SS-C1-XS-1611-002. Representative. None. Trimmer no. Place of test. Villeneuve. Folding lines used no. Test pilot. Fukuoka Seiko. Thurnheer Claude. Harness.
Flight test report: EN 926-2:2013 & LTF 91/09 Manufacturer
Supair Sàrl
Certification number
PG_1142.2017
Address
Parc Altais / 34 rue Adrastée 74650 Chavanod France
Date of flight test
10. 03. 2017
Glider model
Taska XS
Classification
C
Serial number
SS-C1-XS-1611-002
Representative
None
Trimmer
no
Place of test
Villeneuve
Folding lines used
no
Test pilot
Fukuoka Seiko
Thurnheer Claude
Harness
Supair - Altiplume S
Advance - Success 4 M
Harness to risers distance (cm)
40
44
Distance between risers (cm)
48
44
Total weight in flight (kg)
65
85
1. Inflation/Take-off
A
Rising behaviour
Smooth, easy and constant rising A
Smooth, easy and constant rising
A
Special take off technique required
No
A
No
A
2. Landing
A
Special landing technique required
No
A
No
A
3. Speed in straight flight
B
Trim speed more than 30 km/h
Yes
A
Yes
A
Speed range using the controls larger than 10 km/h
Yes
A
Yes
A
Minimum speed
Less than 25 km/h
A
25 km/h to 30 km/h
B
4. Control movement
C
Increasing / greater than 55 cm
A
not available
0
not available
0
Increasing / 45 cm to 60 cm
C
Symmetric control pressure / travel
not available
0
not available
0
5. Pitch stability exiting accelerated flight
A
Dive forward angle on exit
Dive forward less than 30°
A
Dive forward less than 30°
A
Collapse occurs
No
A
No
A
6. Pitch stability operating controls during accelerated flight
A
Collapse occurs
No
A
No
A
7. Roll stability and damping
A
Oscillations
Reducing
A
Reducing
A
8. Stability in gentle spirals
A
Tendency to return to straight flight
Spontaneous exit
A
Spontaneous exit
A
9. Behaviour exiting a fully developed spiral dive
B
Initial response of glider (first 180°)
No immediate reaction
B
No immediate reaction
B
Tendency to return to straight flight
Spontaneous exit (g force decreasing, rate of turn decreasing)
A
Spontaneous exit (g force decreasing, rate of turn decreasing)
A
Max. weight in flight up to 80 kg Symmetric control pressure / travel Max. weight in flight 80 kg to 100 kg Symmetric control pressure / travel Max. weight in flight greater than 100 kg
Test Report generated automatically by AIR TURQUOISE SA, valid without signature
//
GB | REV 04 | 07.06.2016
//
ISO | 71.8.2
//
Page 1 of 4
Turn angle to recover normal flight
720° to 1 080°, spontaneous recovery
10. Symmetric front collapse
B
B
720° to 1 080°, spontaneous recovery
B
Approximately 30 % chord Entry
Rocking back less than 45°
A
Rocking back less than 45°
A
Recovery
Spontaneous in less than 3 s
A
Spontaneous in less than 3 s
A
Dive forward angle on exit Change of course
Dive forward 0° to 30° Keeping course
A
Dive forward 0° to 30° Keeping course
A
Cascade occurs
No
A
No
A
Folding lines used
No
No
At least 50% chord Entry
Rocking back less than 45°
A
Rocking back less than 45°
A
Recovery
Spontaneous in less than 3 s
A
Spontaneous in 3 s to 5 s
B
Dive forward angle on exit / Change of course
Dive forward 30° to 60° / Entering a turn of less than 90°
B
Dive forward 30° to 60° / Keeping course
B
Cascade occurs
No
A
No
A
Folding lines used
No
No
With accelerator Entry
Rocking back less than 45°
A
Rocking back less than 45°
A
Recovery
Spontaneous in 3 s to 5 s
B
Spontaneous in 3 s to 5 s
B
Dive forward angle on exit / Change of course
Dive forward 30° to 60° / Entering a turn of less than 90°
B
Dive forward 30° to 60° / Keeping course
B
Cascade occurs
No
A
No
A
Folding lines used
No
11. Exiting deep stall (parachutal stall)
A
Deep stall achieved
Yes
A
Yes
A
