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does not, try to weight-shift towards the collapsed side. If this does not 
resolve the issue, pull the brake handle on the collapsed side decisively 
and quickly all the way (100%) down and release it back up immediately. 
You may have to repeat this action to provoke the re-opening of the 
collapsed 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 normal flying speed.

Frontal collapse
Due to the KOYOT 4 ’s design, in normal flying conditions frontal 
collapses are unlikely to take place. The wing’s profile has great buffering 
abilities when dealing with extreme incidence changes. A frontal collapse 
may occur in strong turbulent conditions, entering or exiting powerful 
thermals. Frontal collapses usually re-inflate without the glider turning, but 
a symmetrically applied quick braking action with a quick deep pump of 
both brakes will accelerate the re-inflation if necessary. Release the brake 
lines immediately to return to default glider air speed.

Negative spin
A negative spin does not conform to the KOYOT 4 ’s normal flight 
behaviour. Certain circumstances however, may provoke a negative spin 
(such as trying to turn when flying at very low air speed whilst applying 
a lot of brake). It is not easy to give any specific recommendation about 
this situation other than quickly restoring the wing’s default air speed 
and angle of attack by progressively reducing the tension on the brake 
lines. The normal wing reaction will be to have a lateral surge on the re-
accelerated side with a rotation not greater than 360º before returning to 
default air speed and a straight flight path trajectory.

Parachutal stall
The possibility of entering or remaining in a parachutal stall have been 
eliminated from the KOYOT 4 .
A parachutal stall is virtually impossible with this wing.  If it did enter into 
a parachutal stall, the wing loses forward motion, becomes unstable 
and there is a lack of pressure on the brake lines, although the canopy 

appears to be fully inflated. To regain normal air speed, release brake line 
tension symmetrically and manually push on the A-lines or weight-shift 
your body to any side WITHOUT PULLING ON THE BRAKE LINES.

Deep Stall
The possibility of the KOYOT 4 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 performing dangerous manoeuvres in turbulent air.

To provoke a deep stall, the wing has to be slowed down to its minimum 
air speed by symmetrically pulling the brake lines all the way (100%) down 
until the stall point is reached and held there. The glider will first pitch 
rearward and then reposition itself overhead, rocking slightly, depending 
on how the manoeuvre is done. 

When entering a stall, remain clear-headed and ease off the brake lines 
until reaching the half-way point of the total brake travel. The wing will 
then surge violently forward and could reach a point below you. It is most 
important to maintain brake pressure until the glider has returned to its 
default overhead flying position.

To resume normal flight conditions, progressively and symmetrically 
release the brake line tension to regain air speed. When the wing reaches 
the overhead position, the brakes must be fully released. The wing will 
then surge forward to regain full air speed. Do not brake excessively at 
this moment as the wing needs to accelerate to pull away from the stall 
configuration. If you have to control a possible frontal collapse, briefly 
pull both brake handles down to bring the wing back up and release 
them immediately while the glider is still in transition to reposition itself 
overhead.

Cravat
A cravat may happen after an asymmetric collapse, when the end 
of the wing is trapped between the lines. Depending on the nature 
of the tangle, this situation could rapidly cause the wing to spin. The 

Summary of Contents for KOYOT 4

Page 1: ...KOYOT 4 User s manual...

Page 2: ...user manual and we recommend you read it carefully The NIVIUK Gliders Team USER S MANUAL NIVIUK Gliders KOYOT 4 This manual provides you with the necessary information on the main characteristics of...

Page 3: ...IN FLIGHT 10 4 1 FLYING IN TURBULENCE 10 4 2 POSSIBLE CONFIGURATIONS 10 4 3 ACCELERATED FLIGHT 12 4 4 FLYING WITHOUT BRAKE LINES 12 4 5 KNOT S IN FLIGHT 12 5 LOSING ALTITUD 13 5 1 BIG EARS 13 5 2 B3...

Page 4: ...different size wings will react differently during manoeuvres Even within the same size at maximum or minimum load the behaviour and reactions of the wing may vary Description of flight characteristi...

Page 5: ...or parasitic drag This optimises glide in all phases of the flight Because the flexible rods always return to their original shape the integrity of the profile is never affected Nitinol provides the h...

Page 6: ...erials used to manufacture the wing can be viewed in the final pages of this manual 1 5 ELEMENTS COMPONENTS The KOYOT 4 is delivered with a series of accessories that will greatly assist you in the ma...

