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114 

14 CFR Ch. I (1–1–24 Edition) 

§ 121.291 

(2) Must be in addition to the throt-

tle-actuated device installed under the 
type certification airworthiness re-
quirements; and 

(3) May utilize any part of the throt-

tle-actuated system including the 
aural warning device. 

(c) The flap position sensing unit 

may be installed at any suitable place 
in the airplane. 

[Doc. No. 6258, 29 FR 19202, Dec. 31, 1964, as 
amended by Amdt. 121–3, 30 FR 3638, Mar. 19, 
1965; Amdt. 121–130, 41 FR 47229, Oct. 28, 1976; 
Amdt. 121–227, 56 FR 63762, Dec. 5, 1991; Amdt. 
121–251, 60 FR 65929, Dec. 20, 1995] 

§ 121.291 Demonstration of emergency 

evacuation procedures. 

(a) Except as provided in paragraph 

(a)(1) of this section, each certificate 
holder must conduct an actual dem-
onstration of emergency evacuation 
procedures in accordance with para-
graph (a) of appendix D to this part to 
show that each type and model of air-
plane with a seating capacity of more 
than 44 passengers to be used in its pas-
senger-carrying operations allows the 
evacuation of the full capacity, includ-
ing crewmembers, in 90 seconds or less. 

(1) An actual demonstration need not 

be conducted if that airplane type and 
model has been shown to be in compli-
ance with this paragraph in effect on or 
after October 24, 1967, or, if during type 
certification, with § 25.803 of this chap-
ter in effect on or after December 1, 
1978. 

(2) Any actual demonstration con-

ducted after September 27, 1993, must 
be in accordance with paragraph (a) of 
appendix D to this part in effect on or 
after that date or with § 25.803 in effect 
on or after that date. 

(b) Each certificate holder con-

ducting operations with airplanes with 
a seating capacity of more than 44 pas-
sengers must conduct a partial dem-
onstration of emergency evacuation 
procedures in accordance with para-
graph (c) of this section upon: 

(1) Initial introduction of a type and 

model of airplane into passenger-car-
rying operation; 

(2) Changing the number, location, or 

emergency evacuation duties or proce-
dures of flight attendants who are re-
quired by § 121.391; or 

(3) Changing the number, location, 

type of emergency exits, or type of 
opening mechanism on emergency 
exits available for evacuation. 

(c) In conducting the partial dem-

onstration required by paragraph (b) of 
this section, each certificate holder 
must: 

(1) Demonstrate the effectiveness of 

its crewmember emergency training 
and evacuation procedures by con-
ducting a demonstration, not requiring 
passengers and observed by the Admin-
istrator, in which the flight attendants 
for that type and model of airplane, 
using that operator’s line operating 
procedures, open 50 percent of the re-
quired floor-level emergency exits and 
50 percent of the required non-floor- 
level emergency exits whose opening 
by a flight attendant is defined as an 
emergency evacuation duty under 
§ 121.397, and deploy 50 percent of the 
exit slides. The exits and slides will be 
selected by the administrator and must 
be ready for use within 15 seconds; 

(2) Apply for and obtain approval 

from the responsible Flight Standards 
office before conducting the dem-
onstration; 

(3) Use flight attendants in this dem-

onstration who have been selected at 
random by the Administrator, have 
completed the certificate holder’s 
FAA-approved training program for the 
type and model of airplane, and have 
passed a written or practical examina-
tion on the emergency equipment and 
procedures; and 

(4) Apply for and obtain approval 

from the responsible Flight Standards 
office before commencing operations 
with this type and model airplane. 

(d) Each certificate holder operating 

or proposing to operate one or more 
landplanes in extended overwater oper-
ations, or otherwise required to have 
certain equipment under § 121.339, must 
show, by simulated ditching conducted 
in accordance with paragraph (b) of ap-
pendix D to this part, that it has the 
ability to efficiently carry out its 
ditching procedures. For certificate 
holders subject to § 121.2(a)(1), this 
paragraph applies only when a new 
type or model airplane is introduced 
into the certificate holder’s operations 
after January 19, 1996. 

