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4

1. CHARACTERISTICS

1.1  WHO IS IT DESIGNED FOR?

The Koyot 3 P is equipped with the most sophisticated technology, 
ensuring maximum safety and achieving excellent performance for  
progression without limits.

Aimed at the wide range of pilots, from beginners to experienced pilots 
who want to get maximum enjoyment out of each flight without any 
stress.

With the new KOYOT 3 P you can also discover and enjoy hike & fly or 
vol-bivouac adventures. A wing with extremely low weight and volume, 
so you can choose not only when and how to progress, but also when 
and from where to do it. 

1.2 CERTIFICATION

The KOYOT 3 P has been submitted for the European EN and LTF 
certification. All certification tests were performed at the Swiss testing 
house Air Turquoise. 

All sizes passed the load, shock and flight tests.

The load test proved that the wing  can withstand the stipulated 8G. 

The shock test proved that he wing can resist 1000 daN of force.

The flight test resulted in the following certification for all KOYOT 3 P 
sizes:

EN   A
LTF  A

We recommend that only pilots who are familiar with gliders of this 
certification or above fly this paraglider.

Only the aeronautical 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 the necessary information on how the paraglider 
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.

-Description of flight characteristics of LTF/EN A paragliders:
Paragliders with maximum passive safety and extremely forgiving flight 
characteristics. Gliders with good collapse resistance in normal flight.

-Description of the skills required by the pilot to fly an EN A wing:
Designed for all pilots, including pilots under instruction.

For further information on the flight test and the corresponding 
certification number, please see the final pages of this manual or see 
niviuk.com.

1.3 IN-FLIGHT BEHAVIOUR

Niviuk developed this wing by adopting very specific goals: to improve 
performance, excellent handling; to facilitate more control for the pilot. 

To increase performance while maintaining the highest level of 
safety. To ensure that the wing transmits the maximum feedback in 
an understandable and comfortable way so that the pilot can focus 

Содержание KOYOT 3 P

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 20: ...20 10 3 RISERS PLAN...

Страница 21: ...21 10 4 SUSPENSION PLAN...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 26: ......

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