§29.62 Rejected take-off: Category A

The rejected take-off distance and procedures for each condition where take-off is approved will be established with: (a) The take-off path requirem ents of CS 29.59 and 29.60 bei ng used up to the TDP where the cri tical engi ne fai lure i s recogni sed, and the rotorcraft l anded and brought t o a stop on the take-off surface; (b) The rem aining engi nes operat ing wi thin approved limits; (c) The landing gear rem aining ext ended throughout the entire rejected take-off; and (d) The use of only the primary controls until the rotorcraft is on the ground. Secondary controls located on the primary cont rol m ay not be used until the rotorcraft is on the ground. Means other than wheel brakes m ay be used to stop the rotorcraft if the m eans are safe and reliable and consistent resul ts can be expected under normal operating conditions.