Manufacturer Swing Flugsportgeräte GmbH. Classification B. Winch towing Yes. Number of seats min / max 1 / 1. Accelerator Yes. Trimmers No. Behaviour at ...
SWING Arcus 6.24 Type designation SWING Arcus 6.24 Type test reference no DHV GS-01-1823-09 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 (72kg)
Behaviour at max weight in flight (90kg)
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
http://www.dhv.de/DHVonlineDB/source/technictestreport2en.php?item=-1100&lang=en (1 sur 3)06/03/2009 07:29:40
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 6.24
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 30° to 60° 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
A
Recovery from a developed full stall
Dive forward angle on exit Dive forward 0° to 30° 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°
A Rocking back less than 45° Spontaneous in less than 3 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
A Dive forward 0° to 30° 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
http://www.dhv.de/DHVonlineDB/source/technictestreport2en.php?item=-1100&lang=en (2 sur 3)06/03/2009 07:29:40
DHV Testreport EN926-2:2005 :: SWING Arcus 6.24
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
http://www.dhv.de/DHVonlineDB/source/technictestreport2en.php?item=-1100&lang=en (3 sur 3)06/03/2009 07:29:40
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.
Type test reference no DHV GS-01-1822-09. Holder of certification Swing Flugsportgeräte GmbH. Manufacturer Swing Flugsportgeräte GmbH. Classification B.
Type test reference no DHV GS-01-1822-09. Holder of certification Swing Flugsportgeräte GmbH. Manufacturer Swing Flugsportgeräte GmbH. Classification 1-2 ...
However we like to mention that we don`t take any liability for possi- ... many happy landings with your U-Turn OBSESSION 2. The Research and Development team at U-Turn can proudly look back at many success- ful years in the ...... descent because a
Feb 9, 2009 - 10. the glider is opened in free fall - this is not a parachute. .... There is further information and a list of the approved propulsion systems ..... If you do not have an email address, enter [email protected] as the email address in the.
However we like to mention that we don`t take any liability for possi- ... many happy landings with your U-Turn OBSESSION 2. The Research and Development team at U-Turn can proudly look back at many success- ful years in the ...... descent because a
same passion for flight as the pilots who choose to fly NOVA wings. This passion and our ..... test distance over a given height. With headwind or a sinking ...
Dein Gleitschirm ist für den Flug mit einem Motor geeignet. Bitte prü- .... services. To claim or use these services, you must register your wing at our myNOVA ..... ces and must have insurance as is required by their country of origin. ... ans you
Not a gram of unnecessary weight combined with the highest pos- sible technical .... Launches and ground handling on a training hill will also help to familiarise ...
Technora lines guarantees the best mechanical strength properties with minimal drag. ..... Empty the glider from all debris such as leaves, twigs, grass, sand etc.
Ulrich Loos. Twentyfiftysix by Ulrich Loos download pdf. Technical Manual TM 4-48.01 MCRP 4-11.3N TO 13C7-2-1001 Airdrop of Supplies and Equipment: Rigging Potable. Water and Water Purification Units. Francis Lieber. Legal and Political Hermeneutics,
Ebenso sind die. Bremsleinen zu kontrollieren, dass alles richtig eingeleint und frei ist. ⢠Die Sichtkontrolle muss genau dem Leinenübersichtsplan entsprechen.
Nov 11, 2013 - Der Gleitschirm darf nur mit einer für das Fluggebiet gültigen Pilotenlizenz ... 12 / 38. 3. Technische Beschreibung. Der Boomerang 9 ist ein ...
SWING XL·XXL ... SWING XL 80 · XXL 90 · 100% Design yourself .... formula : Price of sofa in the main fabric group , for each coordinated stripe we will add to ...
Mar 15, 2011 - Zitate in Fachartikeln), unabhängig davon, auf welche Art und ..... 10 SWING IM WORLD WIDE WEB . ..... Kapitel 4. 17. Anpassen der Bremsgriffe. Der Stratus 8 ist mit einem Swing Multigrip .... (ab circa 6 m/s) muss der Gleitschirm ...
Jan 31, 2018 - particularly tricky problem-let us say. the question of how many ..... Before we try to assess these, let us see what industrialisation artuilly meant to the ...... of good Spanish red wine and 140 gallons of water are put on board.
carabiner was used the way it was designed for, they ordered a detailed material .... safety features (with different manual actuations) til opening the lock, or.
Sep 5, 2017 - Attaching the towline release system . ..... glider. 3. Inspection Information (PDF/Download): ..... The Maintenance and Service book has a.