spaschal on DSK3GDR082PROD with CFR

Federal Aviation Administration, DOT

Section 21.183

(1) The applicant presents evidence to
the FAA that the aircraft conforms to
a type design approved under a type
certificate or a supplemental type certificate and to applicable Airworthiness Directives;
(2) The aircraft (except an experimentally certificated aircraft that previously had been issued a different airworthiness certificate under this section) has been inspected in accordance
with the performance rules for 100-hour
inspections set forth in Section 43.15 of this
chapter, or an equivalent performance
standard acceptable to the FAA, and
found airworthy by - 
(i) The manufacturer;
(ii) The holder of a repair station certificate as provided in Part 145 of this
chapter;
(iii) The holder of a mechanic certificate as authorized in Part 65 of this
chapter; or
(iv) The holder of a certificate issued
under part 121 of this chapter, and having a maintenance and inspection organization appropriate to the aircraft
type; and
(3) The FAA finds after inspection,
that the aircraft conforms to the type
design, and is in condition for safe operation.
(e)
Noise
requirements.
Notwithstanding all other provisions of this
section, the following must be complied with for the original issuance of a
standard airworthiness certificate:
(1) For transport category large airplanes and jet (turbojet powered) airplanes that have not had any flight
time before the dates specified in
Section 36.1(d), no standard airworthiness certificate is originally issued under this
section unless the FAA finds that the
type design complies with the noise requirements in Section 36.1(d) in addition to
the applicable airworthiness requirements in this section. For import airplanes, compliance with this paragraph
is shown if the country in which the
airplane was manufactured certifies,
and the FAA finds, that Section 36.1(d) (or the
applicable airplane noise requirements
of the country in which the airplane
was manufactured and any other requirements the FAA may prescribe to
provide noise levels no greater than
those provided by compliance with

Section 36.1(d)) and paragraph (c) of this section are complied with.
(2) For normal, utility, acrobatic,
commuter, or transport category propeller driven small airplanes (except
for those airplanes that are designed
for  - agricultural aircraft operations - 
(as defined in Section 137.3 of this chapter, as
effective on January 1, 1966) or for dispensing fire fighting materials to
which Section 36.1583 of this chapter does not
apply) that have not had any flight
time before the applicable date specified in part 36 of this chapter, no standard airworthiness certificate is originally issued under this section unless
the applicant shows that the type design complies with the applicable noise
requirements of part 36 of this chapter
in addition to the applicable airworthiness requirements in this section. For
import airplanes, compliance with this
paragraph is shown if the country in
which the airplane was manufactured
certifies, and the FAA finds, that the
applicable requirements of part of this
chapter (or the applicable airplane
noise requirements of the country in
which the airplane was manufactured
and any other requirements the FAA
may prescribe to provide noise levels
no greater than those provided by compliance with the applicable requirements of part 36 of this chapter) and
paragraph (c) of this section are complied with.
(f) Passenger emergency exit requirements. Notwithstanding all other provisions of this section, each applicant for
issuance of a standard airworthiness
certificate for a transport category airplane manufactured after October 16,
1987, must show that the airplane
meets the requirements of Section 25.807(c)(7)
in effect on July 24, 1989. For the purposes of this paragraph, the date of
manufacture of an airplane is the date
the inspection acceptance records reflect that the airplane is complete and
meets the FAA-approved type design
data.
(g) Fuel venting and exhaust emission
requirements. Notwithstanding all other
provisions of this section, and irrespective of the date of application, no airworthiness certificate is issued, on and
after the dates specified in part 34 for
the airplanes specified therein, unless

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