movements at sufficient altitude and with moder...

Page 12: ...you have landed do not leave the wing in the sun store it properly If you use your wing in a sandy area try to avoid the sand from entering through the cell openings of the leading edge If sand is ins...

Page 13: ...dealers are not responsible for any act or accident that may be the result of practicing this sport You must not use this equipment if you are not trained Do not take advice or accept any informal tra...

Page 14: ...4 4 4 FLATTENING 15 15 15 15 15 CORD MAXIMUM 2 47 2 58 2 69 2 8 2 9 MINIMUM 0 49 0 52 0 54 0 56 0 58 AVERAGE 1 97 2 06 2 14 2 23 2 31 LINES TOTAL METERS M 208 218 227 236 245 HEIGHT M 6 5 6 8 7 09 7 3...

Page 15: ...ASCADES TNL 080 TEIJIM LIMITED JAPAN UPPER CASCADES DC 100 LIROS GMHB GERMANY MIDDLE CASCADES TNL 080 TEIJIM LIMITED JAPAN MIDDLE CASCADES TNL 140 TEIJIM LIMITED JAPAN MIDDLE CASCADES TNL 220 TEIJIM L...

Page 16: ...16 11 3 RISERS ARRANGEMENT...

Page 17: ...17 11 4 LINE PLAN...

Page 18: ...61 5550 5654 12 5453 5460 5520 RISERS LENGHT M M A B C D 470 470 470 STANDARD 320 370 470 ACCELERATED 11 5 LENGHTS HOOK 3 21 NIVIUK HOOK 3 21 LINES HEIGHT M M A B C D BR 1 6014 5909 6003 6103 6716 2 5...

Page 19: ...812 5920 12 5712 5719 5781 RISERS LENGHT M M A B C D 470 470 470 470 STANDARD 360 380 420 470 ACELERATED 11 8 LENGHTS HOOK 3 27 NIVIUK HOOK 3 27 LINES HEIGHT M M A B C D BR 1 6881 6762 6870 6983 7667...

Page 20: ...7601 3 7040 6921 6991 7108 7415 4 7065 6947 7045 7156 7285 5 7023 6975 7075 7176 7139 6 6978 6914 6988 7084 7095 7 6923 6822 6869 6955 7172 8 6942 6834 6900 6978 6967 9 6740 6725 6801 6885 10 6576 66...

Page 21: ...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_0668 2013 Date of issue DMY 06 02 2013 Manufacturer Niviuk G...

Page 22: ...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 A 21 A 22 A 23 A 24 0 Class B In accordance with EN standards 926 2 2005 926 1 2006 PG_0630 2012 Date of issue DMY 09 01 2...

Page 23: ...5 8 Range of trimmers cm 0 Number of risers 3 Total speed range with accessories km h 24 Projected area m2 24 65 Harness used for testing max weight Inspections whichever happens first Harness type AB...

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

Reviews: