282
14 CFR Ch. I (1–1–19 Edition)
§ 25.783
(2) Each door that could be a hazard
if it unlatches must be designed so that
unlatching during pressurized and un-
pressurized flight from the fully closed,
latched, and locked condition is ex-
tremely improbable. This must be
shown by safety analysis.
(3) Each element of each door oper-
ating system must be designed or,
where impracticable, distinctively and
permanently marked, to minimize the
probability of incorrect assembly and
adjustment that could result in a mal-
function.
(4) All sources of power that could
initiate unlocking or unlatching of any
door must be automatically isolated
from the latching and locking systems
prior to flight and it must not be pos-
sible to restore power to the door dur-
ing flight.
(5) Each removable bolt, screw, nut,
pin, or other removable fastener must
meet the locking requirements of
§ 25.607.
(6) Certain doors, as specified by
§ 25.807(h), must also meet the applica-
ble requirements of §§ 25.809 through
25.812 for emergency exits.
(b)
Opening by persons.
There must be
a means to safeguard each door against
opening during flight due to inad-
vertent action by persons. In addition,
design precautions must be taken to
minimize the possibility for a person to
open a door intentionally during flight.
If these precautions include the use of
auxiliary devices, those devices and
their controlling systems must be de-
signed so that—
(1) No single failure will prevent
more than one exit from being opened;
and
(2) Failures that would prevent open-
ing of the exit after landing are im-
probable.
(c)
Pressurization prevention means.
There must be a provision to prevent
pressurization of the airplane to an un-
safe level if any door subject to pres-
surization is not fully closed, latched,
and locked.
(1) The provision must be designed to
function after any single failure, or
after any combination of failures not
shown to be extremely improbable.
(2) Doors that meet the conditions
described in paragraph (h) of this sec-
tion are not required to have a dedi-
cated pressurization prevention means
if, from every possible position of the
door, it will remain open to the extent
that it prevents pressurization or safe-
ly close and latch as pressurization
takes place. This must also be shown
with any single failure and malfunc-
tion, except that—
(i) With failures or malfunctions in
the latching mechanism, it need not
latch after closing; and
(ii) With jamming as a result of me-
chanical failure or blocking debris, the
door need not close and latch if it can
be shown that the pressurization loads
on the jammed door or mechanism
would not result in an unsafe condi-
tion.
(d)
Latching and locking.
The latching
and locking mechanisms must be de-
signed as follows:
(1) There must be a provision to latch
each door.
(2) The latches and their operating
mechanism must be designed so that,
under all airplane flight and ground
loading conditions, with the door
latched, there is no force or torque
tending to unlatch the latches. In addi-
tion, the latching system must include
a means to secure the latches in the
latched position. This means must be
independent of the locking system.
(3) Each door subject to pressuriza-
tion, and for which the initial opening
movement is not inward, must—
(i) Have an individual lock for each
latch;
(ii) Have the lock located as close as
practicable to the latch; and
(iii) Be designed so that, during pres-
surized flight, no single failure in the
locking system would prevent the
locks from restraining the latches nec-
essary to secure the door.
(4) Each door for which the initial
opening movement is inward, and
unlatching of the door could result in a
hazard, must have a locking means to
prevent the latches from becoming dis-
engaged. The locking means must en-
sure sufficient latching to prevent
opening of the door even with a single
failure of the latching mechanism.
(5) It must not be possible to position
the lock in the locked position if the
latch and the latching mechanism are
not in the latched position.
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