background image

15

vertical descending speed increases to –6 to –8 m/s, depending on the 
conditions and how the manoeuvre is performed.

To exit the manoeuvre, simultaneously release both risers. The wing will 
then slightly surge forward and automatically return to normal flight. It is 
better to let go of the lines quickly rather than slowly.

This is an easy descent technique to perform, but remember that 
the wing will stop flying, will lose all forward horizontal speed, and 
its reactions will change markedly when compared to a normal flight 
configuration.

5.3 SPIRAL DIVE

This is a more effective way to rapidly lose altitude. Beware that the wing 
will experience and be subjected to a tremendous amount of descending 
and rotating speed (g-force), which can cause a loss of orientation and 
consciousness (blackout). This manoeuvre must therefore be done 
gradually to increase one’s capacity to resist the g-force exerted on 
the body. With practise, you will fully appreciate and understand it. 
Only practise this manoeuvre at high altitude and with enough ground 
clearance.

To start the manoeuvre, first weight shift and pull the brake handle 
located on the inner side of the turn. The intensity of the turn can be 
controlled by braking slightly using the outer brake handle.

A paraglider flying at its maximum rotating speed can reach –20 m/s, or 
the equivalent of a 70 km/h vertical descent, and will stabilise in a spiral 
dive from 15m/s onwards. 

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 momentarily applying tension to the 
outer brake handle opposite to the turn. The pilot must also weight shift 
and lean towards the opposite side of the turn at the same time.

The exit should be performed gradually and smoothly so that the 
changes in pressure and speed can be noted.

When exiting the spiral, the glider will briefly experience an asymmetrical 
acceleration and dive, depending on how the manoeuvre was carried out.

Practise these manoeuvres at sufficient altitude and with moderation.

5.4 SLOW DESCENT TECHNIQUE

This technique allows descent without straining the wing or taxing the 
pilot. Glide normally while searching for descending air and begin to turn 
as if climbing in a thermal, but with the intention to sink.

Common sense has to be used to avoid dangerous areas of rotor when 
looking for descending air. Safety is the most important consideration.

6. SPECIAL METHODS

6.1 TOWING

The KOYOT 3 P does not experience any problems whilst being towed. 
Only qualified winch personnel should handle the certified equipment to 
carry out this operation. The wing must be inflated similarly as during a 
normal takeoff.

It is important to use the brakes to correct the flight path alignment, 
especially if the glider begins to turn. Since the wing is subject to a slow 
airspeed and with a high positive angle of attack, we must make any 
corrections with a high degree of feel and delicacy, in order to avoid a 
stall.

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: ......

Reviews: