Federal Aviation Administration, DOT

Section 121.2

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 this part on
and after the date on which that person
is issued a certificate and operations
specifications under this part.
(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 (d) unless that airplane
meets the applicable requirement of
this paragraph (d):
(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 this part an airplane manufactured on or after a date listed in
this paragraph 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:
(A) Section 121.305(j), Third attitude
indicator.
(B) Section 121.311(f), Safety belts
and shoulder harnesses.
(ii) Manufactured on or after December 20, 1997; Section 121.317(a), Fasten
seat belt light.
(iii) Manufactured on or after December 20, 1999: Section 121.293, Takeoff
warning system.
(iv) Manufactured on or after March
12, 1999: Section 121.310(b)(1), Interior
emergency exit locating sign.
(2) For transport category turbopropeller powered airplanes that have a
passenger seat configuration of 20-30
seats manufactured on or after March
20, 1997: Section 121.305(j), Third attitude indicator.
(f) New type certification requirements.
No person may operate an airplane for

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