283
Federal Aviation Administration, DOT
§ 25.783
(6) It must not be possible to unlatch
the latches with the locks in the
locked position. Locks must be de-
signed to withstand the limit loads re-
sulting from—
(i) The maximum operator effort
when the latches are operated manu-
ally;
(ii) The powered latch actuators, if
installed; and
(iii) The relative motion between the
latch and the structural counterpart.
(7) Each door for which unlatching
would not result in a hazard is not re-
quired to have a locking mechanism
meeting the requirements of para-
graphs (d)(3) through (d)(6) of this sec-
tion.
(e)
Warning, caution, and advisory in-
dications.
Doors must be provided with
the following indications:
(1) There must be a positive means to
indicate at each door operator’s station
that all required operations to close,
latch, and lock the door(s) have been
completed.
(2) There must be a positive means
clearly visible from each operator sta-
tion for any door that could be a haz-
ard if unlatched to indicate if the door
is not fully closed, latched, and locked.
(3) There must be a visual means on
the flight deck to signal the pilots if
any door is not fully closed, latched,
and locked. The means must be de-
signed such that any failure or com-
bination of failures that would result
in an erroneous closed, latched, and
locked indication is improbable for—
(i) Each door that is subject to pres-
surization and for which the initial
opening movement is not inward; or
(ii) Each door that could be a hazard
if unlatched.
(4) There must be an aural warning
to the pilots prior to or during the ini-
tial portion of takeoff roll if any door
is not fully closed, latched, and locked,
and its opening would prevent a safe
takeoff and return to landing.
(f)
Visual inspection provision.
Each
door for which unlatching of the door
could be a hazard must have a provi-
sion for direct visual inspection to de-
termine, without ambiguity, if the
door is fully closed, latched, and
locked. The provision must be perma-
nent and discernible under operational
lighting conditions, or by means of a
flashlight or equivalent light source.
(g)
Certain maintenance doors, remov-
able emergency exits, and access panels.
Some doors not normally opened ex-
cept for maintenance purposes or emer-
gency evacuation and some access pan-
els need not comply with certain para-
graphs of this section as follows:
(1) Access panels that are not subject
to cabin pressurization and would not
be a hazard if open during flight need
not comply with paragraphs (a)
through (f) of this section, but must
have a means to prevent inadvertent
opening during flight.
(2) Inward-opening removable emer-
gency exits that are not normally re-
moved, except for maintenance pur-
poses or emergency evacuation, and
flight deck-openable windows need not
comply with paragraphs (c) and (f) of
this section.
(3) Maintenance doors that meet the
conditions of paragraph (h) of this sec-
tion, and for which a placard is pro-
vided limiting use to maintenance ac-
cess, need not comply with paragraphs
(c) and (f) of this section.
(h)
Doors that are not a hazard.
For
the purposes of this section, a door is
considered not to be a hazard in the un-
latched condition during flight, pro-
vided it can be shown to meet all of the
following conditions:
(1) Doors in pressurized compart-
ments would remain in the fully closed
position if not restrained by the
latches when subject to a pressure
greater than
1
⁄
2
psi. Opening by persons,
either inadvertently or intentionally,
need not be considered in making this
determination.
(2) The door would remain inside the
airplane or remain attached to the air-
plane if it opens either in pressurized
or unpressurized portions of the flight.
This determination must include the
consideration of inadvertent and inten-
tional opening by persons during either
pressurized or unpressurized portions
of the flight.
(3) The disengagement of the latches
during flight would not allow depres-
surization of the cabin to an unsafe
level. This safety assessment must in-
clude the physiological effects on the
occupants.
VerDate Sep<11>2014
12:50 Apr 30, 2019
Jkt 247046
PO 00000
Frm 00293
Fmt 8010
Sfmt 8010
Y:\SGML\247046.XXX
247046
spaschal on DSK3GDR082PROD with CFR