For AB Engineering/training/experienced and knowledgeable people
1. What is the maximum rudder deflection (degrees) available for low speed op's (such as asymmetrics)?
2. What is the limited (NORMAL law) maximum rudder deflection (degrees) available at high altitudes at normal cruise type speeds?
3. Is pedal deflection (when rudder limiter is operational, NORMAL law) designed to be the same foot feel (travel in inches/centimetres) across the entire speed envelope?
4. Is pedal deflection (when rudder limit is 10 degrees, ALTN or DIRECT law) the same foot feel (travel in inches/centimetres) as NORMAL law?
The questions are asked without implication or speculation, rather to understand IF degraded control protections might have an impact on high altitude, high speed upset recovery control inputs verses control surface outputs.
Thankyou