Page 7: ...see below The speed system is engaged when the pilot pushes the speed bar included as standard with this glider model with their feet see 2 5 1 Speed system assembly The speed system uses an action re...

Page 8: ...hould not require a great deal of physical effort Inflate the wing with a little pressure from the body using the harness This may be assisted by using the A lines Do not pull on them just accompany t...

Page 9: ...is especially important Choose an appropriate location facing the wind Position the paraglider in a crescent configuration to facilitate inflation A clean wing layout will ensure a trouble free take...

Page 10: ...o long in case this induces a stall If you have to take corrective action make the input then re establish the correct flying speed 4 2 POSSIBLE CONFIGURATIONS To become familiar with the possible inc...

Page 11: ...ble with this wing If it did enter into a parachutal stall the wing loses forward motion becomes unstable and there is a lack of pressure on the brake lines although the canopy appears to be fully inf...

Page 12: ...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 obst...

Page 13: ...brakes This can obviously lead to a significant speed decrease In KOYOT 4s with a very pronounced arc pulling big ears means an increase in drag On a very arched wing the ears do not fold they just h...

Page 14: ...e KOYOT 4 The airflow over the profile is interrupted and the wing enters a situation similar to parachuting To enter this manoeuvre the B risers are gripped below the maillons and symmetrically pulle...

Page 15: ...ECIAL METHODS 6 1 TOWING The KOYOT 4 does not experience any problem whilst being towed Only qualified winch personnel should handle the certified equipment to carry out this operation The wing must b...

Page 16: ...the sun Pack it properly and stow it away in its backpack If your wing is wet from contact with salt water immerse it in fresh water and dry it away from direct sunlight 7 2 STORAGE It is important f...

Page 17: ...vere life changing injuries to the pilot or even death Manufacturers and dealers cannot be held responsible for your decisions actions or accidents that may result from participating in this sport You...

Page 18: ...18...

Page 19: ...19...

Page 20: ...m2 18 75 20 45 22 16 23 86 26 42 CORD MAXIMUM m 2 64 2 76 2 87 2 98 3 14 LINES TOTAL m 220 226 240 245 263 MAIN 2 1 3 2 2 1 3 2 2 1 3 2 2 1 3 2 2 1 3 2 RISERS NUMBER 3 1 A A B C A A B C A A B C A A B...

Page 21: ...CK SPORTWARE CO CHINA THREAD SERAFIL 60 AMAN GERMANY SUSPENSION LINES FABRIC CODE SUPPLIER UPPER CASCADES TNL 80 TEIJIM LIMITED JAPAN UPPER CASCADES TNL 140 TEIJIM LIMITED JAPAN MIDDLE CASCADES TNL 80...

Page 22: ...10 3 RISERS PLAN 22...

Page 23: ...10 4 SUSPENSION PLAN 23...

Page 24: ...0 340 340 383 470 A B C D BR 1 5873 5776 5825 5935 6769 2 5839 5741 5795 5907 6447 3 5799 5709 5769 5876 6324 4 5763 5677 5743 5842 6177 5 5702 5637 5724 5825 6013 6 5595 5542 5617 5705 6024 7 5530 54...

Page 25: ...0 340 340 383 470 A B C D BR 1 6688 6573 6634 6759 7693 2 6655 6539 6606 6731 7333 3 6615 6512 6582 6703 7196 4 6578 6480 6555 6667 7034 5 6513 6440 6538 6657 6852 6 6394 6334 6419 6524 6868 7 6322 62...

Page 26: ...7596 4 6952 6848 6929 7047 7427 5 6891 6809 6911 7031 7237 6 6766 6699 6787 6892 7254 7 6685 6648 6757 6838 7318 8 6478 6429 6325 7159 9 6209 6248 6997 10 6893 A A B C 470 470 470 470 340 340 383 470...

Page 27: ...A 3 A 4 A 5 A 6 A 7 A 8 A 9 A 10 A 11 A 12 A 13 A 14 A 15 A 16 A 17 A 18 A 19 A 20 A 21 A 22 A 23 0 Classification A In accordance with standards EN 926 2 2013 EN 926 1 2015 LTF 91 09 PG_1547 2019 Da...

Page 28: ...4 A 5 A 6 A 7 A 8 A 9 A 10 A 11 A 12 A 13 A 14 A 15 A 16 A 17 A 18 A 19 A 20 A 21 A 22 A 23 0 Classification A In accordance with standards EN 926 2 2013 EN 926 1 2015 LTF 91 09 PG_1550 2019 Date of i...

Page 29: ...niviuk com...

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