448
14 CFR Ch. I (1–1–19 Edition)
§ 135.169
(i) RTCA DO–204, Minimum Oper-
ational Performance Standards
(MOPS) 406 MHz Emergency Locator
Transmitters (ELTs), Sept. 29, 1989, and
(ii) RTCA DO–204A, Minimum Oper-
ational Performance Standards
(MOPS) 406 MHz Emergency Locator
Transmitters (ELT), Dec. 6, 2007.
[Doc. No. FAA–2010–0982, 79 FR 9973, Feb. 21,
2014, as amended by Amdt. 135–138, 83 FR
1189, Jan. 10, 2018]
§ 135.169
Additional airworthiness re-
quirements.
(a) Except for commuter category
airplanes, no person may operate a
large airplane unless it meets the addi-
tional airworthiness requirements of
§§ 121.213 through 121.283 and 121.307 of
this chapter.
(b) No person may operate a small
airplane that has a passenger-seating
configuration, excluding pilot seats, of
10 seats or more unless it is type cer-
tificated—
(1) In the transport category;
(2) Before July 1, 1970, in the normal
category and meets special conditions
issued by the Administrator for air-
planes intended for use in operations
under this part;
(3) Before July 19, 1970, in the normal
category and meets the additional air-
worthiness standards in Special Fed-
eral Aviation Regulation No. 23;
(4) In the normal category and meets
the additional airworthiness standards
in appendix A;
(5) In the normal category and com-
plies with section 1.(a) of Special Fed-
eral Aviation Regulation No. 41;
(6) In the normal category and com-
plies with section 1.(b) of Special Fed-
eral Aviation Regulation No. 41;
(7) In the commuter category; or
(8) In the normal category, as a
multi-engine certification level 4 air-
plane as defined in part 23 of this chap-
ter.
(c) No person may operate a small
airplane with a passenger seating con-
figuration, excluding any pilot seat, of
10 seats or more, with a seating con-
figuration greater than the maximum
seating configuration used in that type
airplane in operations under this part
before August 19, 1977. This paragraph
does not apply to—
(1) An airplane that is type certifi-
cated in the transport category; or
(2) An airplane that complies with—
(i) Appendix A of this part provided
that its passenger seating configura-
tion, excluding pilot seats, does not ex-
ceed 19 seats; or
(ii) Special Federal Aviation Regula-
tion No. 41.
(d) Cargo or baggage compartments:
(1) After March 20, 1991, each Class C
or D compartment, as defined in § 25.857
of part 25 of this chapter, greater than
200 cubic feet in volume in a transport
category airplane type certificated
after January 1, 1958, must have ceiling
and sidewall panels which are con-
structed of:
(i) Glass fiber reinforced resin;
(ii) Materials which meet the test re-
quirements of part 25, appendix F, part
III of this chapter; or
(iii) In the case of liner installations
approved prior to March 20, 1989, alu-
minum.
(2) For compliance with this para-
graph, the term ‘‘liner’’ includes any
design feature, such as a joint or fas-
tener, which would affect the capa-
bility of the liner to safely contain a
fire.
[Doc. No. 16097, 43 FR 46783, Oct. 10, 1978, as
amended by Amdt. 135–2, 44 FR 53731, Sept.
17, 1979; Amdt. 135–21, 52 FR 1836, Jan. 15,
1987; 52 FR 34745, Sept. 14, 1987; Amdt. 135–31,
54 FR 7389, Feb. 17, 1989; Amdt. 135–55, 60 FR
6628, Feb. 2, 1995; Docket FAA–2015–1621,
Amdt. 135–136, 81 FR 96701, Dec. 30, 2016]
§ 135.170
Materials for compartment
interiors.
(a) No person may operate an air-
plane that conforms to an amended or
supplemental type certificate issued in
accordance with SFAR No. 41 for a
maximum certificated takeoff weight
in excess of 12,500 pounds unless within
one year after issuance of the initial
airworthiness certificate under that
SFAR, the airplane meets the compart-
ment interior requirements set forth in
§ 25.853(a) in effect March 6, 1995 (for-
merly § 25.853 (a), (b), (b–1), (b–2), and
(b–3) of this chapter in effect on Sep-
tember 26, 1978).
(b) Except for commuter category
airplanes and airplanes certificated
under Special Federal Aviation Regula-
tion No. 41, no person may operate a
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