Recovery
Spontaneous in less than 3 s
A
Spontaneous in less than 3 s
A
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 0° to 30°
A
Change of course
Changing course less than 45°
A
Changing course less than 45°
A
Cascade occurs
No
A
No
A
12. High angle of attack recovery
A
Recovery
Spontaneous in less than 3 s
A
Spontaneous in less than 3 s
A
Cascade occurs
No
A
No
A
13. Recovery from a developed full stall
A
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 0° to 30°
A
Collapse
No collapse
A
No collapse
A
Cascade occurs (other than collapses)
No
A
No
A
Rocking back
Less than 45°
A
Less than 45°
A
Line tension
Most lines tight
A
Most lines tight
A
14. Asymmetric collapse
B
No
Small asymmetric collapse Change of course until re-inflation / Maximum dive forward or roll angle
Less than 90° / Dive or roll angle 15° to 45°
A
Less than 90° / Dive or roll angle 15° to 45°
A
Re-inflation behaviour
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Total change of course
Less than 360°
A
Less than 360°
A
Collapse on the opposite side occurs
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
Twist occurs
No
A
No
A
Cascade occurs
No
A
No
A
Folding lines used
No
No
Large asymmetric collapse Change of course until re-inflation / Maximum dive forward or roll angle
90° to 180° / Dive or roll angle 15° to 45°
B
90° to 180° / Dive or roll angle 15° to 45°
B
Re-inflation behaviour
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Total change of course
Less than 360°
A
Less than 360°
A
Test Report generated automatically by AIR TURQUOISE SA, valid without signature
//
GB | REV 04 | 07.06.2016
//
ISO | 71.8.2
//
Page 2 of 4
Collapse on the opposite side occurs
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
Twist occurs
No
A
No
A
Cascade occurs
No
A
No
A
Folding lines used
No
No
Small asymmetric collapse with fully activated accelerator Change of course until re-inflation / Maximum dive forward or roll angle
Less than 90° / Dive or roll angle 15° to 45°
A
Less than 90° / Dive or roll angle 15° to 45°
A
Re-inflation behaviour
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Total change of course
Less than 360°
A
Less than 360°
A
Collapse on the opposite side occurs
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
Twist occurs
No
A
No
A
Cascade occurs
No
A
No
A
Folding lines used
No
No
Large asymmetric collapse with fully activated accelerator Change of course until re-inflation / Maximum dive forward or roll angle
90° to 180° / Dive or roll angle 15° to 45°
B
90° to 180° / Dive or roll angle 15° to 45°
B
Re-inflation behaviour
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Total change of course
Less than 360°
A
Less than 360°
A
Collapse on the opposite side occurs
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
Twist occurs
No
A
No
A
Cascade occurs
No
A
No
A
Folding lines used
No
15. Directional control with a maintained asymmetric collapse
A
Able to keep course
Yes
A
Yes
A
180° turn away from the collapsed side possible in 10 s
Yes
A
Yes
A
Amount of control range between turn and stall or spin
More than 50 % of the symmetric control travel
A
More than 50 % of the symmetric control travel
A
16. Trim speed spin tendency
A
Spin occurs
No
A
No
A
17. Low speed spin tendency
A
Spin occurs
No
A
No
A
18. Recovery from a developed spin
A
Spin rotation angle after release
Stops spinning in less than 90°
A
Stops spinning in less than 90°
A
Cascade occurs
No
A
No
A
19. B-line stall
A
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 s
A
Spontaneous in less than 3 s
A
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 0° to 30°
