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4. IN FLIGHT

We recommend that you read the certification test report. 
The report contains all the necessary information on how the KOYOT 3 P 
reacts during each of the tested manoeuvres. 

It is important to point out that the appropriate response to each adverse 
manoeuvre can vary from size to size; even within the same size at 
maximum or minimum load the behaviour and reactions of the wing may 
vary. 

Having the knowledge that the testing house provides through the test 
report is fundamental to learning how to deal with possible situations.

To become familiar with the manoeuvres described below, we 
recommend practising within the auspices of a licensed training outfit.

4.1 FLYING IN TURBULENCE

The KOYOT 3 P has an excellent profile 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 pilot 
is the ultimate safety factor.

We recommend active flying in turbulent conditions, always taking 
measures to maintain control of the wing, preventing it from collapsing 
and restoring the speed required by the wing after each correction.

Do not correct the glider (braking) for too long in case this provokes a 
stall. Whenever necessary, control a situation, react to it and then re-
establish the required speed.

4.2  POSSIBLE CONFIGURATIONS

To become familiar with the manoeuvres described below, we 
recommend practising within the environment of a competent training 
outfit. The pilot must adapt their use of the brakes depending on the 
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 reactions may be different depending on the wing-loading.

In the test report, you will find all the necessary information on how to 
handle your new wing during each of the tested manoeuvres. Having this 
information is crucial to know how to react during these manoeuvres in 
real flight, so you can deal with these situations as safely as possible.

Asymmetric collapse

In spite of the KOYOT 3 P’s profile stability, strong turbulent air may 
cause the wing to collapse asymmetrically in very strong turbulence, 
especially if the pilot is unable to fly actively and prevent the collapse. In 
this case the glider conveys a loss of pressure through the brake lines 
and the harness. To prevent the collapse from happening, pull the brake 
handle corresponding to the affected side of the wing. It will increase the 
incidence of the wing (angle of attack). If the collapse does happen, the 
KOYOT 3 P will not react violently, the turning tendency is gradual and 
easily controlled. Weight-shift toward the open, flying side (the opposite 
side of the collapse) to keep the wing flying straight, while applying light 
brake pressure to that side if necessary. Normally, the collapsed side of 
the wing should then recover and reopen by itself. If it does not, then pull 
the brake handle on the collapsed side decisively and quickly all the way 
(100%) down. You may have to repeat this pumping action to provoke 
the re-opening of the deflated glider side. Do not over-brake or slow 
down the flying side of the wing (control the turn). Once the collapsed 
side is open make sure you return to the default flying speed.

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...

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