DHV Test report LTF 2003

MAC Para Magus XC 21 Type designation MAC Para Magus XC 21 Type test reference no DHV GS-01-1752-08 Holder of certification MAC Para Technology ltd Manufacturer MAC Para Technology ltd Classification 2-3 GH Winch towing Yes Number of seats min / max 1 / 1 Accelerator Yes Trimmers No   Behaviour at min weight in flight (70kg) Behaviour at max weight in flight (85kg) Take off 2 2 Inflation unevenly, delayed evenly, immediately Rising behaviour comes over pilot delayed comes over pilot delayed Take off speed average average Take off handling average average   Straight flight 2 2 Roll damping average average   Turn handling 2 2 Spin tendency average average Control travel slight average Agility average average   Symmetric stall 2-3 2-3 Deep-stall limit early < 60 cm early < 60 cm Full stall limit early < 65 cm early < 65 cm Increase in steering power average slight   Front collapse 2-3 2 Pre-acceleration average slight Opening behaviour not spontaneously spontaneous, delayed with pumping   Asymmetric collapse 2-3 2-3 Turn tendency 180 - 360 degrees 180 - 360 degrees Change of course 180 - 360 degrees 180 - 360 degrees Rate of turn high high Max. roll/pitch angle greater than 45 degrees greater than 45 degrees Loss of altitude high high Stabilization spontaneous spontaneous Opening behaviour spontaneous, delayed spontaneous   Countersteering an asymmetric collapse 2 2-3 Stabilization countersteering easy countersteering demanding Control travel slight slight Control pressure increase average slight Turn in opposite direction easy, no tendency to stall demanding, tendency to stall Opening behaviour spontaneous, delayed spontaneous, delayed   Full stall, symm. exit 2-3 2 Spin out of straight flight 2 2 Spin out of turn 2-3 2 Spiral dive 2 2 Entry average average Spin tendency average average Exit turn continues through < 180 degrees turn continues through 180 - 360 degrees Sink rate after 720 °[m/s] 10 13   B-line stall 2-3 2 Entry demanding demanding Exit spontaneous spontaneous   Big ears 2 1-2 Entry easy easy Recovery not spontaneously spontaneous, quickly   Landing 2 2 Landing behaviour average average   Front collapse (accelerated) 2-3 2-3 Pre-acceleration slight slight Opening behaviour not spontaneously spontaneous, delayed   with pumping   Asymmetric collapse (accelerated) 2-3 2-3 Turn tendency 180 - 360 degrees 180 - 360 degrees Change of course 180 - 360 degrees 180 - 360 degrees Rate of turn high high Max. roll/pitch angle greater than 45 degrees greater than 45 degrees Loss of altitude high high Stabilization spontaneous spontaneous Opening behaviour spontaneous, delayed spontaneous   Big ears accelerated 2 1-2 Entry easy easy Recovery not spontaneously spontaneous, quickly   Supplementary remarks       Asymetric collapse and asymetric collapse (accelerated): tendency for reactionary collapse on opposing canopy side with flight path directional change and difficult recovery. B-Stall: Unstabil mit Neigung zu Frontrosette und Verhängertendenz

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