Section 121.1119

14 CFR Ch. I (1-1-19 Edition)
TABLE 2

Model - Boeing
747
737
777
767
757

Series
Series
Series
Series
Series

(17) Lockheed L-300.
[Doc. No. FAA-2005-22997, 73 FR 42501, July
21, 2008, as amended by Amdt. 121-345, 74 FR
31619, July 2, 2009; Docket FAA-2018-0119,
Amdt. 121-380, 83 FR 9173, Mar. 5, 2018]

Model - Airbus
A318, A319, A320, A321 Series
A300, A310 Series
A330, A340 Series

(l) For any certificate holder for
which the operating certificate is
issued after December 26, 2008, the compliance date specified in paragraph (e)
of this section may be extended by one
year, provided that the certificate
holder meets the requirements of paragraph (k)(2) of this section when its initial
operations
specifications
are
issued and, thereafter, uses ground air
conditioning systems as described in
paragraph (k)(2) of this section on each
airplane subject to the extension.
(m) After the date by which any person is required by this section to modify 100 percent of the affected fleet, no
certificate holder may operate in passenger service any airplane model specified in Table 2 of this section unless
the airplane has been modified to comply with Section 26.33(c) of this chapter.
(n) No certificate holder may operate
any airplane on which an auxiliary fuel
tank is installed after December 26,
2017 unless the FAA has certified the
tank as compliant with Section 25.981 of this
chapter, in effect on December 26, 2008.
(o) Exclusions. The requirements of
this section do not apply to the following airplane models:
(1) Convair CV-240, 340, 440, including
turbine powered conversions.
(2) Lockheed L-188 Electra.
(3) Vickers VC-10.
(4) Douglas DC-3, including turbine
powered conversions.
(5) Bombardier CL-44.
(6) Mitsubishi YS-11.
(7) BAC 1-11.
(8) Concorde.
(9) deHavilland D.H. 106 Comet 4C.
(10) VFW - Vereinigte Flugtechnische
VFW-614.
(11) Illyushin Aviation IL 96T.
(12) Bristol Aircraft Britannia 305.
(13) Handley Page Herald Type 300.
(14) Avions Marcel Dassault - Breguet
Aviation Mercure 100C.
(15) Airbus Caravelle.
(16) Fokker F-27/Fairchild Hiller FH-
227.

Section 121.1119 Fuel tank vent explosion
protection.
(a) Applicability. This section applies
to transport category, turbine-powered
airplanes with a type certificate issued
after January 1, 1958, that have:
(1) A maximum type-certificated passenger capacity of 30 or more; or
(2) A maximum payload capacity of
7,500 pounds or more.
(b) New production airplanes. No certificate holder may operate an airplane
for which the State of Manufacture
issued the original certificate of airworthiness or export airworthiness approval after August 23, 2018 unless
means, approved by the Administrator,
to prevent fuel tank explosions caused
by propagation of flames from outside
the fuel tank vents into the fuel tank
vapor spaces are installed and operational.
[Docket FAA-2014-0500, Amdt. 121-375, 81 FR
41208, June 24, 2016]

Subpart BB [Reserved]
SectionSection 121.1200-121.1399

[Reserved]

Subpart CC [Reserved]
SectionSection 121.1400-121.1499

[Reserved]

Subpart DD - Special Federal
Aviation Regulations
Section 121.1500 SFAR No. 111 - Lavatory Oxygen Systems.
(a) Applicability. This SFAR applies
to the following persons:
(1) All operators of transport category airplanes that are required to
comply with AD 2012-11-09, but only for
airplanes on which the actions required
by that AD have not been accomplished.
(2) Applicants for airworthiness certificates.
(3) Holders of production certificates.
(4) Applicants for type certificates,
including changes to type certificates.
(b) Regulatory relief. Except as noted
in paragraph (d) of this section and

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