[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2004]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR29.62]

[Page 645-646]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
 
PART 29--AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT--Table of Contents
 
                            Subpart B--Flight
 
Sec. 29.62  Rejected takeoff: Category A.

    The rejected takeoff distance and procedures for each condition 
where takeoff is approved will be established with--
    (a) The takeoff path requirements of Secs. 29.59 and 29.60 being 
used up to the TDP where the critical engine failure is recognized and 
the rotorcraft is landed and brought to a complete stop on the takeoff 
surface;
    (b) The remaining engines operating within approved limits;
    (c) The landing gear remaining extended throughout the entire 
rejected takeoff; and
    (d) The use of only the primary controls until the rotorcraft is on 
the ground. Secondary controls located on the primary control may not be 
used until the rotorcraft is on the ground. Means other than wheel 
brakes may be used to stop the rotorcraft if the means

[[Page 646]]

are safe and reliable and consistent results can be expected under 
normal operating conditions.

[Doc. No. 24802, 61 FR 21899, May 10, 1996, as amended by Amdt. 29-44, 
64 FR 45337, Aug. 19, 1999]