Niviuk Hook 4 Скачать руководство пользователя страница 8

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4. IN FLIGHT

4.1 FLYING IN TURBULENCE

The HOOK 4 complies with an excellent homologation to face this type 
of situation with the best safety guarantee. This wing is stable in all types 
of weather conditions. It reacts admirably in passive flight, thus offering 
a high level of safety in turbulent conditions. Nonetheless, all paragliders 
always have to be piloted according to the prevailing weather conditions; 
the pilot is the ultimate safety factor.

We recommend that the pilot adopts a proactive attitude when flying, 
making the necessary fine adjustments to keep the wing in control. He/
she should stop braking to allow it to fly at the required wing speed after 
a correction is made. Do not maintain any correction for longer than 
necessary (braked) this would cause the wing to enter into critical flying 
situation. Whenever necessary, control a situation, react to it and then 
re-establish the required speed.

4.2 POSSIBLE CONFIGURATIONS

We recommend that training to master these manoeuvres be carried out 
under the supervision of a competent school.

Asymmetric collapse
In spite of the great stability of the profile of the HOOK 4, heavy turbulent 
conditions may cause part of the wing to collapse asymmetrically. This 
usually happens when the pilot has not foreseen this possible reaction of 
the wing. When the wing is about to experience an asymmetric collapse 
the brake lines and the harness will transmit a loss of pressure to the pilot. 
To prevent the collapse from happening, pull the brake line corresponding 
to the compromised side of the wing, this will increase the angle of 
incidence. If the collapse does happen the HOOK 4 will not react violently, 
the turn tendency is very gradual and it is easily controlled. Lean your 
body towards the side that is still flying in order to counteract the turn and 

to maintain a straight course, if necessary slightly slow down the same 
side. The collapse will normally open by itself but if that does not happen, 
pull completely on the brake line on the side which has collapsed (100%). 
Do this with a firm movement. You may have to repeat this operation to 
provoke the re-opening. Take care not to over-brake on the side that is 
still flying (turn control) and when the collapse has been solved; remember 
to let the wing recover its flying speed.

Symmetric collapse
In normal flying conditions the design of the HOOK 4 ensures that a 
symmetric collapse is quite improbable. The profile of the wing has been 
designed to widely tolerate extreme changes in the angle of incidence. A 
symmetric collapse may occur in heavy turbulent conditions, on entry or 
exit of strong thermals or lack of adapting the use of the accelerator to the 
prevailing air conditions. Symmetrical collapses usually re-inflate without 
the glider turning but you can symmetrically apply the brake lines with 
a quick deep pump to quicken the re-inflation. Release the brake lines 
immediately to recover optimum flight speed.

Negative spin
This configuration is out of the normal flight behaviour of the HOOK 4. 
Certain circumstances however, may provoke this configuration such 
as trying to turn when the wing is flying at very low speed (while heavily 
braking). It is not easy to give any recommendations about this situation 
since it varies depending on the circumstances. Remember that you 
should restore the relative air speed over the wing. 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 360º before restoring to normal flight conditions.

Parachutal stall
The possibility of this happening has been eliminated by the design of the 
HOOK 4 and it is highly unlikely to happen on this paraglider. If it does 
happen, the feeling would be that the wing would not be advancing; you 

Содержание Hook 4

Страница 1: ...USER S MANUAL HOOK 4...

Страница 2: ...efficiency It s the change from the usual to the extraordinary The HOOK 4 does not leave anything else to wish for except probably more of the same We are confident that you will enjoy flying this win...

Страница 3: ...6 LANDING 7 4 IN FLIGHT 8 4 1 FLYING IN TURBULENCE 8 4 2 POSSIBLE CONFIGURATIONS 8 4 3 USING THE ACCELERATOR 9 4 4 FLYING WITHOUT BRAKE LINES 10 4 5 KNOTS IN FLIGHT 10 5 LOSING HEIGHT 10 5 1 SPLIT A 1...

Страница 4: ...ilots under all levels of training The HOOK 4 passed the essential load test of 8G without experiencing any problems On the flight test all the five sizes of the HOOK 4 received the best certification...

Страница 5: ...s begins So we eliminate possible and understandable errors that may occur during this delicate procedure The lines are semi automatically manufactured and all the sewing is finished under the supervi...

Страница 6: ...between safety and feelings Any change made to these specifications may affect the wing s performance and reactions This would therefore effect the glider s configuration and would not conform to the...

Страница 7: ...to avoid possible flight errors 3 4 PRE FLIGHT CHECK LIST Once you are ready but before you take off carry out another equipment inspection Ensure correct installation of all equipment and that all li...

Страница 8: ...and to maintain a straight course if necessary slightly slow down the same side The collapse will normally open by itself but if that does not happen pull completely on the brake line on the side whi...

Страница 9: ...and well calculated positioning of the line cascades ratify this fact A wing tangle may happen after an asymmetric collapse the end of the wing is trapped between the lines Cravat This situation coul...

Страница 10: ...ed 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...

Страница 11: ...when flying at high altitude To start the manoeuvre first lean your bodyweight and pull the brake line to the side to which you are leaning You can regulate the intensity of the turn by applying a lit...

Страница 12: ...the cell openings of the leading edge If sand is inside the wing remove it before folding 8 2 STORAGE It is important that the wing is correctly folded when stored Store your flying equipment in a co...

Страница 13: ...13 10 GUARANTEE The entire equipment and components are covered by a 2 year guarantee for any manufacture fault The guarantee does not cover misuse or abnormal use of the materials...

Страница 14: ...ING 15 15 15 15 15 CORD MAXIMUM m 2 47 2 58 2 69 2 8 2 9 MINIMUM m 0 49 0 52 0 54 0 56 0 58 AVERAGE m 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 36 7 63...

Страница 15: ...CADES DC 060 LIROS GMHB GERMANY UPPER CASCADES 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...

Страница 16: ...11 3 RISERS PLAN 16...

Страница 17: ...11 4 SUSPENSION PLAN 17...

Страница 18: ...5718 5793 11 5286 5265 5364 12 5184 5180 5238 RISERS LENGHT m m A A B C 470 470 470 470 STANDARD 340 360 380 470 ACCELERATED LINES HEIGHT m m A B C D br 1 6298 6197 6301 6410 7125 2 6234 6135 6212 632...

Страница 19: ...6315 6379 11 5819 5812 5920 12 5706 5719 5781 RISERS LENGHT m m A A B C 470 470 470 470 STANDARD 340 360 380 470 ACCELERATED LINES HEIGHT m m A B C D br 1 6866 6763 6880 6993 7688 2 6799 6696 6784 690...

Страница 20: ...921 6997 7113 7435 4 7045 6947 7050 7161 7304 5 7009 6981 7070 7175 7158 6 6963 6920 6982 7083 7114 7 6909 6828 6864 6955 7190 8 6928 6840 6895 6978 6976 9 6720 6731 6796 6894 10 6556 6696 6824 6884 1...

Страница 21: ...6 A 7 A 8 A 9 A 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 0 24 Class B In accordance with EN standards 926 2 2013 926 1 2006 PG_0957 2015 Date of issue DMY 17 09 2015 Manufa...

Страница 22: ...44 1 A 2 A 3 A 4 A 5 A 6 A 7 A 8 A 9 A 10 B 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 0 24 Class B In accordance with EN standards 926 2 2013 926 1 2006 PG_0959 2015 Date of issue...

Страница 23: ...ider s weight kg 5 5 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 firs...

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

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