Section 135.2

14 CFR Ch. I (1-1-19 Edition)

scheduled
passenger-carrying
operations in the kinds of airplanes described in paragraphs (a)(1)(i), (a)(1)(ii),
or paragraph (a)(1)(iii) of this section.
(b) Obtaining operations specifications.
A certificate holder described in paragraph (a)(1) of this section may not,
after March 20, 1997, operate an airplane described in paragraphs (a)(1)(i),
(a)(1)(ii), or (a)(1)(iii) of this section in
scheduled
passenger-carrying
operations, unless it obtains operations
specifications to conduct its scheduled
operations under part 121 of this chapter on or before March 20, 1997.
(c) Regular or accelerated compliance.
Except as provided in paragraphs (d),
and (e) of this section, each certificate
holder described in paragraph (a)(1) of
this section shall comply with each applicable requirement of part 121 of this
chapter on and after March 20, 1997 or
on and after the date on which the certificate holder is issued operations
specifications under this part, whichever occurs first. Except as provided in
paragraphs (d) and (e) of this section,
each person described in paragraph
(a)(2) of this section shall comply with
each applicable requirement of part 121
of this chapter on and after the date on
which that person is issued a certificate and operations specifications
under part 121 of this chapter.
(d) Delayed compliance dates. Unless
paragraph (e) of this section specifies
an earlier compliance date, no certificate holder that is covered by paragraph (a) of this section may operate
an airplane in 14 CFR part 121 operations on or after a date listed in this
paragraph unless that airplane meets
the applicable requirement of this
paragraph:
(1)
Nontransport
category
turbopropeller powered airplanes type certificated after December 31, 1964, that have a
passenger seat configuration of 10-19
seats. No certificate holder may operate under this part an airplane that is
described in paragraph (a)(1)(i) of this
section on or after a date listed in
paragraph (d)(1) of this section unless
that airplane meets the applicable requirement listed in paragraph (d)(1) of
this section:
(i) December 20, 1997:
(A) Section 121.289, Landing gear
aural warning.

(B) Section 121.308, Lavatory fire protection.
(C) Section 121.310(e), Emergency exit
handle illumination.
(D) Section 121.337(b)(8), Protective
breathing equipment.
(E) Section 121.340, Emergency flotation means.
(ii) December 20, 1999: Section 121.342,
Pitot heat indication system.
(iii) December 20, 2010:
(A) For airplanes described in
Section 121.157(f), the Airplane Performance
Operating Limitations in SectionSection 121.189
through 121.197.
(B) Section 121.161(b), Ditching approval.
(C) Section 121.305(j), Third attitude
indicator.
(D) Section 121.312(c), Passenger seat
cushion flammability.
(iv)
March
12,
1999:
Section
121.310(b)(1), Interior emergency exit
locating sign.
(2) Transport category turbopropeller
powered airplanes that have a passenger
seat configuration of 20-30 seats. No certificate holder may operate under this
part an airplane that is described in
paragraph (a)(1)(ii) of this section on or
after a date listed in paragraph (d)(2) of
this section unless that airplane meets
the applicable requirement listed in
paragraph (d)(2) of this section:
(i) December 20, 1997:
(A) Section 121.308, Lavatory fire protection.
(B) Section 121.337(b) (8) and (9), Protective breathing equipment.
(C) Section 121.340, Emergency flotation means.
(ii) December 20, 2010: Section
121.305(j), Third attitude indicator.
(e) Newly manufactured airplanes. No
certificate holder that is described in
paragraph (a) of this section may operate under part 121 of this chapter an
airplane manufactured on or after a
date listed in this paragraph (e) unless
that airplane meets the applicable requirement listed in this paragraph (e).
(1) For nontransport category turbopropeller powered airplanes type certificated after December 31, 1964, that
have a passenger seat configuration of
10-19 seats:
(i) Manufactured on or after March
20, 1997:

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