The satellite emergency position-indicating radio beacon
(EPIRB) should, in addition to meeting the requirements of the Radio
Regulations, the relevant ITU-R Recommendations, the relevant Inmarsat
technical requirements, and the general requirements set out in Resolution A.694(17), comply with the
following performance standards.
2.1 The satellite EPIRB should be capable of transmitting
a distress alert to a geostationary satellite.
2.2 The satellite EPIRB should be of an automatic
float-free type. The equipment should be reliable even under extreme
conditions.
2.3 The performance of the float-free arrangements
should be in accordance with the requirements of the performance standards
for float-free release and activation arrangements for emergency radio
equipment set out in Resolution A.662(16).
2.4 The satellite EPIRB should:
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.1 be fitted with adequate means to prevent inadvertent
activation;
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.2 be so designed that the electrical portions
are watertight at a depth of 10 m for at least 5 min. Consideration
should be given to a temperature variation of 45°C during transitions
from the mounted position to immersion. The harmful effects of a marine
environment, condensation and water leakage should not affect the
performance of the beacon;
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.3 be automatically activated after floating free;
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.4 be continuously provided with the ship's position
data for automatic inclusion in the distress message when activated;
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.5 be equipped with a search and rescue radar
transponder unless integral facilities are included for automatic
position updating after activation;
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.6 be capable of manual activation and manual
deactivation;
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.7 be provided with means to indicate that signals
are being emitted;
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.8 be capable of floating upright in calm water
and have positive stability and sufficient buoyancy in all sea conditions;
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.9 be capable of being dropped into the water
without damage from a height of 20 m;
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.10 be capable of being tested without using the
satellite system to determine that the EPIRB is capable of operating
properly;
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.11 be of highly visible yellow/orange colour
and be fitted with retroreflective material;
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.12 be equipped with a buoyant captive lanyard
suitable for use as a tether, which should be so arranged as to prevent
its being trapped in the ship's structure when floating free;
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.13 be provided with a low duty cycle light (0.75
cd), active during darkness, to indicate its position to nearby survivors
and to rescue units;
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.14 not be unduly affected by seawater, or oil,
or both; and
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.15 be resistant to deterioration by prolonged
exposure to sunlight.
2.5 The battery should have sufficient capacity
to operate:
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.1 the distress alerting transmitter for 4 h in
accordance with Recommendation ITU-R M.632 or for at least 48 h if
integral facilities are included for automatic position updating;
and
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.2 any other facilities (e.g. SART and flashing
light) for at least 48 h.
2.6 The satellite EPIRB should be so designed
as to operate under any of the following environmental conditions:
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.1 ambient temperature of -20°C to +55°C;
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.2 icing;
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.3 relative wind speeds up to 100 knots; and
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.4 after stowage at temperature between -30°C
and +70°C.
2.7 The installed satellite EPIRB should:
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.1 have local manual activation, remote activation
may also be provided from the navigating bridge, while the device
is installed in the float-free mounting;
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.2 be capable, while mounted on board, of operating
properly over the range of shock and vibrations and other environmental
conditions normally encountered above deck on seagoing vessels; and
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.3 be designed to release itself and float free
before reaching a depth of 4 m at a list or trim of any angle.
2.8 Any connection to the EPIRB, e.g. for the
purpose of supply of data or power, should be corrosion-resistant
and protected against accidental disconnection.
3.1 When the satellite EPIRB is manually operated,
a distress alert should be initiated only by means of a dedicated
distress alert activator.
3.2 The dedicated activator should:
3.3 Manual distress alert initiation should require
at least two independent actions.
3.4 The satellite EPIRB should not be automatically
activated after being manually removed from the release mechanism.
In addition to the general requirements specified in Resolution A.694(17), the following should
be clearly indicated on the exterior of the equipment: