ED Decision 2013/010/R
(a) Each
compartment must be constructed and supported so that it can resist any
vibration, inertia, and air load to which it may be subjected in operation.
(b) Each
compartment must meet the drainage and ventilation requirements of CS 25J1187.
(c) Reserved
(d) Each
part of the compartment subject to high temperatures due to its nearness to
exhaust system parts or exhaust gas impingement must be fireproof.
(e) Each
aeroplane must:
(1) Be designed and constructed so that no
fire originating in any APU fire zone can enter, either through openings or by
burning through external skin, any other zone or region where it would create
additional hazards,
(2) Meet sub-paragraph (e)(1) of this
paragraph with the landing gear retracted (if applicable), and
(3) Have APU compartment external skins, in
areas subject to flame if a fire starts in an APU fire zone, complying with
the following:
(i) For
in-flight operations, APU compartment external skins must be fireproof in the
complete concerned areas, and
(ii) For
ground operations, APU compartment external skins must be:
(a) Fireproof
in the portions of the concerned areas where a skin burn through would affect
critical areas of the aeroplane, and
(b) Fire-resistant or compliant with subparagraph (e)(1) of this paragraph in the remaining portions of the concerned areas.
(See AMC 25.1193(e))
[Amdt 25/1]
[Amdt 25/13]
Loading collections...