Previous Page | Page 450 | Next Page |
441
Federal Aviation Administration, DOT
§ 25.783
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25–72, 55 FR 29779, July 20, 1990]
§ 25.783
Fuselage doors.
(a)
General. This section applies to fu-
selage doors, which includes all doors,
hatches, openable windows, access pan-
els, covers, etc., on the exterior of the
fuselage that do not require the use of
tools to open or close. This also applies
to each door or hatch through a pres-
sure bulkhead, including any bulkhead
that is specifically designed to func-
tion as a secondary bulkhead under the
prescribed failure conditions of part 25.
These doors must meet the require-
ments of this section, taking into ac-
count both pressurized and unpres-
surized flight, and must be designed as
follows:
(1) Each door must have means to
safeguard against opening in flight as a
result of mechanical failure, or failure
of any single structural element.
VerDate Mar<15>2010
10:12 Mar 18, 2014
Jkt 232046
PO 00000
Frm 00451
Fmt 8010
Sfmt 8010
Y:\SGML\232046.XXX
232046
EC28SE91.048</GPH>
pmangrum on DSK3VPTVN1PROD with CFR
Previous Page | Page 450 | Next Page |