ED
Decision 2019/013/R
(See AMC
25.831)
(a) Under normal operating conditions and in
the event of any probable failure conditions of any system that would
adversely affect the ventilating air, the ventilation system must be designed
to provide a sufficient amount of uncontaminated air to enable the crew
members to perform their duties without undue discomfort or fatigue, and to
provide reasonable passenger comfort. For normal operating conditions, the
ventilation system must be designed to provide each occupant with an airflow
that contains at least 0.25 Kg (0.55 lb) of fresh air per minute. (See
AMC 25.831(a).)
(b) Crew and passenger compartment air must be
free from harmful or hazardous concentrations of gases or vapours. In meeting
this requirement, the following apply:
(1) Carbon monoxide concentrations in excess
of one part in 20 000 parts of air are considered hazardous. For test
purposes, any acceptable carbon monoxide detection method may be used.
(2) Carbon dioxide concentration during flight
must be shown not to exceed 0·5% by volume (sea level equivalent) in
compartments normally occupied by passengers or crewmembers. For the purpose
of this subparagraph, “sea level equivalent” refers to conditions of 25° C
(77° F) and 1 013·2 hPa (760 millimetres of mercury) pressure.
(c) There must be provisions made to ensure
that the conditions prescribed in sub-paragraph (b) of this paragraph are met
after reasonably probable failures or malfunctioning of the ventilating,
heating, pressurisation or other systems and equipment. (See AMC 25.831(c).)
(d) If accumulation of hazardous quantities of
smoke in the cockpit area is reasonably probable, smoke evacuation must be
readily accomplished, starting with full pressurisation and without
depressurising beyond safe limits.
(e) Except as provided in sub-paragraph (f) of
this paragraph, means must be provided to enable the occupants of the
following compartments and areas to control the temperature and quantity of
ventilating air supplied to their compartment or area independently of the
temperature and quantity of air supplied to other compartments and areas:
(1) The flight-crew compartment.
(2) Crew-member compartments and areas other
than the flight-crew compartment unless the crewmember compartment or area is
ventilated by air interchange with other compartments or areas under all
operating conditions.
(f) Means to enable the flight crew to
control the temperature and quantity of ventilating air supplied to the
flight-crew compartment independently of the temperature and quantity of
ventilating air supplied to other compartments are not required if all of the
following conditions are met:
(1) The total volume of the flight-crew and
passenger compartments is 22.65m3 (800 cubic ft) or less.
(2) The air inlets and passages for air to
flow between flight-crew and passenger compartments are arrange to provide
compartment temperatures within 2.8°C (5°F) of each other and adequate
ventilation to occupants in both compartments.
(3) The temperature and ventilation controls
are accessible to the flight crew.
[Amdt No:
25/18]
[Amdt
No: 25/23]
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