[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2007]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR27.75]

[Page 576]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
 
PART 27_AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT--Table 
of Contents
 
                            Subpart B_Flight
 
Sec.  27.75  Landing.

    (a) The rotorcraft must be able to be landed with no excessive 
vertical acceleration, no tendency to bounce, nose over, ground loop, 
porpoise, or water loop, and without exceptional piloting skill or 
exceptionally favorable conditions, with--
    (1) Approach or glide speeds appropriate to the type of rotorcraft 
and selected by the applicant;
    (2) The approach and landing made with--
    (i) Power off, for single-engine rotorcraft; and
    (ii) For multiengine rotocraft, one engine inoperative and with each 
operating engine within approved operating limitations; and
    (3) The approach and landing entered from steady autorotation.
    (b) Multiengine rotorcraft must be able to be landed safely after 
complete power failure under normal operating conditions.

[Doc. No. 5074, 29 FR 15695, Nov. 24, 1964, as amended by Amdt. 27-14, 
43 FR 2324, Jan. 16, 1978]