Twist occurs
No
A No
A
Cascade occurs
No
A No
A
With 75% 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°
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
A No
A
Twist occurs
No
A No
A
Cascade occurs
No
A No
A
15. Directional control with a maintained asymmetric collapse
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
Spin occurs
No
A No
A
17. Low speed spin tendency
Spin occurs
No
A No
A
18. Recovery from a developed spin
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
Change of course before release
Change of course less than 45°
A Change of 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
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
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
Behaviour immediately after releasing the accelerator while Stable flight
A Stable flight
A
22. Behaviour exiting a steep spiral
Tendency to return to straight flight
Spontaneous exit
A Spontaneous exit
A
Turn angle to recover normal flight
Less than 720°,spontaneous recovery
A Less than 720°,spontaneous recovery
A
Sink rate when evaluating spiral stability [m/s]
18 m/s
19 m/s
23. Alternative means of directional control
180° turn achievable in 20 s
Yes
A Yes
A
Stall or spin occurs
No
A No
A
24. Any other flight procedure and/or configuration described in the user's manual
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
Comments of test pilot
Comments
no
no
Air Turquoise
Rue de la Poterlaz 6
Case postale 10
CH- 1844 Villeneuve
Switzerland
mobile: +41 79 202 52 30
Tel. no : +41 21 965 65 65
fax : +41 219 65 65 66
email: info@airturquoise.ch
homepage: www.para-test.com
28
13
Class:
B
Accordance with
EN
standards
926-2:2005
&
926-1:2006
Date of issue (D.M.Y):
PG 107.2007
13.02.2008
MODEL:
SKY COUNTRY
DISCOVERY 3-27
Configuration during flight tests
Harness used for flight tests (maxi weight)
Maximum total weight in flight:
Minimum total weight in flight:
Weight of the paraglider:
Number of risers:
Type:
Brand name:
Model:
Seat to lowest part
of risers distance:
Distance between top of
connectors centerlines:
Accessories
Range of the speed
system:
Speed range using brakes:
Range of trimmers:
Total speed range with
accessories:
Inspections
(whichever happens earlier)
:
Serial no: ..........................................................
Date of manufacturing: ....................................
Warning ! before use refer to user 's manual.
Conformity tests according to EN 926-2:2005 & EN 926-1:2006 standards carried out by:
AIR TURQUOISE
Rue de la Poterlaz, 6
Case postale 10
1844 Villeneuve
Switzerland
Tel
00-41 (0) 79 202 52 30
Tel 2
00-41 (0) 78 694 65 66
Fax
00-41 (0) 21 965 65 66
info@airturquoise.ch
www.para-test.com
80 kg
100 kg
6.4 kg
4
ABS
Sol Paragliders
Slider L
46
45
No
13
2 years or 100 hours flying time
MANUFACTURER:
Paraglider
Person or compagny having presented
the glider for testing:
23.79
Projected area:
m
2
None
For detailed information regarding harness
settings used for flight tests, please refer to
flight tests reports.
cm
cm
cm
cm
km/h
km/h
A
B
C
D
1
2
3
4
5
6
7
8
9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24
x x
x
x
x
x x
x
x x
x
x
x
x
x x
x
x
x
x
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www.sc.com.ua
sky_country@mail.ru
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