749
Federal Aviation Administration, DOT
§ 34.6
that are not defined in that part but
that are used in this FAR have the
meaning given them in the Clean Air
Act, as amended by Public Law 91–604.
(h) All interpretations of 40 CFR part
87 that are rendered by the EPA also
apply to this FAR.
(i) If the EPA, under 40 CFR 87.3(a),
approves or accepts any testing and
sampling procedures or methods, ana-
lytical techniques, or related equip-
ment not identical to those specified in
that part, this FAR requires an appli-
cant to show that such alternate,
equivalent, or otherwise nonidentical
procedures have been complied with,
and that such alternate equipment was
used to show compliance, unless the
applicant elects to comply with those
procedures, methods, techniques, and
equipment specified in 40 CFR part 87.
(j) If the EPA, under 40 CFR 87.5, pre-
scribes special test procedures for any
aircraft or aircraft engine that is not
susceptible to satisfactory testing by
the procedures in 40 CFR part 87, the
applicant must show the Administrator
that those special test procedures have
been complied with.
(k) Wherever 40 CFR part 87 requires
agreement, acceptance, or approval by
the Administrator of the EPA, this
FAR requires a showing that such
agreement or approval has been ob-
tained.
(l) Pursuant to 42 U.S.C. 7573, no
state or political subdivision thereof
may adopt or attempt to enforce any
standard respecting emissions of any
air pollutant from any aircraft or en-
gine thereof unless that standard is
identical to a standard made applicable
to the aircraft by the terms of this
FAR.
(m) If EPA, by regulation or exemp-
tion, relaxes a provision of 40 CFR part
87 that is implemented in this FAR, no
state or political subdivision thereof
may adopt or attempt to enforce the
terms of this FAR that are superseded
by the relaxed requirement.
(n) If any provision of this FAR is
rendered inapplicable to a foreign air-
craft as provided in 40 CFR 87.3(c)
(international agreements), and
§ 34.3(d) of this FAR, that provision
may not be adopted or enforced against
that foreign aircraft by a state or po-
litical subdivision thereof.
(o) For exhaust emissions require-
ments of this FAR that apply begin-
ning February 1, 1974, January 1, 1976,
January 1, 1978, January 1, 1984, and
August 9, 1985, continued compliance
with those requirements is shown for
engines for which the type design has
been shown to meet those require-
ments, if the engine is maintained in
accordance with applicable mainte-
nance requirements for 14 CFR chapter
I. All methods of demonstrating com-
pliance and all model designations pre-
viously found acceptable to the Admin-
istrator shall be deemed to continue to
be an acceptable demonstration of
compliance with the specific standards
for which they were approved.
(p) Each applicant must allow the
Administrator to make, or witness,
any test necessary to determine com-
pliance with the applicable provisions
of this FAR.
[Doc. No. 25613, 55 FR 32861, Aug. 10, 1990; 55
FR 37287, Sept. 10, 1990; Amdt. 34–5, 77 FR
76850, Dec. 31, 2012]
§ 34.4
[Reserved]
§ 34.5
Special test procedures.
The Administrator or the Adminis-
trator of the EPA may, upon written
application by a manufacturer or oper-
ator of aircraft or aircraft engines, ap-
prove test procedures for any aircraft
or aircraft engine that is not suscep-
tible to satisfactory testing by the pro-
cedures set forth herein. Prior to tak-
ing action on any such application, the
Administrator or the Administrator of
the EPA shall consult with the other.
§ 34.6
Aircraft safety.
(a) The provisions of this part will be
revised if at any time the Adminis-
trator determines that an emission
standard cannot be met within the
specified time without creating a safe-
ty hazard.
(b) Consistent with 40 CFR 87.6, if the
FAA Administrator determines that
any emission control regulation in this
part cannot be safely applied to an air-
craft, that provision may not be adopt-
ed or enforced against that aircraft by
any state or political subdivision
thereof.
VerDate Sep<11>2014
09:06 Jun 28, 2024
Jkt 262046
PO 00000
Frm 00759
Fmt 8010
Sfmt 8010
Y:\SGML\262046.XXX
262046
jspears on DSK121TN23PROD with CFR