Code of Federal Regulations - Title 14

371

Federal Aviation Administration, DOT

§ 25.5

greater than that for which the air-
plane has been type certificated must
show that the airplane concerned
meets the requirements of:

(1) Sections 25.721(d), 25.783(g),

25.785(c), 25.803(c)(2) through (9), 25.803
(d) and (e), 25.807 (a), (c), and (d), 25.809
(f) and (h), 25.811, 25.812, 25.813 (a), (b),
and (c), 25.815, 25.817, 25.853 (a) and (b),
25.855(a), 25.993(f), and 25.1359(c) in ef-
fect on October 24, 1967, and

(2) Sections 25.803(b) and 25.803(c)(1)

in effect on April 23, 1969.

(b) Irrespective of the date of applica-

tion, each applicant for a supplemental
type certificate (or an amendment to a
type certificate) for an airplane manu-
factured after October 16, 1987, must
show that the airplane meets the re-
quirements of § 25.807(c)(7) in effect on
July 24, 1989.

sions to the sections specified in para-
graph (a) or (b) of this section may be
elected or may be required in accord-
ance with § 21.101(a) of this chapter.

[Amdt. 25–72, 55 FR 29773, July 20, 1990, as
amended by Amdt. 25–99, 65 FR 36266, June 7,
2000]

§ 25.3

Special provisions for ETOPS

type design approvals.

(a)

Applicability. This section applies

to an applicant for ETOPS type design
approval of an airplane:

(1) That has an existing type certifi-

cate on February 15, 2007; or

(2) For which an application for an

original type certificate was submitted
before February 15, 2007.

(b)

Airplanes with two engines. (1) For

ETOPS type design approval of an air-
plane up to and including 180 minutes,
an applicant must comply with
§ 25.1535, except that it need not comply
with the following provisions of Appen-
dix K, K25.1.4, of this part:

(i) K25.1.4(a), fuel system pressure

and flow requirements;

(ii) K25.1.4(a)(3), low fuel alerting;

and

(iii) K25.1.4(c), engine oil tank design.
(2) For ETOPS type design approval

of an airplane beyond 180 minutes an
applicant must comply with § 25.1535.

(c)

Airplanes with more than two en-

gines. An applicant for ETOPS type de-
sign approval must comply with
§ 25.1535 for an airplane manufactured

on or after February 17, 2015, except
that, for an airplane configured for a
three person flight crew, the applicant
need not comply with Appendix K,
K25.1.4(a)(3), of this part, low fuel alert-
ing.

[Doc. No. FAA–2002–6717, 72 FR 1873, Jan. 16,
2007]

§ 25.5

Incorporations by reference.

(a) The materials listed in this sec-

tion are incorporated by reference in
the corresponding sections noted.
These incorporations by reference were
approved by the Director of the Federal
Register in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. These mate-
rials are incorporated as they exist on
the date of the approval, and notice of
any change in these materials will be
published in the F

EDERAL

EGISTER

The materials are available for pur-
chase at the corresponding addresses
noted below, and all are available for
inspection at the National Archives
and Records Administration (NARA),
and at FAA, Transport Airplane Direc-
torate, Aircraft Certification Service,
1601 Lind Avenue, SW., Renton, Wash-
ington 98057–3356. For information on
the availability of this material at
NARA, call 202–741–6030, or go to:

http://

www.archives.gov/federal

lregister/

code

loflfederallregulations/

ibr

llocations.html.

(b) The following materials are avail-

able for purchase from the following
address: The National Technical Infor-
mation Services (NTIS), Springfield,
Virginia 22166.

(1) Fuel Tank Flammability Assess-

ment Method User’s Manual, dated
May 2008, document number DOT/FAA/
AR–05/8, IBR approved for § 25.981 and
Appendix N. It can also be obtained at
the following Web site:

http://

www.fire.tc.faa.gov/systems/fueltank/
FTFAM.stm.

(2) [Reserved]

[73 FR 42494, July 21, 2008]

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