Class: Configuration during flight tests

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2 Class: In accordance with EN standards 926-2:2013 & 926-1:2006: PG_ Date of issue (DMY): Manufacturer: Sky Paragliders a.s. Model: nakis 3 XS Serial number: Configuration during flight tests Paraglider ccessories Maximum weight in flight (kg) 70 Range of speed system (cm) 15 Minimum weight in flight (kg) 55 Speed range using brakes (km/h) 13 Glider's weight (kg) 3.9 Range of trimmers (cm) 0 Number of risers 4 Total speed range with accessories (km/h) 25 Projected area (m2) Harness used for testing (max weight) Inspections (whichever happens first) Harness type S evey 12 months or every 100 flying hours Harness brand Supair Warning! efore use refer to user's manual Harness model Harness to risers distance (cm) 42 Distance between risers (cm) 40 ltiplume M Person or company having presented the glider for testing: none

3 Flight test report: EN 926-2:2013 Manufacturer Sky Paragliders a.s. Certification number PG_ ddress Okružní Frýdlant nad Ostravicí Czech Republic Date of flight test Glider model nakis 3 XS Classification Serial number Representative none Trimmer no Place of test Villeneuve Test pilot Light pilot under ir Turquoise supervision Dupont Philippe Harness Flugsau - XX-Lite Supair - ltiplume M Harness to risers distance (cm) Distance between risers (cm) Total weight in flight (kg) Inflation/Take-off Rising behaviour Smooth, easy and constant rising Smooth, easy and constant rising Special take off technique required No No 2. Landing Special landing technique required No No 3. Speed in straight flight Trim speed more than 30 km/h Yes Yes Speed range using the controls larger than 10 km/h Yes Yes Minimum speed Less than 25 km/h Less than 25 km/h 4. Control movement Max. weight in flight up to 80 kg Symmetric control pressure / travel Increasing / greater than 55 cm Increasing / greater than 55 cm Max. weight in flight 80 kg to 100 kg Symmetric control pressure / travel not available 0 not available 0 Max. weight in flight greater than 100 kg Symmetric control pressure / travel not available 0 not available 0 5. Pitch stability exiting accelerated flight Dive forward angle on exit Dive forward less than 30 Dive forward less than 30 Collapse occurs No No 6. Pitch stability operating controls during accelerated flight Collapse occurs No No 7. Roll stability and damping Oscillations Reducing Reducing 8. Stability in gentle spirals Tendency to return to straight flight Spontaneous exit Spontaneous exit 9. ehaviour exiting a fully developed spiral dive Initial response of glider (first 180 ) Tendency to return to straight flight Immediate reduction of rate of turn Spontaneous exit (g force decreasing, rate of turn decreasing) Immediate reduction of rate of turn Spontaneous exit (g force decreasing, rate of turn decreasing) Test Report generated automatically by IR TURQUOISE S, valid without signature // G REV // ISO // Page 1 of 4

