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6.2 All aeroplanes operated as VFR flights
6.2.1 All aeroplanes when operated as VFR flights shall
be equipped with:
a) a magnetic compass;
b) an accurate timepiece indicating the time in hours,
minutes and seconds;
c) a sensitive pressure altimeter;
d) an airspeed indicator; and
ej such additional instruments or equipment as may be
prescribed by the appropriate authority.
6.2.2 Recommendation.- VFR flights which are operated
us controlled flights should be equipped in accordance
with 6.6.
6.3 All aeroplanes on flights over water
6.3.1 Seaplanes
A11 seaplanes for all flights shall be equipped with:
a) one life jacket, or equivalent individual floatation device,
for each person on board, stowed in a position readily
accessible from his seat or berth:
Part I1
b) equipment for making the sound signals prescribed in the
International Regulations for Preventing Collisions at
Sea, where applicable;
c) one anchor;
d) one sea anchor (drogue), when necessary to assist in
manoeuvring.
Note.- "Seaplanes" includes amphibiuns operated as
seaplanes.
6.3.2 Landplanes
Recommendation.- All single-engined ladplufies when
flying en route over water beyond gliding distance from the
shore should cary one life jacket or equivalent individual
floatation device far each person on board, stowed in a
positiort easily accessible from die seat or berth of the person
for whose use if is provided.
Note.- "Landplanes" includes amphibians operated as
landphnes.
6.3.3 All aeroplanes on extended flights over water
All aeroplanes when operated on extended flights over water
shall be equipped with:
/
3 cm Not over 2 m
x.
-. -
MARKING OF BREAK-IN POINTS (see 6.1.4)
Chapter 6 Annex 6 - Operation of Aircraj?
a) when the aeroplane may be over water at a distance of
more than 93 krn (50 NM) away from land suitable for
making an emergency landing:
6.5.3 Aeroplanes for which the individual
certificate of airworthiness is first
issued before 1 Januaty 1990
-one life jacket or equivalent individual floatation Recommendation.- Pressurized aeroplanes intended to
device for each person on board. stowed in a position be operated at flight altitudes at which the atmospheric
easily accessible from the seat or berth of the person pressure is less than 376 hPa should be equipped with a
for whose use it is provided; device to provide positive warning to the flight crew of any
dangerous loss of pressurization.
b) when over water away from land suitable for making an
emergency landing at a distance of more than 185 km
(100 NM), in the case of single-engined aeroplanes, and
more than 370 km (200NM), in the case of multi-engined
aeroplanes capable of continuing flight with one engine
inoperativ w
6.6 All aeroplanes operated in accordance
with the instrument flight rules
All aeroplanes when operated in accordance with the
instrument flight rules or when the aeroplane cannot be
1) life-saving rafts in sufficient numbers to carry all maintained in a desired attitude without reference to one or
persons on board, stowed so as to facilitate their
more flight instruments, shall be equipped with:
ready use in emergency, provided with such lifesaving
equipment -including means of sustaining a) a magnetic compass;
life as is appropriate to the flight to be undertaken;
and b) an accurate timepiece indicating the time in hours,
minutes and seconds;
2) equipment for making the pyrotechnical distress
signals described in Annex 2. C) a sensitive pressure altimeter;
Note.-Due to the long history of misreadings, the use
of drum-pointer altimeters is not recommended.
6.4 All aeroplanes on flights over
designated land areas
d) an airspeed indicating system with a means of preventing
malfunctioning due to either condensation or icing;
Aeroplanes when operated across land areas which have been e) a turn and slip indicator;
designated by the State concerned as areas in which search and
rescue would be especially difficult, shall be equipped with f) an attitude indicator (artificial horizon);
such signalling devices and life-saving equipment (including
means of sustaining life) as may be appropriate to the area g) a heading indicator (directional gyroscope);
overflown.
Note.- The requiremenrs of e), fl and g) above, may
be met by combi~tionso f instruments or by integrated
flight director systems provided that the safeguards
against total .failure, inherent in the three separate
65 All aeroplanes on high altitude [lights instruments, are retained.
　
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