| Control Wheel Deflection | Ailerons | Spoilers | |||||
|---|---|---|---|---|---|---|---|
| 1/2/3 | 4 | 5/6 | 7/8 | 9 | 10/11/12 | ||
0°
|
0° | down | - | down | down | - | down |
10°![]() (2 units trim) |
4° | down | - | down | down | - | down |
15°![]() (3 units trim) |
6.5° | breakout | - | breakout | breakout | - | breakout |
30°![]() (6 units trim) |
13° | 3° | - | 3° | 3° | - | 3° |
55°
|
20° full deflection |
10° | - | 10° | 10° | - | 10° |
85°
|
20° | 44° | - | 44°/30° | 30°/44° | - | 44° |
| full deflection | |||||||
| Ground speedbrakes |
20° | 44° | 55° | 44°/30° | 30°/44° | 55° | 44° |
Note: If the control wheel is deflected to the left,
only the left flight spoilers extend (and vice-versa).
Aircraft Maintenance Manual