4 Turn angle to recover normal flight 10. Symmetric front collapse Less than 720, spontaneous recovery Less than 720, spontaneous recovery pproximately 30 % chord Entry Rocking back less than 45 Rocking back less than 45 Recovery Spontaneous in less than 3 s Spontaneous in less than 3 s Dive forward angle on exit Change of Dive forward 0 to 30 Keeping Dive forward 0 to 30 Keeping Cascade occurs No No Folding lines used No No t least 50% chord Entry Rocking back less than 45 Rocking back less than 45 Recovery Spontaneous in less than 3 s Spontaneous in less than 3 s Dive forward angle on exit / Change of Cascade occurs No No Folding lines used No No With accelerator Entry Rocking back less than 45 Rocking back less than 45 Recovery Spontaneous in less than 3 s Spontaneous in 3 s to 5 s Dive forward angle on exit / Change of Cascade occurs No No Folding lines used No No 11. Exiting deep stall (parachutal stall) Deep stall achieved Yes Yes Recovery Spontaneous in less than 3 s Spontaneous in less than 3 s Dive forward angle on exit Dive forward 0 to 30 Dive forward 0 to 30 Change of Changing less than 45 Changing less than 45 Cascade occurs No No 12. High angle of attack recovery Recovery Spontaneous in less than 3 s Spontaneous in less than 3 s Cascade occurs No No 13. Recovery from a developed full stall Dive forward angle on exit Dive forward 0 to 30 Dive forward 0 to 30 Collapse No collapse No collapse Cascade occurs (other than collapses) No No Rocking back Less than 45 Less than 45 Line tension Most lines tight Most lines tight 14. symmetric collapse Small asymmetric collapse Change of until re-inflation / Maximum dive forward or Less than 90 / Dive or 0 to 15 Less than 90 / Dive or 15 to 45 Re-inflation behaviour Spontaneous re-inflation Spontaneous re-inflation Total change of Less than 360 Less than 360 spontaneous Twist occurs No No Cascade occurs No No Folding lines used No No Large asymmetric collapse Change of until re-inflation / Maximum dive forward or Less than 90 / Dive or 15 to to 180 / Dive or 15 to 45 Re-inflation behaviour Spontaneous re-inflation Spontaneous re-inflation Total change of Less than 360 Less than 360 Test Report generated automatically by IR TURQUOISE S, valid without signature // G REV // ISO // Page 2 of 4

5 spontaneous Twist occurs No No Cascade occurs No No Folding lines used No No Small asymmetric collapse with fully activated accelerator Change of until re-inflation / Maximum dive forward or Less than 90 / Dive or 0 to 15 Less than 90 / Dive or 0 to 15 Re-inflation behaviour Spontaneous re-inflation Spontaneous re-inflation Total change of Less than 360 Less than 360 spontaneous Twist occurs No No Cascade occurs No No Folding lines used No No Large asymmetric collapse with fully activated accelerator Change of until re-inflation / Maximum dive forward or Less than 90 / Dive or 15 to to 180 / Dive or 15 to 45 Re-inflation behaviour Spontaneous re-inflation Spontaneous re-inflation Total change of Less than 360 Less than 360 spontaneous Twist occurs No No Cascade occurs No No Folding lines used No No 15. Directional control with a maintained asymmetric collapse ble to keep Yes Yes 180 turn away from the collapsed side possible in 10 s Yes Yes mount of control range between turn and stall or spin 16. Trim speed spin tendency More than 50 % of the symmetric control travel More than 50 % of the symmetric control travel Spin occurs No No 17. Low speed spin tendency Spin occurs No No 18. Recovery from a developed spin Spin rotation angle after release Stops spinning in less than 90 Stops spinning in less than 90 Cascade occurs No No 19. -line stall Change of before release Changing less than 45 Changing less than 45 ehaviour before release Remains stable with straight span Remains stable with straight span Recovery Spontaneous in less than 3 s Spontaneous in less than 3 s Dive forward angle on exit Dive forward 0 to 30 Dive forward 0 to 30 Cascade occurs No No 20. ig ears Entry procedure Dedicated controls Dedicated controls ehaviour during big ears Stable flight Stable flight Recovery Spontaneous in less than 3 s Spontaneous in 3 s to 5 s Dive forward angle on exit Dive forward 0 to 30 Dive forward 0 to ig ears in accelerated flight Entry procedure Dedicated controls Dedicated controls ehaviour during big ears Stable flight Stable flight Recovery Spontaneous in less than 3 s Spontaneous in 3 s to 5 s Dive forward angle on exit Dive forward 0 to 30 Dive forward 0 to 30 Test Report generated automatically by IR TURQUOISE S, valid without signature // G REV // ISO // Page 3 of 4

6 ehaviour immediately after releasing the accelerator while maintaining big ears 22. lternative means of directional control Stable flight Stable flight 180 turn achievable in 20 s Yes Yes Stall or spin occurs No No 23. ny other flight procedure and/or configuration described in the user's manual Procedure works as described not available 0 Yes Procedure suitable for novice pilots not available 0 Yes Cascade occurs not available 0 No 24. Comments of test pilot Comments Test Report generated automatically by IR TURQUOISE S, valid without signature // G REV // ISO // Page 4 of 4