Eden 2-23

Manufacturer: MAC Para Technology ltd

Declaration of conformity issued to: Plasser Andrea
DHV Test Reference Number  DHV GS-01-0915-01
Classification / Harness group  1 -- 2 / GH
Number of seats  1
Trimming system  Accelerator
Winch towing  Yes

Behaviour at min. take off weight (62 kgs) Behaviour at max. take off weight (80 kgs)
TAKE-OFF  1 -- 2  1 -- 2
Inflation  evenly, immediately  evenly, immediately
Rising behaviour  immediately comes over pilot  immediately comes over pilot
Lift off speed  average  average
Take-off behaviour overall  easy  easy
LEVEL FLIGHT  1 -- 2  1 -- 2
Trim speed   36 km/h   37 km/h
Speed accelerated     48 km/h
Roll damping  average  average
TURN BEHAVIOUR  1 -- 2  1 -- 2
Spin tendency  slight  slight
Control travel  average  average
Agility  average  average
SYMMETRIC STALL  1 -- 2  1 -- 2
Deep stall limit  average 60 cm - 75 cm  average 60 cm - 75 cm
Full stall limit  average 65 cm - 80 cm  average 65 cm - 80 cm
Control pressure increase  average  average
SYMMETRIC TUCK  1 -- 2  1 -- 2
Tendency to shoot forward  slight  slight
Opening behaviour  spontaneous, delayed  spontaneous, delayed
SYMMETRIC TUCK (ACCELERATED)  -  1 -- 2
Tendency to shoot forward  -  average
Opening behaviour  -  spontaneous, delayed
ASYMMETRIC TUCK  1 -- 2  1 -- 2
Turn  90 - 180 degrees  90 - 180 degrees
Rate of turn  average  average
Loss of altitude  average  average
Stabilization  spontaneous  spontaneous
Opening behaviour  spontaneous, impulsive  spontaneous, impulsive
ASYMMETRIC TUCK (ACCELERATED)  -  1 -- 2
Turn  -  90 - 180 degrees
Rate of turn  -  average
Loss of altitude  -  average
Stabilization  -  spontaneous
Opening behaviour  -  spontaneous, delayed
COUNTERSTEERING AN ASYMMETRIC TUCK  1 -- 2  1 -- 2
Stabilization  countersteering easy  countersteering easy
Control travel  average  average
Control pressure increase  average  average
Opposite turn  easy, no tendency to stall  easy, no tendency to stall
Opening behaviour  spontaneous, delayed  spontaneous, delayed
FULLSTALL (symmetric exit)  1 -- 2  1 -- 2
FULLSTALL (asymmetric exit)  1 -- 2  1 -- 2
SPIN AT TRIM SPEED  1 -- 2  1 -- 2
SPIN IN STATIONARY TURN  1 -- 2  1 -- 2
SPIRAL DIVE  1 -- 2  1 -- 2
Entry  easy  easy
Spin tendency  slight  slight
Exit  spontaneous  spontaneous
B LINE STALL  1 -- 2  1 -- 2
Entry  easy  easy
Exit  delayed acceleration < 4 sec  delayed acceleration < 4 sec
LANDING  1 -- 2  1 -- 2
Landing behaviour  easy  easy
ADDITIONAL FLIGHT SAFETY REMARKS