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a) when flying over water and at a distance of more than
93 km (50 NM) away from the shore, in the case of
landplanes operated in accordance with 5.2.9 or 5.2.10;
b) when flying en route over water beyond gliding distance
from the shore, in the case of all other landplanes; and
c) when taking off or landing at an aerodrome where, in
the opinion of the State of the Operator, the take-off or
approach path is so disposed over water that in the event
of a mishap there would be a likelihood of a ditching.
Chapter 6 Annex 6 — Operation of Aircraft
6-7 12/31/111/0/016
No. 30
6.5.2.2 The equipment referred to in 6.5.2.1 shall comprise
one life jacket or equivalent individual flotation device
for each person on board, stowed in a position easily accessible
from the seat or berth of the person for whose use it is
provided.
Note.— “Landplanes” includes amphibians operated as
landplanes.
6.5.3 All aeroplanes on long-range
over-water flights
6.5.3.1 In addition to the equipment prescribed in 6.5.1 or
6.5.2 whichever is applicable, the following equipment shall
be installed in all aeroplanes when used over routes on which
the aeroplane may be over water and at more than a distance
corresponding to 120 minutes at cruising speed or 740 km
(400 NM), whichever is the lesser, away from land suitable for
making an emergency landing in the case of aircraft operated
in accordance with 5.2.9 or 5.2.10, and 30 minutes or 185 km
(100 NM), whichever is the lesser, for all other aeroplanes:
a) life-saving rafts in sufficient numbers to carry all persons
on board, stowed so as to facilitate their ready use
in emergency, provided with such life-saving equipment
including means of sustaining life as is appropriate to
the flight to be undertaken; and
b) equipment for making the pyrotechnical distress signals
described in Annex 2.
6.5.3.2 Each life jacket and equivalent individual flotation
device, when carried in accordance with 6.5.1 a), 6.5.2.1 and
6.5.2.2, shall be equipped with a means of electric illumination
for the purpose of facilitating the location of persons, except
where the requirement of 6.5.2.1 c) is met by the provision of
individual flotation devices other than life jackets.
6.6 All aeroplanes on flights over
designated land areas
Aeroplanes, when operated across land areas which have been
designated by the State concerned as areas in which search and
rescue would be especially difficult, shall be equipped with
such signalling devices and life-saving equipment (including
means of sustaining life) as may be appropriate to the area
overflown.
6.7 All aeroplanes on high altitude flights
Note.— Approximate altitude in the Standard Atmosphere
corresponding to the value of absolute pressure used in this
text is as follows:
Absolute pressure Metres Feet
700 hPa 3 000 10 000
620 hPa 4 000 13 000
376 hPa 7 600 25 000
6.7.1 An aeroplane intended to be operated at flight altitudes
at which the atmospheric pressure is less than 700 hPa in
personnel compartments shall be equipped with oxygen storage
and dispensing apparatus capable of storing and dispensing the
oxygen supplies required in 4.3.8.1.
6.7.2 An aeroplane intended to be operated at flight altitudes
at which the atmospheric pressure is less than 700 hPa
but which is provided with means of maintaining pressures
greater than 700 hPa in personnel compartments shall be provided
with oxygen storage and dispensing apparatus capable of
storing and dispensing the oxygen supplies required in 4.3.8.2.
6.7.3 Pressurized aeroplanes newly introduced into service
on or after 1 July 1962 and intended to be operated at flight
altitudes at which the atmospheric pressure is less than 376 hPa
shall be equipped with a device to provide positive warning to
the pilot of any dangerous loss of pressurization.
6.7.4 Recommendation.— Pressurized aeroplanes introduced
into service before 1 July 1962 and intended to be
operated at flight altitudes at which the atmospheric pressure
is less than 376 hPa should be equipped with a device to
provide positive warning to the pilot of any dangerous loss of
pressurization.
6.7.5 An aeroplane intended to be operated at flight
altitudes at which the atmospheric pressure is less than
376 hPa, or which, if operated at flight altitudes at which the
atmospheric pressure is more than 376 hPa, cannot descend
safely within four minutes to a flight altitude at which the
atmospheric pressure is equal to 620 hPa and for which the
individual certificate of airworthiness is first issued on or after
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