[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: 14CFR21.5]



[Page 121-122]

 

                     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



[[Page 122]]



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]