455
Federal Aviation Administration, DOT
§ 135.180
(3) of this section, and must be readily
accessible.
(k) On each large passenger-carrying
turbojet-powered airplane, each ven-
tral exit and tailcone exit must be—
(1) Designed and constructed so that
it cannot be opened during flight; and
(2) Marked with a placard readable
from a distance of 30 inches and in-
stalled at a conspicuous location near
the means of opening the exit, stating
that the exit has been designed and
constructed so that it cannot be opened
during flight.
(l)
Portable lights.
No person may op-
erate a passenger-carrying airplane un-
less it is equipped with flashlight stow-
age provisions accessible from each
flight attendant seat.
[Doc. No. 26530, 57 FR 19245, May 4, 1992; 57
FR 29120, June 30, 1992, as amended at 57 FR
34682, Aug. 6, 1992]
§ 135.179
Inoperable instruments and
equipment.
(a) No person may take off an air-
craft with inoperable instruments or
equipment installed unless the fol-
lowing conditions are met:
(1) An approved Minimum Equipment
List exists for that aircraft.
(2) The responsible Flight Standards
office has issued the certificate holder
operations specifications authorizing
operations in accordance with an ap-
proved Minimum Equipment List. The
flight crew shall have direct access at
all times prior to flight to all of the in-
formation contained in the approved
Minimum Equipment List through
printed or other means approved by the
Administrator in the certificate hold-
ers operations specifications. An ap-
proved Minimum Equipment List, as
authorized by the operations specifica-
tions, constitutes an approved change
to the type design without requiring
recertification.
(3) The approved Minimum Equip-
ment List must:
(i) Be prepared in accordance with
the limitations specified in paragraph
(b) of this section.
(ii) Provide for the operation of the
aircraft with certain instruments and
equipment in an inoperable condition.
(4) Records identifying the inoperable
instruments and equipment and the in-
formation required by (a)(3)(ii) of this
section must be available to the pilot.
(5) The aircraft is operated under all
applicable conditions and limitations
contained in the Minimum Equipment
List and the operations specifications
authorizing use of the Minimum Equip-
ment List.
(b) The following instruments and
equipment may not be included in the
Minimum Equipment List:
(1) Instruments and equipment that
are either specifically or otherwise re-
quired by the airworthiness require-
ments under which the airplane is type
certificated and which are essential for
safe operations under all operating
conditions.
(2) Instruments and equipment re-
quired by an airworthiness directive to
be in operable condition unless the air-
worthiness directive provides other-
wise.
(3) Instruments and equipment re-
quired for specific operations by this
part.
(c) Notwithstanding paragraphs (b)(1)
and (b)(3) of this section, an aircraft
with inoperable instruments or equip-
ment may be operated under a special
flight permit under §§ 21.197 and 21.199
of this chapter.
[Doc. No. 25780, 56 FR 12311, Mar. 22, 1991; 56
FR 14920, Apr. 8, 1991, as amended by Amdt.
135–60, 61 FR 2616, Jan. 26, 1996; Amdt. 135–91,
68 FR 54586, Sept. 17, 2003; Docket FAA–2018–
0119, Amdt. 135–139, 83 FR 9175, Mar. 5, 2018]
§ 135.180
Traffic Alert and Collision
Avoidance System.
(a) Unless otherwise authorized by
the Administrator, after December 31,
1995, no person may operate a turbine
powered airplane that has a passenger
seat configuration, excluding any pilot
seat, of 10 to 30 seats unless it is
equipped with an approved traffic alert
and collision avoidance system. If a
TCAS II system is installed, it must be
capable of coordinating with TCAS
units that meet TSO C–119.
(b) The airplane flight manual re-
quired by § 135.21 of this part shall con-
tain the following information on the
TCAS I system required by this sec-
tion:
(1) Appropriate procedures for—
(i) The use of the equipment; and
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