CS 26.150 Compartment
interiors
Compliance
with point 26.150 of Part-26 is demonstrated
by complying with CS 25.853 and Appendix F or equivalent, CS 25.853(e) or
equivalent and CS 25.791 or equivalent or with the following:
For each
compartment occupied by the crew or passengers the following apply:
(a) Upon any major replacement of any
individual group of components as specified in Appendix
F, Part I,
sub-paragraph (a)(1)(i), such as interior ceiling panels, wall panels, etc.,
this individual group of components complies with Appendix
F, Part I, of this
CS-26. (See GM1
26.150(a))
(b) Seat cushions, except those on flight crew
member seats, on large aeroplanes, type certificated after 1 January 1958,
comply with the fire protection specifications of Appendix
F, Part II.
(c) (1) Heat release (other than for lavatory
interiors or flight deck), for interior ceiling and wall panels (other than
lighting lenses), partitions, and the outer surfaces of galleys, large
cabinets and stowage compartments (other than underseat stowage compartments
and compartments for stowing small items, such as magazines and maps), in
large aeroplanes which had their initial Certificate of Airworthiness issued
on or after 20 August 1988, but prior to 20 August 1990, and having a MOPSC of
more than 19, comply with the heat release rate testing provisions of Appendix
F Part IV, except
that the total heat release over the first two minutes of sample exposure does
not exceed 100 kilowatt-minutes per square metre, and the peak heat release
rate does not exceed 100 kilowatts per square metre.
(2) Heat release and smoke density (other than
for lavatory interiors or flight deck) for interior ceiling and wall panels
(other than lighting lenses), partitions, and the outer surfaces of galleys,
large cabinets and stowage compartments (other than underseat stowage
compartments and compartments for stowing small items, such as magazines and
maps), in large aeroplanes, having a MOPSC of more than 19, which had their
initial Certificate of Airworthiness issued on or after 20 August 1990, comply
with the heat release and smoke density specifications of Appendix F Parts IV and V. (See GM1 26.150(c))
(d) Large aeroplanes having a MOPSC of more
than 19, Type Certificated after 1 January 1958 upon the first substantially
complete replacement of the cabin interior components, (i.e. interior ceiling
and wall panels (other than lighting lenses), partitions, and the outer
surfaces of galleys, large cabinets and stowage compartments (other than
underseat stowage compartments and compartments for stowing small items, such
as magazines and maps)), comply with the heat release and smoke density
specifications of Appendix F Parts IV and V. (See GM1 26.150(d))
(e) Smoking prohibition is indicated by a
placard so stating.
(f) Each disposal receptacle for towels,
paper or waste is fully enclosed and constructed of materials adequate in
resistance to fire such that any fire likely to occur in it under normal use
is contained. The ability of the disposal receptacle to contain those fires
under all probable conditions of wear, misalignment, and ventilation expected
in service is demonstrated by test unless appropriate maintenance tasks are
put in place to ensure that excess wear or misalignment are quickly repaired.
A placard containing the legible words or symbology indicating ‘No Cigarette
Disposal’ is located on or near each disposal receptacle door.
[Issue:
26/3]
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