Flight test report Dudek Paragliders ul. Centralna 2U 86-031 Osielsko Poland Representive None Type of glider Synthesis 31 Trimmer Closed trimmer Manufacturer

Certification number

Address

Date of flight test Place of test

PG 088.2007 07/06/2007 Villeneuve

Classification C

Test Pilot Harness Total weight in flight

Alain Zoller Sol Paragliders - Slider L 110 kg

Min weight 1. Inflation/Take-off Rising behaviour Smooth, easy and constant rising Special take off technique required No 2. Landing Special landing technique required No 3. Speed in straight flight Trim speed more than 30 km/h Yes Speed range using the controls larger than 10 km/h Yes Minimum speed Less than 25 km/h 4. Control movement Max. weight in flight up to 80 kg Symmetric control pressure/travel not available Max. weight in flight 80 kg to 100 kg Symmetric control pressure/travel not available Max. weight in flight greater than 100 kg Symmetric control pressure/travel Increasing, Greater than 65 cm 5. Pitch stability exiting accelerated flight Dive forward angle on exit Dive forward less than 30° Collapse occurs No 6. Pitch stability operating controls during accelerated flight Collapse occurs No 7. Roll stability and damping Oscillations Reducing 8. Stability in gentle spirals Tendency to return to straight flight Spontaneous exit 9. Behaviour in a steeply banked turn Sink rate after two turns More than 14 m/s 10. Symmetric front collapse Entry Rocking back less than 45° Recovery Spontaneous in less than 3 s Dive forward angle on exit Dive foward 0°to 30°, Keeping course Cascade occurs No With accelerator Entry Rocking back less than 45° Recovery Spontaneous in less than 3 s Dive forward angle on exit Dive foward 0°to 30°, Keeping course Cascade occurs No 11. Exiting deep stall (parachutal stall) Deep stall achieved Yes Recovery Spontaneous in less than 3 s Dive forward angle on exit Dive forward 0°to 30° Change of course Changing course less than 45° Cascade occurs No 12. High angle of attack recovery Recovery Spontaneous in less than 3 s Cascade occurs No 13. Recovery from a developed full stall Dive forward angle on exit Dive forward 0°to 30° Collapse No collapse Cascade occurs (other than collapse) No Rocking back Less than 45° Line tension Most line tight 14. Asymmetric collapse With 50% collapse-Maximum dive forward or roll angle Change of course until re-inflation Less than 90°, Dive or roll angle 15° to 45° Re-inflation behaviour Spontaneous re-inflation Total change of course Less than 360° Collapse on the opposite side occurs No Twist occurs No Cascade occurs No With 75% collapse-Maximum dive forward or roll angle Change of course until re-inflation 90° to 180°, Dive or roll angle 45° to 60° Re-inflation behaviour Spontaneous re-inflation Total change of course Less than 360° Collapse on the opposite side occurs No Twist occurs No Cascade occurs No With 50% collapse and accelerator-Maximum dive forward or roll angle Change of course until re-inflation 90° to 180°, Dive or roll angle 15° to 45° Re-inflation behaviour Spontaneous re-inflation Total change of course Less than 360° Collapse on the opposite side occurs No

Claude Thurnheer Advance Bi-pro 135 kg Max weight A Smooth, easy and constant rising A No

A A

A No

A

A Yes A Yes A 25 km/h to 30 km/h

A A B

0 not available 0 not available

0 0

A Increasing, Greater than 65 cm

A

A Dive forward less than 30° A No

A A

A No

A

A Reducing

A

A Spontaneous exit

A

B More than 14 m/s

B

A A A A

Rocking back less than 45° Spontaneous in less than 3 s Dive foward 0°to 30°, Keeping course No

A A A A

A A A A

Rocking back less than 45° Spontaneous in less than 3 s Dive foward 0°to 30°, Keeping course No

A A A A

A A A A A

Yes Spontaneous in less than 3 s Dive forward 0°to 30° Changing course less than 45° No

A A A A A

A Spontaneous in less than 3 s A No

A A

A A A A A

Dive forward 30°to 60° No collapse No Less than 45° Most line tight

B A A A A

A A A A A A

Less than 90°, Dive or roll angle 15° to 45° Spontaneous re-inflation Less than 360° No No No

A A A A A A

C A A A A A

90° to 180°, Dive or roll angle 15° to 45° Spontaneous re-inflation Less than 360° No No No

B A A A A A

B A A A

Less than 90°, Dive or roll angle 45° to 60� Spontaneous re-inflation Less than 360° No

C A A A

Twist occurs No Cascade occurs No With 75% collapse and accelerator-Maximum dive forward or roll angle Change of course until re-inflation 90° to 180°, Dive or roll angle 45° to 60° Re-inflation behaviour Spontaneous re-inflation Total change of course Less than 360° Collapse on the opposite side occurs No Twist occurs No Cascade occurs No 15. Directional control with a maintained asymmetric collapse Able to keep course Yes 180° turn away from the collapsed side possible in 10 s Yes Amount of control range between turn and stall or spin More than 50 % of the symmetric control travel 16. Trim speed spin tendency Spin occurs No 17. Low speed spin tendency Spin occurs No 18. Recovery from a developed spin Spin rotation angle after release Stops spinning in less than 90° Cascade occurs No 19. B-line stall Change of course before release Change of course less than 45° Behaviour before release Remains stable with straight span Recovery Spontaneous in less than 3 s Dive forward angle on exit Dive forward 0° to 30° Cascade occurs No 20. Big ears Entry procedure Dedicated controls Behaviour during big ears Stable flight Recovery Spontaneous in less than 3 s Dive forward angle on exit Dive forward 0° to 30° 21. Big ears in accelerated flight Entry procedure not available Behaviour during big ears not available Recovery not available Dive forward angle on exit not available Behaviour immediately after releasing the accelerator while not available 22. Behaviour exiting a steep spiral Tendency to return to straight flight Spontaneous exit Turn angle to recover normal flight Less than 720°,spontaneous recovery Sink rate when evaluating spiral stability [m/s] 21 m/s 23. Alternative means of directional control 180° turn achievable in 20 s Yes Stall or spin occurs No 24. Any other flight procedure and/or configuration described in the user's manual Procedure works as described Yes Procedure suitable for novice pilots Yes Cascade occurs No Comments of test pilot Comments Impossible to make B-Stall with accelerator

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A No A No

A A

C A A A A A

90° to 180°, Dive or roll angle 45° to 60� Spontaneous re-inflation Less than 360° No No No

C A A A A A

A Yes A Yes A More than 50 % of the symmetric control travel

A A A

A No

A

A No

A

A Stops spinning in less than 90° A No

A A

A A A A A

Change of course less than 45° Remains stable with straight span Spontaneous in less than 3 s Dive forward 0° to 30° No

A A A A A

A A A A

Dedicated controls Stable flight Spontaneous in less than 3 s Dive forward 0° to 30°

A A A A

Dedicated controls Stable flight Spontaneous in 3 s to 5 s Dive forward 0° to 30° Stable flight

A A A A A

0 0 0 0 0

A Spontaneous exit A Less than 720°,spontaneous recovery 24 m/s

A A

A Yes A No

A A

A Yes A Yes A No

A A A

no