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recorder system shall be operated continuously from the moment when the
aircraft commences to taxi under its own power for the purpose of flight until
the conclusion of taxiing after landing.
6.4 Where an aircraft is required to be so equipped by this section, the cockpit
voice recorder system shall be operated continuously from the start of the use
of the check list before starting engines for the purpose of flight until
completion of the final check list at the termination of the flight.
6.5 Where an aircraft is required to be so equipped by this section the operator
shall ensure that:
(a) the flight data recorder retains its last 25 hours of recording; and
(b) the cockpit voice recorder retains its last 30 minutes of recording; and
(c) data from the last 2 occasions on which the flight data recorder system
was calibrated from which the accuracy of the system can be determined
are preserved.
6.6 The operator of an aircraft which is required by this section to be equipped
with recorders shall take action to ensure that during ground maintenance
periods the recorders are not activated unless the maintenance is associated
with the flight data recording equipment or with the aircraft engines.
6.7 An aircraft required to be fitted with a flight data recorder system and/or a
cockpit voice recorder system may operate with an unserviceable recorder
system for a period of 21 days commencing on the day on which the system
was determined to be unserviceable providing that:
(a) the aircraft does not depart from an aerodrome where staff and equipment
are available to replace the unserviceable units; and
(b) where the aircraft is required to be fitted with both a flight data recorder
and cockpit voice recorder system, 1 system is serviceable; and
(c) the aircraft is not operating training or test flights.
7 ASSIGNED ALTITUDE INDICATOR AND ALTITUDE ALERTING SYSTEM
7.1 Piston engined aircraft and unpressurised turbine engine aircraft operating
above 15 000 feet in controlled airspace under Instrument Flight Rules (except
night V.M.C.) shall be equipped with an altitude alerting system.
7.2 Pressurised turbine engined aircraft operating in controlled airspace under
Instrument Flight Rules (except night V.M.C.) shall be equipped with an
altitude alerting system.
7.3 Unless equipped with an altitude alerting system, an aircraft operating in
controlled airspace under Instrument Flight Rules (except night V.M.C.) shall
be equipped with an assigned altitude indicator.
7.4 An altitude alerting system or an assigned altitude indicator shall be so
designed and located that:
(a) it can be readily adjusted for setting from each pilot seat; and
SECTION 20.18 -6-
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
(b) the assigned altitude/flight level display is clearly discernible by day and
night to all operating flight crew members whose duties involve
altitude/flight level assignment monitoring; and
(c) altitude/flight levels may be pre-selected unambiguously in increments
commensurate with levels at which the aircraft may be operated.
7.5 The assigned altitude indicator shall be demonstrated to the satisfaction of
CASA.
7.6 The altitude alerting system shall be demonstrated to the satisfaction of CASA
and be capable of:
(a) alerting the pilot upon approaching or departing from a pre-selected level
in both climb and descent by aural and/or visual signals in sufficient time
to establish level flight at the pre-selected level, except that altitude
alerting systems in aircraft first registered in Australia before 1 January
1983 need not alert the pilot when departing from a pre-selected altitude;
and
(b) providing the required signals from sea level to the highest operating
altitude approved for the aircraft in which it is installed; and
(c) being tested without separate equipment to determine proper operation of
the alerting signals; and
(d) accepting necessary barometric pressure settings in millibars if the system
or device operates on barometric pressure.
8 RADIATION INDICATOR
All aeroplanes intended to be operated above 49 000 feet shall carry equipment
to measure and indicate continuously the dose rate of total cosmic radiation
being received (i.e. the total of ionizing and neutron radiation of galactic and
solar origin) and the cumulative dose on each flight. The display unit shall be
readily visible to a flight crew member.
9 GROUND PROXIMITY WARNING SYSTEM
9.1 Subject to paragraphs 9.1A and 9.1C, a turbine engined aeroplane that:
(a) has a maximum take-off weight of more than 15 000 kg or is carrying 10
or more passengers; and
(b) is engaged in regular public transport, or charter, operations;
　
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