[Code of Federal Regulations]

[Title 14, Volume 1]

[Revised as of January 1, 2006]

From the U.S. Government Printing Office via GPO Access

[CITE: 14CFR29.62]



[Page 654]

 

                     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 Sec. Sec. 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 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]