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3.5 WING INFLATION, CONTROL, AND TAKE-OFF

Smoothly and progressively infl ate the wing (chapter 2.6 INSPECTION AND 
WING INFLATION ON THE GROUND). The PEAK infl ates easily and does 
not require excessive energy. It does not tend to over-take you, so the wing 
infl ation phase is carried out without anguish. These take off characteristics 
provide a perfect control phase and enough time for the pilot to decide 
whether to accelerate and take off. 
Whenever the wind speed allows it, we recommend a reverse launch 
technique, this type of launch allows you to carry out a better visual check 
of the wing. The PEAK is especially easy to control in this position in strong 
winds. However, wind speeds up to 25 to 30 km/h are considered strong and 
extra consideration should be given to any thought of fl ight.
Preparation and positioning of the wing on the take off is especially important. 
Choose a location, which is appropriate for the direction of the wind. Position 
the paraglider as if it were part of a large circle, taking into account the shape 
of the canopy in fl ight. All this will assist in a trouble free take-off.

3.6 LANDING

The PEAK lands excellently, it transforms the wing speed into lift on the pilot’s 
demand, allowing an enormous margin of error. You will not have to wrap the 
brake lines around your hand to get greater braking effi ciency.

4. IN FLIGHT

4.1 FLYING IN TURBULENCE

The PEAK has an excellent profi le to withstand the very different aero-
logical conditions so allowing the best possible piloting and stability. It reacts 
admirably in passive fl ight, thus offering a high level of safety in turbulent 
conditions. Nonetheless, the pilot always has to pilot according to the 
prevailing weather conditions, the pilot is the ultimate safety factor.
We recommend active piloting, making the necessary fi ne adjustments to 
keep the wing in control. He/she should stop braking to allow it to fl y 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 fl ying 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 profi le of the PEAK, 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 PEAK will not react violently, the turn tendency is 
very gradual and it is easily controlled. Lean your body towards the side that 
is still fl ying 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 fi rm 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 fl ying (turn control) and when the collapse has 
been solved, remember to let the wing recover its fl ying speed.

Symmetric collapse

In normal fl ying conditions the design of the PEAK ensures that a symmetric 
collapse is quite improbable. The profi le 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-infl ate without the glider turning 

Summary of Contents for PEAK 23

Page 1: ...PEAK USER S MANUAL...

Page 2: ...nce and stability not yet seen in this category With an aspect ratio of 6 6 we feel that the overall qualities of our competition glider have successfully been transferred to the Serial class We are s...

Page 3: ...NTROL AND TAKE OFF 7 3 6 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 HE...

Page 4: ...nding actively to your demands It will make the PEAK your best ally to be on top of the thermal and to enjoy the performance and speed Glide ratio and speed in these domains the PEAK is outstanding Th...

Page 5: ...r that completes the acceleration gear of the wing a small fabric repair kit made of auto adhesive ripstop a pair of special handles for more precise piloting and a user s manual with the answers all...

Page 6: ...rising movement of the wing Once the wing is in the 12 o clock position simply apply correct pressure on the brake lines and the PEAK will sit over your head 2 7 ADJUSTING THE BRAKES The length of the...

Page 7: ...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 sit...

Page 8: ...It is very important that the pressure on the brake lines is maintained until the wing is well established vertical above To regain normal flight conditions progressively and symmetrically release the...

Page 9: ...ot before take off immediately stop running and do not take off 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 lin...

Page 10: ...arachuting To carry out this manoeuvre you have to take the B risers below the maillons and symmetrically pull both of them down approx 20 30cms and then hold this position The initial phase is quite...

Page 11: ...t should be folded like an accordion with the leading edge reinforcements flat and the rigifoils positioned one upon the other This method will ensure that the profile remains in good shape without al...

Page 12: ...the repair kit so long as no stitches are involved in the tear Any other type of tear must be repaired in a specialized repair shop or by qualified personnel Do not accept a home repair 9 SAFETY AND...

Page 13: ...ON CANOPY FABRIC CODE SUPPLIER UPPER SURFACE SKYTEX 40 9017 E77A NCV FRANCE BOTTOM SURFACE SKYTEX 40 9017 E77A NCV FRANCE PROFILES SKYTEX 40 9017 E29A NCV FRANCE DIAGONALS SKYTEX 40 9017 E29A NCV FRAN...

Page 14: ...14 11 3 RISER ARRANGEMENT PEAK...

Page 15: ...15 11 4 LINE PLAN PEAK...

Page 16: ...599 5 598 603 5 667 13 591 5 593 598 671 RISERS LENGTHS CM A B C 47 47 47 STANDARD 27 31 ACCELERATED 11 6 DIMENSIONS PEAK 25 NIVIUK PEAK 25 LINES HEIGHT CM A B C BR 1 703 5 697 706 791 2 695 5 689 69...

Page 17: ...3 5 641 5 647 5 721 13 634 5 636 5 641 5 725 5 RISERS LENGTHS CM A B C 47 47 47 STANDARD 27 31 ACCELERATED 11 8 DIMENSIONS PEAK 29 NIVIUK PEAK 29 LINES HEIGHT CM A B C BR 1 761 753 763 856 5 2 752 5 7...

Page 18: ...11 12 13 14 15 16 17 18 19 20 21 22 23 24 x x x x x x x x x x x x x x x x x x x www niviuk com info niviuk com x x x x 26 11 Class D Accordance with EN standards 926 2 2005 926 1 2006 Date of issue D...

Page 19: ...5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 x x x x x x x x x x x x x x x x x x x x x x x www niviuk com info niviuk com 28 12 Class D Accordance with EN standards 926 2 2005 926 1 2006 Dat...

Page 20: ...niviuk com The importance of small details Bisgr c...

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