[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: 14CFR27.71]

[Page 564]
 
                     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. 27.71  Glide performance.

    For single-engine helicopters and multiengine helicopters that do 
not meet the Category A engine isolation requirements of Part 29 of this 
chapter, the minimum rate of descent airspeed and the best angle-of-
glide airspeed must be determined in autorotation at--
    (a) Maximum weight; and
    (b) Rotor speed(s) selected by the applicant.

[Amdt. 27-21, 49 FR 44433, Nov. 6, 1984]