A
Cascade occurs
No
A
No
A
20. Big ears
A
Entry procedure
Dedicated controls
A
Dedicated controls
A
Behaviour during big ears
Stable flight
A
Stable flight
A
Recovery
Spontaneous in less than 3 s
A
Spontaneous in less than 3 s
A
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 0° to 30°
A
21. Big ears in accelerated flight
B
Entry procedure
Dedicated controls
A
Dedicated controls
A
Behaviour during big ears
Stable flight
A
Stable flight
A
Recovery
Spontaneous in less than 3 s
A
Recovery through pilot action in less than a further 3 s
B
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 0° to 30°
A
Test Report generated automatically by AIR TURQUOISE SA, valid without signature
No
//
GB | REV 04 | 07.06.2016
//
ISO | 71.8.2
//
Page 3 of 4
Behaviour immediately after releasing the accelerator while maintaining big ears
Stable flight
A
Stable flight
A
22. Alternative means of directional control
A
180° turn achievable in 20 s
Yes
A
Yes
A
Stall or spin occurs
No
A
No
A
23. Any other flight procedure and/or configuration described in the user's manual
0
Procedure works as described
not available
0
not available
0
Procedure suitable for novice pilots
not available
0
not available
0
Cascade occurs
not available
0
not available
0
24. Comments of test pilot Comments
Test Report generated automatically by AIR TURQUOISE SA, valid without signature
Line measurement of Flight test glider. Inspection report number : PG_1001.2015. S/N: PR1-Q-39D-150. Gliders Manufacturers name: Ozone Jomo XS. Value : ...
Leaf Light XS. Serial number: SA-BL1-XS-1606-002. Configuration during flight tests. Paraglider. Accessories. Maximum weight in flight (kg). 80. Range of speed ...
Classification of a paraglider's behaviour in the asymmetric collapse test to 50%. Cascade occurs. Recovery. Deep stall achieved. No. A. Dive forward angle on ...
In accordance with EN standards 926-2:2013 & 926-1:2006: PG_1001.2015. Date of issue (DMY):. 17. 12. 2015. Manufacturer: Ozone Gliders. Model: Jomo XS.
C. 0. 0. -. Test-criteria. Minimum take off weight. Maximum take off weight. Special take off technique ... Smooth, easy and constant rising, no pilot correction ...
Manufacturer: Sky Paragliders a.s.. Model: Apollo XS. Serial number: 2151â11â0605. Configuration during flight tests. Paraglider. Accessories. Maximum weight ...
In accordance with EN standards 926-2:2013 & 926-1:2006: PG_0933.2015. Date of issue (DMY):. 12. 05. 2015. Manufacturer: Ozone Gliders. Model: Mojo 5 XS.
In accordance with EN standards 926-2:2005 & 926-1:2006: PG_0730.2013. Date of issue (DMY):. 25. 09. 2013. Manufacturer: Ozone Gliders. Model: Geo 4 XS.
In accordance with EN standards 926-2:2013 & 926-1:2006: PG_0933.2015. Date of issue (DMY):. 12. 05. 2015. Manufacturer: Ozone Gliders. Model: Mojo 5 XS.
14. 06. 2013. Manufacturer: Ozone Gliders. Model: Buzz Z4 XS. Serial number: ... Access S. Person or company having presented the glider for testing: none.
In accordance with EN standards 926-2:2013 & 926-1:2006: PG_1010.2015. Date of issue (DMY):. 29. 04. 2016. Manufacturer: Ozone Gliders. Model: Buzz Z5 ...
During installation, observ e the applicable safety regulations for your country. 8. Never install and ... Power cables to power multiple devices must have a cross-section of at least 1.5 mm². Within the EU ..... (valid in the European Union and oth
Please read this User's Manual carefully, so that you can begin making optimum ... Veuillez lire attentivement ce Manuel Utilisateur : vous apprendrez rapidement à utiliser votre appareil Cameo Light de façon optimale. .... The warning triangle wit