In the case of the A380, the maximum bank angle permitted is 67 degrees, and it is 33 degrees in normal flight operation. To roll the aircraft, this system would have to be overridden.
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Maximum and minimum glideslope angles are 3.25 degrees and 2.5 degrees respectively.
For Part 91 General Aviation operations the required flight crew must use supplemental oxygen for any portion of the flight that exceeds 30 minutes above a cabin pressure altitude of 12,500 feet mean sea level (MSL) up to and including 14,000 feet (MSL).