[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: 14CFR21.27]



[Page 125-126]

 

                     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 B_Type Certificates

 

Sec. 21.27  Issue of type certificate: surplus aircraft of the Armed 

Forces.



    (a) Except as provided in paragraph (b) of this section an applicant 

is entitled to a type certificate for an aircraft in the normal, 

utility, acrobatic, commuter, or transport category that was designed 

and constructed in the United States, accepted for operational use, and 

declared surplus by, an Armed Force of the United States, and that is 

shown to comply with the applicable certification requirements in 

paragraph (f) of this section.

    (b) An applicant is entitled to a type certificate for a surplus 

aircraft of the Armed Forces of the United States that is a counterpart 

of a previously type certificated civil aircraft, if he shows compliance 

with the regulations governing the original civil aircraft type 

certificate.

    (c) Aircraft engines, propellers, and their related accessories 

installed in surplus Armed Forces aircraft, for which a type certificate 

is sought under this section, will be approved for use on those aircraft 

if the applicant shows that on the basis of the previous military 

qualifications, acceptance, and service record, the product provides 

substantially the same level of airworthiness as would be provided if 

the engines or propellers were type certificated under Part 33 or 35 of 

the Federal Aviation Regulations.

    (d) The Administrator may relieve an applicant from strict 

compliance with a specific provision of the applicable requirements in 

paragraph (f) of this section, if the Administrator finds that the 

method of compliance proposed by the applicant provides substantially 

the same level of airworthiness and that strict compliance with those 

regulations would impose a severe burden on the applicant. The 

Administrator may use experience that was satisfactory to an Armed Force 

of the United States in making such a determination.

    (e) The Administrator may require an applicant to comply with 

special conditions and later requirements than those in paragraphs (c) 

and (f) of this section, if the Administrator finds that compliance with 

the listed regulations would not ensure an adequate level of 

airworthiness for the aircraft.

    (f) Except as provided in paragraphs (b) through (e) of this 

section, an applicant for a type certificate under this section must 

comply with the appropriate regulations listed in the following table:



------------------------------------------------------------------------

                                 Date accepted for

                                  operational use

        Type of aircraft            by the Armed      Regulations that

                                   Forces  of the         apply \1\

                                   United States

------------------------------------------------------------------------

Small reciprocating-engine       Before May 16,     CAR Part 3, as

 powered airplanes.               1956.              effective May 15,

                                 After May 15,       1956.

                                  1956.             CAR Part 3, or FAR

                                                     Part 23.

Small turbine engine-powered     Before Oct. 2,     CAR Part 3, as

 airplanes.                       1959.              effective Oct. 1,

                                 After Oct. 1,       1959.

                                  1959.             CAR Part 3 or FAR

                                                     Part 23.

Commuter category airplanes....  After (Feb. 17,

                                  1987).

                                 FAR Part 23 as of

                                  (Feb. 17, 1987)..

Large reciprocating-engine       Before Aug. 26,    CAR Part 4b, as

 powered airplanes.               1955.              effective Aug. 25,

                                 After Aug. 25,      1955.

                                  1955.             CAR Part 4b or FAR

                                                     Part 25.

Large turbine engine-powered     Before Oct. 2,     CAR Part 4b, as

 airplanes.                       1959.              effective Oct. 1,

                                 After Oct. 1,       1959.

                                  1959.             CAR Part 4b or FAR

                                                     Part 25.

Rotorcraft with maximum

 certificated takeoff weight

 of:

  6,000 pounds or less.........  Before Oct. 2,     CAR Part 6, as

                                  1959.              effective Oct. 1,

                                 After Oct. 1,       1959.

                                  1959.             CAR Part 6, or FAR

                                                     Part 27.

  Over 6,000 pounds............  Before Oct. 2,     CAR Part 7, as

                                  1959.              effective Oct. 1,

                                 After Oct. 1,       1959.

                                  1959.             CAR Part 7, or FAR

                                                     Part 29.\1\ Where

                                                     no specific date is

                                                     listed, the

                                                     applicable

                                                     regulations are

                                                     those in effect on

                                                     the date that the

                                                     first aircraft of

                                                     the particular

                                                     model was accepted

                                                     for operational use

                                                     by the Armed

                                                     Forces.

------------------------------------------------------------------------





[[Page 126]]





[Doc. No. 5085, 29 FR 14564, Oct. 24, 1964, as amended by Amdt. 21-59, 

52 FR 1835, Jan. 15, 1987; 52 FR 7262, Mar. 9, 1987; 70 FR 2325, Jan. 

13, 2005]