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297 

Federal Aviation Administration, DOT 

Pt. 121, App. L 

A

PPENDIX

TO

P

ART

121—T

YPE

C

ER

-

TIFICATION

R

EGULATIONS

M

ADE

P

RE

-

VIOUSLY

E

FFECTIVE

 

Appendix L lists regulations in this part 

that require compliance with standards con-
tained in superseded type certification regu-
lations that continue to apply to certain 
transport category airplanes. The tables set 
out citations to current CFR section, appli-

cable aircraft, superseded type certification 
regulation and applicable time periods, and 
the CFR edition and F

EDERAL

R

EGISTER

doc-

uments where the regulation having prior ef-
fect is found. Copies of all superseded regula-
tions may be obtained at the Federal Avia-
tion Administration Law Library, Room 924, 
800 Independence Avenue SW., Washington, 
DC. 

Part 121 section 

Applicable aircraft 

Provisions: CFR/FR references 

§ 121.312(a)(1)(i) ............

Transport category; or nontransport category 

type certificated before January 1, 1965; pas-
senger capacity of 20 or more; manufactured 
prior to August 20, 1990.

Heat release rate testing. 14 CFR 25.853(d) in 

effect March 6, 1995: 14 CFR parts 1 to 59, 
Revised as of January 1, 1995, and amended 
by Amdt. 25–83, 60 FR 6623, February 2, 
1995. 

Formerly 14 CFR 25.853(a–1) in effect August 

20, 1986: 14 CFR parts 1 to 59, Revised as of 
January 1, 1986. 

§ 121.312(a)(1)(ii) ...........

Transport category; or nontransport category 

type certificated before January 1, 1965; pas-
senger capacity of 20 or more; manufactured 
after August 19, 1990.

Heat release rate and smoke testing. 14 CFR 

25.853(d) in effect March 6, 1995: 14 CFR 
parts 1 to 59, Revised as of January 1, 1995, 
and amended by Amdt. 25–83, 60 FR 6623, 
February 2, 1995. 

Formerly 14 CFR 25.853(a–1) in effect Sep-

tember 26, 1988: 14 CFR parts 1 to 59, Re-
vised as of January 1, 1988, and amended by 
Amdt. 25–66, 53 FR 32584, August 25, 1988 

§ 121.312(a)(2)(i) ............

Transport category; or nontransport category 

type certificate before January 1, 1965; appli-
cation for type certificate filed prior to May 1, 
1972; substantially complete replacement of 
cabin interior on or after May 1, 1972.

Provisions of 14 CFR 25.853 in effect on April 

30, 1972: 14 CFR parts 1 to 59, Revised as of 
January 1, 1972. 

§ 121.312(a)(3)(i) ............

Transport category type certificated after January 

1, 1958; nontransport category type certificated 
after January 1, 1958, but before January 1, 
1965; passenger capacity of 20 or more; sub-
stantially complete replacement of the cabin in-
terior on or after March 6, 1995.

Heat release rate testing. 14 CFR 25.853(d) in 

effect March 6, 1995: 14 CFR parts 1 to 59, 
Revised as of January 1, 1995; and amended 
by \n25–83, 60 FR 6623, February 2, 1995. 

Formerly 14 CFR 25.853(a–1) in effect August 

20, 1986: 14 CFR parts 1 to 59, Revised as of 
January 1, 1986. 

§ 121.312(a)(3)(ii) ...........

Transport category type certificated after January 

1, 1958; nontransport category type certificated 
after January 1, 1958, but before January 1, 
1965; passenger capacity of 20 or more; sub-
stantially complete replacement of the cabin in-
terior on or after August 20, 1990.

Heat release rate and smoke testing. 14 CFR 

25.853(d) in effect March 6, 1995; 14 CFR 
parts 1 to 59, Revised as of January 1, 1995; 
and amended by \n25–83, 60 FR 6623, Feb-
ruary 2, 1995. 

Formerly 14 CFR § 25.853(a–1) in effect Sep-

tember 26, 1988: CFR, Title 14, Parts 1 to 59, 
Revised as of January 1, 1988, and amended 
by \n25–66, 53 FR 32584, August 25, 1988. 

§ 121.312(b) (1) and (2)

Transport category airplane type certificated after 

January 1, 1958; Nontransport category air-
plane type certificated after December 31, 
1964.

Seat cushions. 14 CFR 25.853(c) effective on 

November 26, 1984: 14 CFR parts 1 to 59, 
Revised as of January 1, 1984, and amended 
by \n25–59, 49 FR 43188, October 26, 1984. 

§ 121.312(c) ....................

Airplane type certificated in accordance with 

SFAR No. 41; maximum certificated takeoff 
weight in excess of 12,500 pounds.

Compartment interior requirements. 14 CFR 

25.853(a) in effect March 6, 1995: 14 CFR 
parts 1 to 59, Revised as of January 1, 1995, 
and amended by \n25–83, 60 FR 6623, Feb-
ruary 2, 1995. 

Formerly 14 CFR 25.853(a), (b–1), (b–2), and 

(b–3) in effect on September 26, 1978: 14 
CFR parts 1 to 59, Revised as of January 1, 
1978. 

§ 121.314(a) ...................

Transport category airplanes type certificated 

after January 1, 1958.

Class C or D cargo or baggage compartment 

definition, 14 CFR 25.857 in effect on June 16, 
1986, 14 CFR parts 1 to 59, Revised 1/1/97, 
and amended by Amendment 25–60, 51 FR 
18243, May 16, 1986. 

[Doc. No. 28154, 60 FR 65936, Dec. 20, 1995, as amended by Amdt. 121–269, 63 FR 8049, Feb. 17, 
1998] 

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