408
14 CFR Ch. I (1–1–19 Edition)
§ 135.2
scheduled passenger-carrying oper-
ations in the kinds of airplanes de-
scribed 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 para-
graph (a)(1) of this section may not,
after March 20, 1997, operate an air-
plane described in paragraphs (a)(1)(i),
(a)(1)(ii), or (a)(1)(iii) of this section in
scheduled passenger-carrying oper-
ations, unless it obtains operations
specifications to conduct its scheduled
operations under part 121 of this chap-
ter 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 ap-
plicable requirement of part 121 of this
chapter on and after March 20, 1997 or
on and after the date on which the cer-
tificate holder is issued operations
specifications under this part, which-
ever 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 certifi-
cate 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 certifi-
cate holder that is covered by para-
graph (a) of this section may operate
an airplane in 14 CFR part 121 oper-
ations on or after a date listed in this
paragraph unless that airplane meets
the applicable requirement of this
paragraph:
(1)
Nontransport category turbo-
propeller powered airplanes type certifi-
cated after December 31, 1964, that have a
passenger seat configuration of 10–19
seats.
No certificate holder may oper-
ate 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 re-
quirement 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 pro-
tection.
(C) Section 121.310(e), Emergency exit
handle illumination.
(D) Section 121.337(b)(8), Protective
breathing equipment.
(E) Section 121.340, Emergency flota-
tion means.
(ii) December 20, 1999: Section 121.342,
Pitot heat indication system.
(iii) December 20, 2010:
(A) For airplanes described in
§ 121.157(f), the Airplane Performance
Operating Limitations in §§ 121.189
through 121.197.
(B) Section 121.161(b), Ditching ap-
proval.
(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 cer-
tificate 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 pro-
tection.
(B) Section 121.337(b) (8) and (9), Pro-
tective breathing equipment.
(C) Section 121.340, Emergency flota-
tion 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 oper-
ate 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 re-
quirement listed in this paragraph (e).
(1) For nontransport category turbo-
propeller powered airplanes type cer-
tificated 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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