Certifi cation U-Turn BLACKLIGHT L
Page 34
100
kg
125
kg
2
2
2
B
0
0
-
Test-criteria
41046
41056
Special take off technique required
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
B
A
A
Dive forward angle on exit
A
A
A
A
A
A
Dive forward angle on exit
A
B
A
A
Dive forward less than 30°
Dive forward less than 30°
5. Pitch stability exiting accelerated flight - 4.1.5
Increasing
Increasing
>65 cm
>65 cm
Max. weight in flight greater than 100kg
No
Less than 25 km/h
4. Control movement - 4.1.4
A
Special landing technique required
Yes
Yes
Trim speed more than 30km/h
3. Speeds in straight flight - 4.1.3
Yes
Max. weight in flight 80 to 100kg
30° - 60°
Keeping course
A
6. Pitch stability operating controls during accelerated flight - 4.1.6
Spontaneous exit
Sink rate after two turns
10. Symmetric front collapse - 4.1.10
No
No
Collapse occurs
Collapse occurs
Recovery
9. Behaviour in a steeply banked turn - 4.1.9
No
A
More than 14m/s
Oscillations
Tendency to return to straight flight
8. Stability in gentle spirals - 4.1.8
A
Spontaneous in less than 3 sec
Rocking back less than 45°
Spontaneous in less than 3 sec
Spontaneous in less than 3 sec
Spontaneous in less than 3 sec
No
Reducing
No
Rocking back less than 45°
Spontaneous exit
No
7. Roll stability and damping - 4.1.7
Reducing
12m/s to 14m/s
0° - 30°
Rocking back less than 45°
A
No
tr
im
sp
e
e
d
0° - 30°
Cascade occurs
0° - 30°
Recovery
Keeping course
a
cce
le
ra
te
d
Entry
Rocking back less than 45°
No
Entry
Cascade occurs
11. Exiting deep stall (parachutal stall) - 4.1.11
A
Keeping course
No
Keeping course
EAPR Testequipment
Academy Test Equipment
-
-
-
Less than 25 km/h
No
Evaluation
Dive forward angle on exit
A
No
A
Yes
-
Max. weight in flight up to 80kg
Speed range using the controls larger than 10km/h
A
Classification
Smooth, easy and constant rising
Rising behavior
Smooth, easy and constant rising
A
1. Inflation / take-off - 4.1.1
B
Evaluation
Manufacturer
Model
Date of testing
Minimum take off weight
17.05.12
Type testing No.
Location
Bad Grönenbach:
Blacklight L
Pilot's take off weight
Testpilot
Harness
Tschofen Johannes
Anselm Rauh
26.05.12
EAPR-GS-7564/12
Schruns
28.05.12
EAPR e.V - Marktstr. 11 - D-87730 Bad Grönenbach - Germany
Maximum take off weight
2. Landing - 4.1.2
Minimum speed
Flight Test-Report
Stand - 08.04.2010 Seite 1
Содержание BLACKLIGHT S
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Страница 29: ...Certification U Turn BLACKLIGHT S Page 25...
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