U-Turn BLACKLIGHT S, Руководство пользователя

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Certifi cation U-Turn BLACKLIGHT M
Page 31
80 kg 110 kg
2 2 2 B 0 0 -
Test-criteria 40977 40991
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 B A
A A
A A
Dive forward angle on exit B B
A A
Increasing >65 cm
Increasing
Evaluation
No
Smooth, easy and constant rising
4. Control movement - 4.1.4
Yes
No
Less than 25 km/h Less than 25 km/h
No
Special landing technique required
Speed range using the controls larger than 10km/h Yes
Trim speed more than 30km/h
Max. weight in flight up to 80kg
Max. weight in flight 80 to 100kg > 60cm
-
6. Pitch stability operating controls during accelerated flight - 4.1.6
Spontaneous exit
Max. weight in flight greater than 100kg A
No
30° - 60° Keeping course
No
7. Roll stability and damping - 4.1.7
Reducing
12m/s to 14m/s More than 14m/s
B
Sink rate after two turns
10. Symmetric front collapse - 4.1.10
Rocking back less than 45°
Spontaneous in less than 3 sec
Rocking back less than 45°
No Collapse occurs
Collapse occurs
Recovery
9. Behaviour in a steeply banked turn - 4.1.9
Oscillations
Tendency to return to straight flight
8. Stability in gentle spirals - 4.1.8
No
A Spontaneous in less than 3 sec
Spontaneous exit
No
No
Keeping course
No
Reducing
Rocking back less than 45° Rocking back less than 45°
B Spontaneous in 3 to 5 sec
Keeping course
a
cce
le
ra
te
d
tr
im
sp
e
e
d
30° - 60°
Cascade occurs
30° - 60°
Recovery
Spontaneous in 3 to 5 sec
Entry
Keeping course
No
11. Exiting deep stall (parachutal stall) - 4.1.11
Entry
Cascade occurs
A
0° - 30°
-
Academy Test Equipment Academy-Equipment
-
- A
3. Speeds in straight flight - 4.1.3
Dive forward less than 30° Dive forward less than 30°
5. Pitch stability exiting accelerated flight - 4.1.5
Dive forward angle on exit
A
No
A Yes
Yes
A
Classification
Smooth, easy and constant rising Rising behavior
A
1. Inflation / take-off - 4.1.1
B
Evaluation
Manufacturer
Model
Date of testing
Minimum take off weight
09.03.12
Type testing No.
Location
Bad Grönenbach: Blacklight M
Pilot's take off weight
Testpilot
Harness
Mike Küng Tschofen Johannes
23.03.12
EAPR-GS-7547/12
Ac Schruns
16.04.12
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