14 Minimum weight in flight (kg) 14 Glider's weight (kg) 20 Projected area (m2) ABS. every 12 months or every 100 flying hours Harness brand

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2 Class: PG_ In accordance with EN standards 926-2:25 & 926-1:26: Date of issue (DMY): Manufacturer: Model: pco viation Ltd. Karma Evo S Serial number: Configuration during flight tests Paraglider ccessories Maximum weight in flight (kg) 95 Range of speed system (cm) Minimum weight in flight (kg) 7 Speed range using brakes (km/h) Glider's weight (kg) 4.9 Range of trimmers (cm) Number of risers 3 Total speed range with accessories (km/h) 2 Projected area (m2) Harness used for testing (max weight) Inspections (whichever happens first) Harness type BS every 12 months or every 1 flying hours Harness brand Sup'ir Warning! Before use refer to user's manual Harness model XX-Lite Person or company having presented the glider for testing: ne Harness to risers distance (cm) 49 Distance between risers (cm)

3 Flight test report: EN Manufacturer pco viation Ltd. Certification number PG_ ddress 7, Chalamish St., Industrial park 389 Caesarea Israel Date of flight test Representative ne Place of test Villeneuve Glider model Karma Evo S Classification Trimmer no Test pilot Thurnheer Claude Zoller lain Harness Sup' ir - ccess M Sup'ir - XX-Lite Total weight in flight (kg) 7 1. Inflation/Take-off 95 Rising behaviour Smooth, easy and constant rising Smooth, easy and constant rising Special take off technique required 2. Landing Special landing technique required 3. Speed in straight flight Trim speed more than 3 km/h Speed range using the controls larger than 1 km/h Minimum speed Less than 25 km/h Less than 25 km/h 4. Control movement Increasing / greater than 55 cm Increasing / greater than 6 cm 5. Pitch stability exiting accelerated flight Max. weight in flight up to 8 kg Max. weight in flight 8 kg to 1 kg Max. weight in flight greater than 1 kg Dive forward less than 3 Dive forward less than 3 Collapse occurs 6. Pitch stability operating controls during accelerated flight Reducing 12 m/s to m/s Collapse occurs 7. Roll stability and damping Oscillations Reducing 8. Stability in gentle spirals Tendency to return to straight flight 9. Behaviour in a steeply banked turn Sink rate after two turns 12 m/s to m/s 1. Symmetric front collapse Entry / Change of Dive forward to 3 / Keeping Dive forward to 3 / Keeping With accelerator Entry Flight test report: PG_ / page 1 of 3

4 / Change of Dive forward to 3 / Keeping Dive forward to 3 / Keeping 11. Exiting deep stall (parachutal stall) Deep stall achieved Dive forward to 3 Dive forward to 3 Change of Changing less than 45 Changing less than High angle of attack recovery 13. from a developed full stall Dive forward to 3 Dive forward to 3 Collapse collapse collapse (other than collapses) Rocking back Less than 45 Less than 45 Line tension Most lines tight Most lines tight. symmetric collapse Less than 9 / Dive or Less than 9 / Dive or With 5% collapse Change of until re-inflation / Maximum dive forward or Less than 36 Less than 36 9 to / Dive or Less than 9 / Dive or With 75% collapse Change of until re-inflation / Maximum dive forward or Less than 36 Less than 36 Less than 9 / Dive or Less than 9 / Dive or With 5% collapse and accelerator Change of until re-inflation / Maximum dive forward or Less than 36 Less than 36 Less than 9 / Dive or Less than 9 / Dive or With 75% collapse and accelerator Change of until re-inflation / Maximum dive forward or Less than 36 Less than Directional control with a maintained asymmetric collapse ble to keep turn away from the collapsed side possible in 1 s mount of control range between turn and stall or spin More than 5 % of the symmetric control travel More than 5 % of the symmetric control travel Flight test report: PG_ / page 2 of 3

5 16. Trim speed spin tendency Spin occurs 17. Low speed spin tendency Spin occurs. from a developed spin Spin rotation angle after release Stops spinning in less than 9 Stops spinning in less than B-line stall Change of before release Changing less than 45 Changing less than 45 Behaviour before release Remains stable with straight span Remains stable with straight span Dive forward to 3 Dive forward to 3 2. Big ears Entry procedure Behaviour during big ears Dive forward to 3 Dive forward to Big ears in accelerated flight Entry procedure Behaviour during big ears Dive forward to 3 Dive forward to 3 Behaviour immediately after releasing the accelerator while maintaining big ears 22. Behaviour exiting a steep spiral Tendency to return to straight flight Turn angle to recover normal flight Less than 72, spontaneous recovery Less than 72, spontaneous recovery Sink rate when evaluating spiral stability [m/s] 23. lternative means of directional control turn achievable in 2 s Stall or spin occurs 24. ny other flight procedure and/or configuration described in the user's manual Procedure works as described Procedure suitable for novice pilots 25. Comments of test pilot Comments Flight test report: PG_ / page 3 of 3