CS 25.405 Secondary control system
ED Decision 2007/010/R
Secondary controls, such as wheel brake, spoiler, and tab controls, must be designed for the maximum forces that a pilot is likely to apply to those controls. The following values may be used:
PILOT CONTROL FORCE LIMITS (SECONDARY CONTROLS).
|
Control |
Limit pilot
forces |
|
Miscellaneous: *Crank, wheel, or lever. |
but not less than 222 N (50 lbf) nor more than 667 N (150 lbf) (R = radius in mm). (Applicable to any angle within 20o of plane of control). |
|
Twist |
15 Nm (133 in.lbf) |
|
Push-pull |
To be chosen by applicant. |
*Limited to flap, tab, stabiliser, spoiler, and landing gear operation controls.
[Amdt. 25/3]