Deutscher Hängegleiterverband e.V. im DAeC
DHV/OeAeC-Technikreferat
LBA-anerkannte Prüfstelle für Hängegleiter und Gleitsegel
Beauftragter der österreichischen Luftfahrtbehörde
GS Testflug DHV03 Airwave Magic 4 M  
Test No 015944-GSTF03-729-Claude
Test date 21.12.2005
Type Airwave Magic 4 M
Test type GS Testflug DHV03
Order Auftrag GS Musterprüfung Airwave Magic 4 M (Airwave Villinger Ges.m.b.H.)
Customer Airwave Villinger Ges.m.b.H.
Test standard Lufttüchtigkeitsforderungen für HG und GS
Expert Thurnheer
Result positive
Billing to: 100%
Technical peculiarities
 
 
Datum / Unterschrift (Thurnheer)
DHV test flight main data 
Harness type Advance Hi-Comp
Take off weight [kg] 105
Weight limit for certification [kg] 105
Number of pilots 1
Trim speed [km/h] 38
Accelerated speed [km/h] 53
Classification 2-3
Supplementary remarks 

 
PG test flight specific 
Harness category  GH 
Accelerator used?  Yes 
Trimms 
DHV PG Test flight 2003 data 
Take off 
Take off class. 
Inflation evenly, immediately
Rising behaviour overshoots, symmetric action on the controls necessary
Take off speed average
Take off handling average
Straight flight 
Straight flight class. 2
Speed range high
Roll damping average
Pitch damping slight
Yaw stability average
Turn handling 
Turn handling class. 2
Spin tendency average
Control travel average
Agility average
Control pressure increase high
Control without brakes control through rear risers possible
Symmetric stall 
Deep-stall limit 2-3
Deep-stall limit early < 60 cm
Full stall limit early < 65 cm
Full stall with full steering way yes, soft stall
Falling back average
Increase in steering power high
Front collapse 
Front collapse class. 2
Effort average
Pre-acceleration average
Opening behaviour spontaneous, delayed
Front collapse (accelerated) 
Front collapse accelerated class. 2-3
Effort average
Pre-acceleration average
Opening behaviour spontaneous, delayed
 
Asymmetric collapse 
Asymmetric collapse class. 2-3
Turn tendency 90 - 180 degrees
Change of course 90 - 180 degrees
Rate of turn high
  with deceleration
Max. roll/pitch angle greater than 45 degrees
Loss of altitude average
Stabilization spontaneous
Opening behaviour spontaneous, delayed
 
Asymmetric collapse (accelerated) 
Asymmetric collapse acc. class. 2-3
Turn tendency 90 - 180 degrees
Change of course 90 - 180 degrees
Rate of turn high
  with deceleration
Max. roll/pitch angle greater than 45 degrees
Loss of altitude average
Stabilization spontaneous
Opening behaviour spontaneous, delayed
 
Countersteering an asymmetric collapse 
Countersteering an asymmetric collapse class. 2
Stabilization countersteering easy
Control travel average
Control pressure increase high
Turn in opposite direction easy, no tendency to stall
Opening behaviour spontaneous, delayed
 
Full stall, symm. exit 
Fullstall, symm. exit class 2
Behaviour nervous
-
Reaction average shoot forward
no collapse
Turn tendency no turn
Rate of turn
Loss of altitude
Stabilization
Opening behaviour
Spin out of straight flight 
Spin out of straight flight class. 2
Rate of turn average
Exit turn continues through < 90 degrees
Reaction average shoot forward to one side
  no collapse
Turn tendency no turn
Rate of turn
 
Loss of altitude
Stabilization
Opening behaviour
 
Spin out of turn 
Spin out of turn class. 2
Reaction average shoot forward to one side
no collapse
Turn tendency no turn
Rate of turn
Loss of altitude
Stabilization
Opening behaviour
Spiral dive 
Spiral dive class. 2
Entry average
Spin tendency average
Exit turn continues through 180 - 360 degrees
Sink rate after 720 °[m/s] 12
B-line stall 
B-line stall class. 2-3
Entry demanding
Exit spontaneous
Big ears 
Big ears 2
Entry easy
Recovery not spontaneously
Big ears accelerated 
Big ears acc. class. 2
Entry easy
Recovery not spontaneously
Landing 
Landing class. 2
Point of flare average
Landing speed average
Landing behaviour average
02.03.2006 12:20:26