Type test reference no DHV GS-01-1822-09. Holder of certification Swing Flugsportgeräte GmbH. Manufacturer Swing Flugsportgeräte GmbH. Classification B.
SWING Arcus 6.22 Type designation SWING Arcus 6.22 Type test reference no DHV GS-01-1822-09 Holder of certification Swing Flugsportgeräte GmbH Manufacturer Swing Flugsportgeräte GmbH Classification B Winch towing Yes Number of seats min / max 1 / 1 Accelerator Yes Trimmers No
Inflation/take-off
Behaviour at min weight in flight (70kg)
Behaviour at max weight in flight (80kg)
Videocutting in process
Videocutting in process
A
A
Rising behaviour Smooth, easy and constant rising Special take off technique required No
A
Landing
Special landing technique required No
A
Speeds in straight flight
Smooth, easy and constant rising No
A No
A
Trim speed more than 30 km/h Yes
Yes
Speed range using the controls larger than 10 km/h Yes
Yes
Minimum speed Less than 25 km/h
A
Control movement
Symmetric control pressure Increasing Symmetric control travel Greater than 55 cm
A
Pitch stability exiting accelerated flight
Dive forward angle on exit Dive forward less than 30° Collapse occurs No
Pitch stability operating controls during accelerated flight
A
Collapse occurs No
A
Roll stability and damping
Oscillations Reducing
A
Stability in gentle spirals
Tendency to return to straight flight Spontaneous exit
Behaviour in a steeply banked turn
A
Sink rate after two turns 12 m/s to 14 m/s
Symmetric front collapse
A Entry Rocking back less than 45° Recovery Spontaneous in less than 3 s Dive forward angle on exit Dive forward 0° to 30° Change of course Keeping course Cascade occurs No
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Less than 25 km/h
A Increasing Greater than 60 cm
A Dive forward less than 30° No
A No
A Reducing
A Spontaneous exit
A 12 m/s to 14 m/s
A Rocking back less than 45° Spontaneous in less than 3 s Dive forward 0° to 30° Keeping course No
DHV Testreport EN926-2:2005 :: SWING Arcus 6.22
B
Symmetric front collapse in accelerated flight
Entry Rocking back less than 45° Recovery Spontaneous in 3 s to 5 s Dive forward angle on exit Dive forward 0° to 30° Change of course Keeping course Cascade occurs No
A
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
A
High angle of attack recovery
Recovery Spontaneous in less than 3 s Cascade occurs No
B
Recovery from a developed full stall
Dive forward angle on exit Dive forward 30° to 60° Collapse No collapse Cascade occurs (other than collapses) No Rocking back Less than 45° Line tension Most lines tight
A
Asymmetric collapse 45-50%
Change of course until re-inflation Less than 90° Maximum dive forward or roll angle Dive or roll angle 15° to 45°
B Rocking back less than 45° Spontaneous in 3 s to 5 s Dive forward 0° to 30° Keeping course No
A Yes Spontaneous in less than 3 s Dive forward 0° to 30° Changing course less than 45° No
A Spontaneous in less than 3 s No
B Dive forward 30° to 60° No collapse No Less than 45° Most lines tight
A Less than 90° Dive or roll angle 15° to 45°
Re-inflation behaviour Spontaneous re-inflation
Spontaneous re-inflation
Total change of course Less than 360°
Less than 360°
Collapse on the opposite side occurs No
No
Twist occurs No
No
Cascade occurs No
No
A
Asymmetric collapse 70-75%
Change of course until re-inflation Less than 90° Maximum dive forward or roll angle Dive or roll angle 15° to 45°
A Less than 90° Dive or roll angle 15° to 45°
Re-inflation behaviour Spontaneous re-inflation
Spontaneous re-inflation
Total change of course Less than 360°
Less than 360°
Collapse on the opposite side occurs No
No
Twist occurs No
No
Cascade occurs No
No
Asymmetric collapse 45-50% in accelerated flight
A
Change of course until re-inflation Less than 90° Maximum dive forward or roll angle Dive or roll angle 15° to 45°
A Less than 90° Dive or roll angle 15° to 45°
Re-inflation behaviour Spontaneous re-inflation
Spontaneous re-inflation
Total change of course Less than 360°
Less than 360°
Collapse on the opposite side occurs No
No
Twist occurs No
No
Cascade occurs No
No
Asymmetric collapse 70-75% in accelerated flight
B
Change of course until re-inflation 90° to 180° Maximum dive forward or roll angle Dive or roll angle 15° to 45°
B 90° to 180° Dive or roll angle 15° to 45°
Re-inflation behaviour Spontaneous re-inflation
Spontaneous re-inflation
Total change of course Less than 360°
Less than 360°
Collapse on the opposite side occurs No
No
Twist occurs No
No
Cascade occurs No
No
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DHV Testreport EN926-2:2005 :: SWING Arcus 6.22
Directional control with a maintained asymmetric collapse
A
A
Able to keep course Yes
Yes
180° turn away from the collapsed side possible in Yes 10 s
Yes
Amount of control range between turn and stall or More than 50 % of the symmetric control travel More than 50 % of the symmetric control travel spin
A
Trim speed spin tendency
Spin occurs No
A
Low speed spin tendency
Spin occurs No
A
Recovery from a developed spin
Spin rotation angle after release Stops spinning in less than 90° Cascade occurs No
A
B-line stall
Change of course before release Changing 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
A
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°
A
Big ears in accelerated flight
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° Behaviour immediately after releasing the Stable flight accelerator while maintaining big ears
A
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] 14
Alternative means of directional control
A
180° turn achievable in 20 s Yes Stall or spin occurs No
Any other flight procedure and/or configuration described in the user's manual No other flight procedure or configuration described in the user's manual
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A No
A No
A Stops spinning in less than 90° No
A Changing course less than 45° Remains stable with straight span Spontaneous in less than 3 s Dive forward 0° to 30° No
A Dedicated controls Stable flight Spontaneous in less than 3 s Dive forward 0° to 30°
A Dedicated controls Stable flight Spontaneous in less than 3 s Dive forward 0° to 30° Stable flight
A Spontaneous exit Less than 720°, spontaneous recovery 14
Type test reference no DHV GS-01-1822-09. Holder of certification Swing Flugsportgeräte GmbH. Manufacturer Swing Flugsportgeräte GmbH. Classification B.
Manufacturer Swing Flugsportgeräte GmbH. Classification B. Winch towing Yes. Number of seats min / max 1 / 1. Accelerator Yes. Trimmers No. Behaviour at ...
Type test reference no DHV GS-01-1822-09. Holder of certification Swing Flugsportgeräte GmbH. Manufacturer Swing Flugsportgeräte GmbH. Classification 1-2 ...
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