Federal Aviation Administration, DOT

Pt. 121, App. L

b. Each turbopropeller powered airplane
subject to this appendix must be demonstrated to comply with the airplane performance 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 takeoff run.
vii. Section 23.61 Takeoff flight path.
viii. Section 23.65 Climb: All engines operating.
ix. Section 23.67 Climb: one engine inoperative.
x. Section 23.75 Landing.
xi. Section 23.77 Balked landing.
xii. Sections 23.1581 through 23.1589 Airplane flight manual and approved manual
material.
6. Operation. After compliance with the
final airplane performance operating limitations 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 SectionSection 121.189
through 121.197.
[Doc. No. 28154, 60 FR 65936, Dec. 20, 1995, as
amended by Doc. No. OST-2002-13435]

APPENDIX L TO PART 121 - TYPE CERTIFICATION REGULATIONS MADE PREVIOUSLY EFFECTIVE
Appendix L lists regulations in this part
that require compliance with standards contained in superseded type certification regulations that continue to apply to certain
transport category airplanes. The tables set
out citations to current CFR section, applicable aircraft, superseded type certification
regulation and applicable time periods, and
the CFR edition and FEDERAL REGISTER documents where the regulation having prior effect is found. Copies of all superseded regulations may be obtained at the Federal Aviation Administration Law Library, Room 924,
800 Independence Avenue SW., Washington,
DC.

Part 121 section

Applicable aircraft

Provisions: CFR/FR references

Section 121.312(a)(1)(i) ............

Transport category; or nontransport category
type certificated before January 1, 1965; passenger capacity of 20 or more; manufactured
prior to August 20, 1990.

Section 121.312(a)(1)(ii) ...........

Transport category; or nontransport category
type certificated before January 1, 1965; passenger capacity of 20 or more; manufactured
after August 19, 1990.

Section 121.312(a)(2)(i) ............

Transport category; or nontransport category
type certificate before January 1, 1965; application for type certificate filed prior to May 1,
1972; substantially complete replacement of
cabin interior on or after May 1, 1972.
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; substantially complete replacement of the cabin interior 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 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.
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 September 26, 1988: 14 CFR parts 1 to 59, Revised as of January 1, 1988, and amended by
Amdt. 25-66, 53 FR 32584, August 25, 1988
Provisions of 14 CFR 25.853 in effect on April
30, 1972: 14 CFR parts 1 to 59, Revised as of
January 1, 1972.

Section 121.312(a)(3)(i) ............

Section 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; substantially complete replacement of the cabin interior on or after August 20, 1990.

Section 121.312(b) (1) and (2)

Transport category airplane type certificated after
January 1, 1958; Nontransport category airplane type certificated after December 31,
1964.

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.
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, February 2, 1995.
Formerly 14 CFR Section 25.853(a-1) in effect September 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.
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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