title-14-part-91-sec91-1037

784

14 CFR Ch. I (1–1–24 Edition)

§ 91.1035

(b) Each cockpit checklist required

by paragraph (a)(1) of this section must
contain the following procedures:

(1) Before starting engines;
(2) Before takeoff;
(3) Cruise;
(4) Before landing;
(5) After landing; and
(6) Stopping engines.
(c) Each emergency cockpit checklist

required by paragraph (a)(2) of this sec-
tion must contain the following proce-
dures, as appropriate:

(1) Emergency operation of fuel, hy-

draulic, electrical, and mechanical sys-
tems.

(2) Emergency operation of instru-

ments and controls.

(3) Engine inoperative procedures.
(4) Any other emergency procedures

necessary for safety.

§ 91.1035

Passenger awareness.

(a) Prior to each takeoff, the pilot in

command of an aircraft carrying pas-
sengers on a program flight must en-
sure that all passengers have been oral-
ly briefed on—

(1)

Smoking: Each passenger must be

briefed on when, where, and under what
conditions smoking is prohibited. This
briefing must include a statement, as
appropriate, that the regulations re-
quire passenger compliance with light-
ed passenger information signs and no
smoking placards, prohibit smoking in
lavatories, and require compliance
with crewmember instructions with re-
gard to these items;

(2)

Use of safety belts, shoulder har-

nesses, and child restraint systems: Each
passenger must be briefed on when,
where and under what conditions it is
necessary to have his or her safety belt
and, if installed, his or her shoulder
harness fastened about him or her, and
if a child is being transported, the ap-
propriate use of child restraint sys-
tems, if available. This briefing must
include a statement, as appropriate,
that the regulations require passenger
compliance with the lighted passenger
information sign and/or crewmember
instructions with regard to these
items;

(3) The placement of seat backs in an

upright position before takeoff and
landing;

(4) Location and means for opening

the passenger entry door and emer-
gency exits;

(5) Location of survival equipment;
(6) Ditching procedures and the use of

flotation equipment required under
§ 91.509 for a flight over water;

(7) The normal and emergency use of

oxygen installed in the aircraft; and

(8) Location and operation of fire ex-

tinguishers.

(b) Prior to each takeoff, the pilot in

command of an aircraft carrying pas-
sengers on a program flight must en-
sure that each person who may need
the assistance of another person to
move expeditiously to an exit if an
emergency occurs and that person’s at-
tendant, if any, has received a briefing
as to the procedures to be followed if
an evacuation occurs. This paragraph
does not apply to a person who has
been given a briefing before a previous
leg of that flight in the same aircraft.

command must advise the passengers
of the name of the entity in oper-
ational control of the flight.

(d) The oral briefings required by

paragraphs (a), (b), and (c) of this sec-
tion must be given by the pilot in com-
mand or another crewmember.

(e) The oral briefing required by

paragraph (a) of this section may be de-
livered by means of an approved re-
cording playback device that is audible
to each passenger under normal noise
levels.

(f) The oral briefing required by para-

graph (a) of this section must be sup-
plemented by printed cards that must
be carried in the aircraft in locations
convenient for the use of each pas-
senger. The cards must—

(1) Be appropriate for the aircraft on

which they are to be used;

(2) Contain a diagram of, and method

of operating, the emergency exits; and

(3) Contain other instructions nec-

essary for the use of emergency equip-
ment on board the aircraft.

§ 91.1037

Large transport category air-

planes: Turbine engine powered;
Limitations; Destination and alter-
nate airports.

(a) No program manager or any other

person may permit a turbine engine
powered large transport category air-
plane on a program flight to take off

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Federal Aviation Administration, DOT

§ 91.1037

that airplane at a weight that (allow-
ing for normal consumption of fuel and
oil in flight to the destination or alter-
nate airport) the weight of the airplane
on arrival would exceed the landing
weight in the Airplane Flight Manual
for the elevation of the destination or
alternate airport and the ambient tem-
perature expected at the time of land-
ing.

(b) Except as provided in paragraph

(c) of this section, no program manager
or any other person may permit a tur-
bine engine powered large transport
category airplane on a program flight
to take off that airplane unless its
weight on arrival, allowing for normal
consumption of fuel and oil in flight (in
accordance with the landing distance
in the Airplane Flight Manual for the
elevation of the destination airport and
the wind conditions expected there at
the time of landing), would allow a full
stop landing at the intended destina-
tion airport within 60 percent of the ef-
fective length of each runway described
below from a point 50 feet above the
intersection of the obstruction clear-
ance plane and the runway. For the
purpose of determining the allowable
landing weight at the destination air-
port, the following is assumed:

(1) The airplane is landed on the most

favorable runway and in the most fa-
vorable direction, in still air.

(2) The airplane is landed on the most

suitable runway considering the prob-
able wind velocity and direction and
the ground handling characteristics of
that airplane, and considering other
conditions such as landing aids and ter-
rain.

son flying a turbine engine powered
large transport category airplane on a
program flight may permit that air-
plane to take off at a weight in excess
of that allowed by paragraph (b) of this
section if all of the following condi-
tions exist:

(1) The operation is conducted in ac-

cordance with an approved Destination
Airport Analysis in that person’s pro-
gram operating manual that contains
the elements listed in § 91.1025(o).

(2) The airplane’s weight on arrival,

allowing for normal consumption of
fuel and oil in flight (in accordance
with the landing distance in the Air-

plane Flight Manual for the elevation
of the destination airport and the wind
conditions expected there at the time
of landing), would allow a full stop
landing at the intended destination air-
port within 80 percent of the effective
length of each runway described below
from a point 50 feet above the intersec-
tion of the obstruction clearance plane
and the runway. For the purpose of de-
termining the allowable landing weight
at the destination airport, the fol-
lowing is assumed:

(i) The airplane is landed on the most

favorable runway and in the most fa-
vorable direction, in still air.

(ii) The airplane is landed on the

most suitable runway considering the
probable wind velocity and direction
and the ground handling characteris-
tics of that airplane, and considering
other conditions such as landing aids
and terrain.

(3) The operation is authorized by

management specifications.

(d) No program manager or other per-

son may select an airport as an alter-
nate airport for a turbine engine pow-
ered large transport category airplane
unless (based on the assumptions in
paragraph (b) of this section) that air-
plane, at the weight expected at the
time of arrival, can be brought to a full
stop landing within 80 percent of the
effective length of the runway from a
point 50 feet above the intersection of
the obstruction clearance plane and
the runway.

(e) Unless, based on a showing of ac-

tual operating landing techniques on
wet runways, a shorter landing dis-
tance (but never less than that re-
quired by paragraph (b) or (c) of this
section) has been approved for a spe-
cific type and model airplane and in-
cluded in the Airplane Flight Manual,
no person may take off a turbojet air-
plane when the appropriate weather re-
ports or forecasts, or any combination
of them, indicate that the runways at
the destination or alternate airport
may be wet or slippery at the esti-
mated time of arrival unless the effec-
tive runway length at the destination
airport is at least 115 percent of the
runway length required under para-
graph (b) or (c) of this section.