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Pull on this line until it is taught, as it should help undo the cravat. If 
ineffective, fly down to the nearest possible landing spot, controlling the 
direction with both weight shift and the use of the brake opposite to the 
tangled side. Be cautious when attempting to undo a tangle while flying 
near terrain or other paragliders; it may not be possible to continue on 
the intended flight path.

Over-controlling

Most flying problems are caused by wrong pilot input, which then 
escalates into a cascade of unwanted and unpredicted incidents. We 
should note that the wrong inputs can lead to loss of control of the glider. 
The KOYOT 3 P 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 
much input, are due to the length of time the pilot continues to over–
control the wing. You have to allow the glider to re-establish normal flying 
speed and attitude after any type of incident. 

4.3 ACELLERATED FLIGHT

The KOYOT 3 P profile was designed for stable flight throughout its entire 
speed range.  The speed-bar can be used in strong winds or significant 
sink.

When accelerating the wing, the profile becomes more sensitive to 
turbulence and closer to a possible frontal collapse. If a loss in internal 
wing pressure is felt, tension on the speed-bar should be reduced to a 
minimum and a slight pull on the brake lines is recommended to increase 
the wing’s incidence angle. Remember to re-establish the air speed after 
correcting the angle of attack.
It is NOT recommended to accelerate near obstacles or in very turbulent 
conditions. If necessary, constantly adjust the movements and pressure 
on the speed-bar whilst doing the same to the brake lines. This balance 
is considered to be ‘active piloting’.

4.4  FLYING WITHOUT BRAKE LINES

If, for any reason at all, the KOYOT 3 P’s brake lines become disabled 
in flight, it will become necessary to pilot the wing with the C-risers and 
weight shifting until landing. The C-lines steer easily because they are not 
under much tension, however you will need to be careful and not handle 
them too heavily in case this causes a stall or negative spin. The wing 
must be flown at full speed during the landing approach, and the C-risers 
will have to be pulled symmetrically all the way down shortly before 
contact with the ground. This braking method is not as effective as using 
the brake lines, and hence the wing will land with a higher ground speed.

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 of the wing 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.

Summary of Contents for KOYOT 3 P

Page 1: ...User s manual KOYOT 3 P...

Page 2: ...f our motto The importance of small details This is the user manual and we recommend you read it carefully The NIiviuk Team USER MANUAL This manual provides you with the necessary information on the m...

Page 3: ...0 3 6 LANDING 10 3 7 PACKING 10 4 IN FLIGHT 11 4 1 FLYING IN TURBULENCE 11 4 2 POSSIBLE CONFIGURATIONS 11 4 3 ACCELERATED FLIGHT 13 4 4 FLYING WITHOUT BRAKE LINES 13 4 5 LINE KNOT S IN FLIGHT 13 5 LOS...

Page 4: ...utical authorities of respective countries can determine pilot competence We recommend pilots read the flight test report carefully especially the comments of the test pilot The report contains all th...

Page 5: ...sed by the arrangement of the air inlets to ensure optimal maintenance of internal pressure Thanks to this design we were able to reduce their size while maintaining the same air flow at all angles to...

Page 6: ...been calculated depending on the workload and aims to achieve the required best performance with the least drag The lines are semi automatically cut to length and all the sewing is completed under th...

Page 7: ...certification report Care should be taken with the chest strap setting as the distance of the chest strap setting will affect the handling of the glider If the chest strap is too wide it allows great...

Page 8: ...nsiderations You should use the type of speed bar you consider appropriate depending on the type of harness personal preferences etc The speed bar is detachable to facilitate its connection and or dis...

Page 9: ...e main brake lines are adjusted at the factory and conform to the length stipulated during certification However the length can be changed to adapt to the pilot s flying style In any case we recommend...

Page 10: ...n appropriate location facing the wind Position the KOYOT 3 P in a crescent configuration to facilitate inflation A clean wing layout will ensure a trouble free take off 3 6 LANDING The KOYOT 3 P land...

Page 11: ...wing loading and avoiding over steering It is important to note that the type of reaction to a manoeuvre can vary from one size of wing to another and even within the same size the behaviour and react...

Page 12: ...HE BRAKE LINES Deep Stall The possibility of the KOYOT 3 P stalling during normal flight is very unlikely It could only happen if you are flying at a very low air speed whilst over steering or perform...

Page 13: ...brake lines This balance is considered to be active piloting 4 4 FLYING WITHOUT BRAKE LINES If for any reason at all the KOYOT 3 P s brake lines become disabled in flight it will become necessary to p...

Page 14: ...ling 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 KOYOT 3 P is desi...

Page 15: ...ds Good enough reasons to familiarise yourself with the manoeuvre and understand how to exit it To exit this manoeuvre the inner brake handle down side of the turn must progressively be relaxed while...

Page 16: ...e reviewed If any Nitinol rod is damaged they are easily replaceable The fabric and the lines do not need to be washed If they become dirty clean them with a soft damp cloth using only water Do not us...

Page 17: ...Please refer to the line plan at the end of this manual Any repair should be done in a specialist repair shop by qualified personnel Niviuk can not be held responsible for any damage caused by incorr...

Page 18: ...76 287 299 M 6 59 6 88 7 16 7 43 206 206 206 206 2 1 3 4 2 1 3 4 2 1 3 4 2 1 3 4 3 A A B C A A B C A A B C A A B C NO NO NO NO M M 110 110 110 110 YES YES YES YES KG 45 60 75 90 KG 73 80 95 115 KG 3 1...

Page 19: ...LON IND KOREA REIFORCEMENT LOOPS D P GERMANY TRAILING EDGE REIFORCEMENT D P GERMANY RIBS REIFORCEMNET SPORTWARE CO CHINA THREAD AMAN GERMANY SUSPENSION LINES FABRIC CODE SUPPLIER UPPER CASCADES EDELRI...

Page 20: ...20 10 3 RISERS PLAN...

Page 21: ...21 10 4 SUSPENSION PLAN...

Page 22: ...451 STB 5 329 5 340 5 405 A A B C 470 470 470 470 360 360 390 470 LINES HEIGHT RISER m m RISERS LENGHT m m STANDARD TRIMMER OPENED A B C D br 1 6 328 6 258 6 370 6 503 6 961 2 6 284 6 211 6 305 6 443...

Page 23: ...062 stb 5 928 5 940 6 011 A A B C 470 470 470 470 360 360 390 470 RISERS LENGHT m m STANDARD TRIMMER OPENED A B C D br 1 6 873 6 797 6 921 7 065 7 550 2 6 828 6 748 6 853 7 002 7 287 3 6 808 6 726 6 8...

Page 24: ...71 9 10 Page 1 of 1 In accordance with standards EN 926 2 2013 EN 926 1 2015 LTF 91 09 10 8 CERTIFICATION SPECIMEN TEST KOYOT 3 P 22 Class A PG_1244 2017 Date of issue DMY 21 12 2017 Manufacturer Niv...

Page 25: ...ture GB REV 01 07 06 2016 ISO 71 9 10 Page 1 of 1 In accordance with standards EN 926 2 2013 EN 926 1 2015 LTF 91 09 Class A PG_1247 2017 Date of issue DMY 21 12 2017 Manufacturer Niviuk Gliders Air G...

Page 26: ......

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