[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2003]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR23.66]

[Page 183]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
 
PART 23--AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES--Table of Contents
 
                            Subpart B--Flight
 
Sec. 23.66  Takeoff climb: One-engine inoperative.

    For normal, utility, and acrobatic category reciprocating engine-
powered airplanes of more than 6,000 pounds maximum weight, and turbine 
engine-powered airplanes in the normal, utility, and acrobatic category, 
the steady gradient of climb or descent must be determined at each 
weight, altitude, and ambient temperature within the operational limits 
established by the applicant with--
    (a) The critical engine inoperative and its propeller in the 
position it rapidly and automatically assumes;
    (b) The remaining engine(s) at takeoff power;
    (c) The landing gear extended, except that if the landing gear can 
be retracted in not more than seven seconds, the test may be conducted 
with the gear retracted;
    (d) The wing flaps in the takeoff position(s):
    (e) The wings level; and
    (f) A climb speed equal to that achieved at 50 feet in the 
demonstration of Sec. 23.53.

[Doc. No. 27807, 61 FR 5186, Feb. 9, 1996]