[Code of Federal Regulations]
[Title 14, Volume 2]
[Revised as of January 1, 2005]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR121.157]

[Page 430-431]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION 
                               (CONTINUED)
 
PART 121_OPERATING REQUIREMENTS: DOMESTIC, FLAG, AND SUPPLEMENTAL 
OPERATIONS--Table of Contents
 
                     Subpart H_Aircraft Requirements
 
Sec. 121.157  Aircraft certification and equipment requirements.

    (a) Airplanes certificated before July 1, 1942. No certificate 
holder may operate an airplane that was type certificated before July 1, 
1942, unless--
    (1) That airplane meets the requirements of Sec. 121.173(c), or
    (2) That airplane and all other airplanes of the same or related 
type operated by that certificate holder meet the performance 
requirements of sections 4a.737-T through 4a.750-T of the Civil Air 
Regulations as in effect on January 31, 1965; or Sec. Sec. 25.45 
through 25.75 and Sec. 121.173(a), (b), (d), and (e) of this title.
    (b) Airplanes certificated after June 30, 1942. Except as provided 
in paragraphs (c), (d), (e), and (f) of this section, no certificate 
holder may operate an airplane that was type certificated after June 30, 
1942, unless it is certificated as a transport category airplane and 
meets the requirements of Sec. 121.173(a), (b), (d), and (e).
    (c) C-46 type airplanes: passenger-carrying operations. No 
certificate holder may operate a C-46 airplane in passenger-carrying 
operations unless that airplane is operated in accordance with the 
operating limitations for transport category airplanes and meets the 
requirements of paragraph (b) of this section or meets the requirements 
of part 4b, as in effect July 20, 1950, and the requirements of Sec. 
121.173 (a), (b), (d) and (e), except that--
    (1) The requirements of sections 4b.0 through 4b.19 as in effect May 
18, 1954, must be complied with;
    (2) The birdproof windshield requirements of section 4b.352 need not 
be complied with;
    (3) The provisions of sections 4b.480 through 4b.490 (except 
sections 4b.484(a)(1) and 4b.487(e)), as in effect May 16, 1953, must be 
complied with; and

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    (4) The provisions of paragraph 4b.484(a)(1), as in effect July 20, 
1950, must be complied with.

In determining the takeoff path in accordance with section 4b.116 and 
the one-engine inoperative climb in accordance with section 4b.120 (a) 
and (b), the propeller of the inoperative engine may be assumed to be 
feathered if the airplane is equipped with either an approved means for 
automatically indicating when the particular engine has failed or an 
approved means for automatically feathering the propeller of the 
inoperative engine. The Administrator may authorize deviations from 
compliance with the requirements of sections 4b.130 through 4b.190 and 
subparts C, D, E, and F of part 4b (as designated in this paragraph) if 
he finds that (considering the effect of design changes) compliance is 
extremely difficult to accomplish and that service experience with the 
C-46 airplane justifies the deviation.
    (d) C-46 type airplanes: cargo operations. No certificate holder may 
use a nontransport category C-46 type airplane in cargo operations 
unless--
    (1) It is certificated at a maximum gross weight that is not greater 
than 48,000 pounds;
    (2) It meets the requirements of Sec. Sec. 121.199 through 121.205 
using the performance data in appendix C to this part;
    (3) Before each flight, each engine contains at least 25 gallons of 
oil; and
    (4) After December 31, 1964--
    (i) It is powered by a type and model engine as set forth in 
appendix C of this part, when certificated at a maximum gross takeoff 
weight greater than 45,000 pounds; and
    (ii) It complies with the special airworthiness requirement set 
forth in Sec. Sec. 121.213 through 121.287 of this part or in appendix 
C of this part.
    (e) Commuter category airplanes. Except as provided in paragraph (f) 
of this section, no certificate holder may operate under this part a 
nontransport category airplane type certificated after December 31, 
1964, and before March 30, 1995, unless it meets the applicable 
requirements of Sec. 121.173 (a), (b), (d), and (e), and was type 
certificated in the commuter category.
    (f) Other nontransport category airplanes. No certificate holder may 
operate under this part a nontransport category airplane type 
certificated after December 31, 1964, unless it meets the applicable 
requirements of Sec. 121.173 (a), (b), (d), and (e), was manufactured 
before March 20, 1997, and meets one of the following:
    (1) Until December 20, 2010:
    (i) The airplane was type certificated in the normal category before 
July 1, 1970, and meets special conditions issued by the Administrator 
for airplanes intended for use in operations under part 135 of this 
chapter.
    (ii) The airplane was type certificated in the normal category 
before July 19, 1970, and meets the additional airworthiness standards 
in SFAR No. 23, 14 CFR part 23.
    (iii) The airplane was type certificated in the normal category and 
meets the additional airworthiness standards in appendix A of part 135 
of this chapter.
    (iv) The airplane was type certificated in the normal category and 
complies with either section 1.(a) or 1.(b) of SFAR No. 41 of 14 CFR 
part 21.
    (2) The airplane was type certificated in the normal category, meets 
the additional requirements described in paragraphs (f)(1)(i) through 
(f)(1)(iv) of this section, and meets the performance requirements in 
appendix K of this part.
    (g) Certain newly manufactured airplanes. No certificate holder may 
operate an airplane under this part that was type certificated as 
described in paragraphs (f)(1)(i) through (f)(1)(iv) of this section and 
that was manufactured after March 20, 1997, unless it meets the 
performance requirements in appendix K of this part.
    (h) Newly type certificated airplanes. No person may operate under 
this part an airplane for which the application for a type certificate 
is submitted after March 29, 1995, unless the airplane is type 
certificated under part 25 of this chapter.

[Doc. No. 6258, 29 FR 19197, Dec. 31, 1964, as amended by Amdt. 121-251, 
60 FR 65927, Dec. 20, 1995; Amdt. 121-256, 61 FR 30434, June 14, 1996]

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