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115 

Federal Aviation Administration, DOT 

§ 121.305 

(e) For a type and model airplane for 

which the simulated ditching specified 
in paragraph (d) has been conducted by 
a part 121 certificate holder, the re-
quirements of paragraphs (b)(2), (b)(4), 
and (b)(5) of appendix D to this part are 
complied with if each life raft is re-
moved from stowage, one life raft is 
launched and inflated (or one slide life 
raft is inflated) and crewmembers as-
signed to the inflated life raft display 
and describe the use of each item of re-
quired emergency equipment. The life 
raft or slide life raft to be inflated will 
be selected by the Administrator. 

[Doc. No. 21269, 46 FR 61453, Dec. 17, 1981, as 
amended by Amdt. 121–233, 58 FR 45230, Aug. 
26, 1993; Amdt. 121–251, 60 FR 65929, Dec. 20, 
1995; Amdt. 121–307, 69 FR 67499, Nov. 17, 2004; 
Docket FAA–2018–0119, Amdt. 121–380, 83 FR 
9172, Mar. 5, 2018] 

§ 121.293 Special airworthiness re-

quirements for nontransport cat-
egory airplanes type certificated 
after December 31, 1964. 

No certificate holder may operate a 

nontransport category airplane manu-
factured after December 20, 1999 unless 
the airplane contains a takeoff warning 
system that meets the requirements of 
14 CFR 25.703. However, the takeoff 
warning system does not have to cover 
any device for which it has been dem-
onstrated that takeoff with that device 
in the most adverse position would not 
create a hazardous condition. 

[Doc. No. 28154, 60 FR 65929, Dec. 20, 1995] 

§ 121.295 Location for a suspect device. 

After November 28, 2009, all airplanes 

with a maximum certificated passenger 
seating capacity of more than 60 per-
sons must have a location where a sus-
pected explosive or incendiary device 
found in flight can be placed to mini-
mize the risk to the airplane. 

[Doc. No. FAA–2006–26722, 73 FR 63880, Oct. 
28, 2008] 

Subpart K—Instrument and 

Equipment Requirements 

S

OURCE

: Docket No. 6258, 29 FR 19205, Dec. 

31, 1964, unless otherwise noted. 

§ 121.301 Applicability. 

This subpart prescribes instrument 

and equipment requirements for all 
certificate holders. 

§ 121.303 Airplane instruments and 

equipment. 

(a) Unless otherwise specified, the in-

strument and equipment requirements 
of this subpart apply to all operations 
under this part. 

(b) Instruments and equipment re-

quired by §§ 121.305 through 121.359 and 
121.803 must be approved and installed 
in accordance with the airworthiness 
requirements applicable to them. 

(c) Each airspeed indicator must be 

calibrated in knots, and each airspeed 
limitation and item of related informa-
tion in the Airplane Flight Manual and 
pertinent placards must be expressed in 
knots. 

(d) Except as provided in §§ 121.627(b) 

and 121.628, no person may take off any 
airplane unless the following instru-
ments and equipment are in operable 
condition: 

(1) Instruments and equipment re-

quired to comply with airworthiness 
requirements under which the airplane 
is type certificated and as required by 
§§ 121.213 through 121.283 and 121.289. 

(2) Instruments and equipment speci-

fied in §§ 121.305 through 121.321, 121.359, 
121.360, and 121.803 for all operations, 
and the instruments and equipment 
specified in §§ 121.323 through 121.351 for 
the kind of operation indicated, wher-
ever these items are not already re-
quired by paragraph (d)(1) of this sec-
tion. 

[Doc. No. 6258, 29 FR 19202, Dec. 31, 1964, as 
amended by Amdt. 121–44, 33 FR 14406, Sept. 
25, 1968; Amdt. 121–65, 35 FR 12709, Aug. 11, 
1970; Amdt. 121–114, 39 FR 44440, Dec. 24, 1974; 
Amdt. 121–126, 40 FR 55314, Nov. 28, 1975; 
Amdt. 121–222, 56 FR 12310, Mar. 22, 1991; 
Amdt. 121–253, 61 FR 2611, Jan. 26, 1996; Amdt. 
121–281, 66 FR 19043, Apr. 12, 2001] 

§ 121.305 Flight and navigational 

equipment. 

No person may operate an airplane 

unless it is equipped with the following 
flight and navigational instruments 
and equipment: 

(a) An airspeed indicating system 

with heated pitot tube or equivalent