[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: 14CFR21.5]

[Page 117]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
 
PART 21--CERTIFICATION PROCEDURES FOR PRODUCTS AND PARTS--Table of Contents
 
                           Subpart A--General
 
Sec. 21.5  Airplane or Rotorcraft Flight Manual.

    (a) With each airplane or rotorcraft that was not type certificated 
with an Airplane or Rotorcraft Flight Manual and that has had no flight 
time prior to March 1, 1979, the holder of a Type Certificate (including 
a Supplemental Type Certificate) or the licensee of a Type Certificate 
shall make available to the owner at the time of delivery of the 
aircraft a current approved Airplane or Rotorcraft Flight Manual.
    (b) The Airplane or Rotorcraft Flight Manual required by paragraph 
(a) of this section must contain the following information:
    (1) The operating limitations and information required to be 
furnished in an Airplane or Rotorcraft Flight Manual or in manual 
material, markings, and placards, by the applicable regulations under 
which the airplane or rotorcraft was type certificated.
    (2) The maximum ambient atmospheric temperature for which engine 
cooling was demonstrated must be stated in the performance information 
section of the Flight Manual, if the applicable regulations under which 
the aircraft was type certificated do not require ambient temperature on 
engine cooling operating limitations in the Flight Manual.

[Amdt. 21-46, 43 FR 2316, Jan. 16, 1978]

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