Rocking back less than 45°. SOL SPORTS. Rua Walter Marquardt, 1180. Jaraguá do Sul/SC - Brasil. Flight Test Report -. Musterprüfnummer: Seite 1 von 2.
1. Inflation / take-off - 4.4.1 Easy rising, some pilot correction is required No
Rising behavior Special take off technique required 2. Landing - 4.4.2
B A
Easy rising, some pilot correction is required No
B A
No
A
No
A
Trim speed more than 30km/h
Yes
A
Yes
A
Speed range using the controls larger than 10km/h
Yes
A
Yes
A
Minimum speed
25 km/h to 30 km/h
B
25 km/h to 30 km/h
B
C
Increasing
Reducing
A
Reducing
A
Spontaneous exit
A
Spontaneous exit
A
No immediate reaction Spontaneous exit 720° to 1080°, spontaneous recovery
B A B
No immediate reaction Spontaneous exit 1080° to 1440°, spontaneous recovery
B A C
No Rocking back less than 45°
A
No Rocking back less than 45°
A
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
30° - 60° No
B A
0° - 30° No
A A
Special landing technique required 3. Speeds in straight flight - 4.4.3
4. Control movement - 4.4.4 Max. weight in flight greater than 100kg
Increasing
50cm - 65cm
A
> 65cm
7. Roll stability and damping - 4.4.7 Oscillations 8. Stability in gentle spirals - 4.4.8 Tendency to return to straight flight 9. Behaviour exiting a fully developed spiral dive - 4.4.9 Initial response of glider (first 180°) Tendency to return to straight flight Turn angle to recover normal flight Folding lines used Entry Recovery Dive forward angle on exit Cascade occurs
accelerated > 50%
10. Symmetric front collapse - 4.4.10
Entering a turn of less than 90°
Keeping course
11. Exiting deep stall (parachutal stall) - 4.4.11 Deep stall achieved
Yes
Recovery
Spontaneous in less than 3 sec
A
Yes Spontaneous in less than 3 sec
A
Dive forward angle on exit Change of course Cascade occurs
30° - 60° Changing course less than 45° No
B A A
30° - 60° Changing course less than 45° No
B A A
Recovery
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
Cascade occurs
No
A
No
A
30° - 60° No collapse No Less than 45° Most lines tight
B A A A A
30° - 60° No collapse No Less than 45° Most lines tight
B A A A A
B
< 90°
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Less than 360° No No No
A A A A
Less than 360° No No No
A A A A
C
90° - 180°
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Less than 360° Yes, no turn reversal No No
A C A A
Less than 360° Yes, no turn reversal No No
A C A A
12. High angle of attack recovery - 4.4.12
13. Recovery from a developed full stall - 4.4.13 Dive forward angle on exit Collapse Cascade occurs (other than collapse) Rocking backward Line tension 14. Asymmetric collapse (accelerated) - 4.4.14 No
Change of course until re-inflation
90° - 180°
Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs Change of course until re-inflation Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs
Flight Test Report -
Musterprüfnummer:
accelerated, max 75% collapse
Re-inflation behavior
accelerated, max 50% collapse
Folding lines used
90° - 180°
No Dive or roll angle
Dive or roll angle
15° - 45°
45° - 60°
EAPR-GS-0377/15
Dive or roll angle
Dive or roll angle
15° - 45°
45° - 60°
A
C
Seite 1 von 2
15. Directional control with a maintained asymmetric collapse - 4.4.15 Able to keep course straight
Yes
A
Yes
A
180° turn away from the collapsed side possible in 10 sec
Yes
A
Yes
A
Amount of control range between turn and stall or spin
25% to 50% of the symmetric control travel
C
More than 50% of the symmetric control travel
A
No
A
No
A
No
A
No
A
Spin rotation angle after release
Stops spinning in less than 90°
A
Stops spinning in 90° to 180°
C
Cascade occurs
No
A
No
A
16. Trim speed spin tendency - 4.4.16 Spin occurs 17. Low speed spin tendency - 4.4.17 Spin occurs 18. Recovery from a developed spin - 4.4.18
19. B-line-stall - 4.4.19 Change of course before release
Changing course less than 45°
A
Changing course less than 45°
A
Behaviour before release
Remains stable with straight span
A
Remains stable with straight span
A
Recovery
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
Dive forward angle on exit Cascade occurs
30° - 60° No
A A
0° - 30° No
A A
Entry procedure
Standard technique
A
Special device required
A
Behaviour during big ears
Stable flight
A
Stable flight
A
Recovery
Spontaneous in 3 to 5 sec
B
Spontaneous in 3 to 5 sec
B
Dive forward angle on exit
0° - 30° Stable flight
A A
0° bis 30° Stable flight
A A
180° turn achievable in 20 sec
Yes
A
Yes
A
Stall or spin occurs
No
A
No
21. Big Ears in accelerated flight - 4.4.21
Behavior when closing the trimmer while maintaining big ears
23. Alternative means of directional control - 4.4.22
A
23. Any other flight procedure and/or configuration described in the user's manual - 4.4.23
NA NA NA
Procedure works as descibed Procedure suitable for novice pilots Cascade occurs
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