297
Federal Aviation Administration, DOT
Pt. 121, App. L
b. Each turbopropeller powered airplane
subject to this appendix must be dem-
onstrated to comply with the airplane per-
formance operating limitation requirements
of this chapter specified as follows:
i. Section 23.45 Performance General.
ii. Section 23.51 Takeoff.
iii. Section 23.53 Takeoff speeds.
iv. Section 23.55 Accelerate stop distance.
v. Section 23.57 Takeoff path.
vi. Section 23.59 Takeoff distance and take-
off run.
vii. Section 23.61 Takeoff flight path.
viii. Section 23.65 Climb: All engines oper-
ating.
ix. Section 23.67 Climb: one engine inoper-
ative.
x. Section 23.75 Landing.
xi. Section 23.77 Balked landing.
xii. Sections 23.1581 through 23.1589 Air-
plane flight manual and approved manual
material.
6.
Operation.
After compliance with the
final airplane performance operating limita-
tions requirements has been demonstrated
and added to the Airplane Flight Manual
performance data of the affected airplane,
that airplane must be operated in accordance
with the performance limitations of §§ 121.189
through 121.197.
[Doc. No. 28154, 60 FR 65936, Dec. 20, 1995, as
amended by Doc. No. OST–2002–13435]
A
PPENDIX
L
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tained in superseded type certification regu-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cable aircraft, superseded type certification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 Copies of all superseded regula-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.
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