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(3) for Helicopters, Section II, para 4.7.4 to 4.7.6 of ICAO
Annex 6, Part III International Operations – Helicopters,
as applicable.
For these purposes, the whole of Australia is a designated
area.
3.2 Australian aircraft (except exempted aircraft) are required to be
fitted with or to carry an ELT which meets the requirements of CAR
252A. Pilots should monitor 121.5MHZ before engine start and
after shutdown. Reception of an ELT transmission must be
reported to ATS or the RCC immediately. Domestic flights are
required to carry survival radio equipment in accordance with CAO
20.11.
4. AIRBORNE WEATHER RADAR
4.1 IFR RPT and CHTR aircraft which are required to be crewed by
two or more pilots must be fitted with an approved airborne
weather radar system. Unpressurised turbine engined aircraft
with a maximum take-off weight of not greater than 5,700KG and
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unpressurised piston engined aircraft are exempt from this
requirement.
4.2 Serviceability of Airborne Weather Radar
4.2.1 An aircraft which is required to be fitted with an airborne weather
radar system must not depart if the radar is unserviceable and
available forecasts indicate probability of thunderstorms or cloud
formations associated with severe turbulence anywhere along the
route to be flown, including the route to a planned alternate.
4.2.2 An aircraft which is required to be fitted with an airborne weather
radar system which becomes unserviceable during a flight may
continue that flight so long as the aircraft avoids penetration of any
cloud formation likely to be associated with severe turbulence.
5. GROUND PROXIMITY WARNING SYSTEM (GPWS)
5.1 A turbine engined aeroplane that:
a. has a maximum take-off weight of more than 15,000KG, or is
carrying 10 or more passengers; and
b. is engaged in regular public transport, or charter operations;
must not be operated under the Instrument Flight Rules unless it is
fitted with an approved and serviceable GPWS.
5.2 An approved and serviceable GPWS must:
a. have a predictive terrain hazard warning function; or
b. if CAO 20.18 para 9.1CA applies, meet the requirements of
CAO 108.36.
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6. SECONDARY SURVEILLANCE RADAR (SSR)
TRANSPONDERS
6.1 Aircraft Requirements
6.1.1 All aircraft must be fitted with an operable Mode A and Mode C
SSR transponder for operations within classes A, B and C
airspace and any class of airspace at or above 10,000FT AMSL.
Aircraft operating in GAAP control zones are exempted from this
requirement.
6.1.2 All aircraft, except aircraft operating to the VFR which are not fitted
with an engine driven electrical system capable of continuously
powering a transponder, must be fitted with a serviceable Mode
A/C or Mode S SSR transponder when operating in Class E
airspace.
Note 1: Mode C operation requires the provision of pressure
altitude information to the transponder equipment.
Note 2: Procedures for operational use of SSR transponders and
transponder codes are detailed at ENR 1.6 Section 8.
6.2 SSR Transponder Exemptions
6.2.1 General exemptions against the requirement for carriage of SSR
transponders are in force for aircraft certified without an
engine-driven electrical system; eg, balloons, gliders and antique
aircraft.
6.2.2 Specific ATC exemptions against the requirement, for carriage of
SSR transponders, for the portions of flights subject to a
clearance, may be available subject to agreement with the
relevant ATC unit as follows:
a. For operation of an aircraft with an operating transponder, but
without operating automatic pressure altitude reporting
equipment having a Mode C capability, the request may be
made at any time.
b. For operation of an aircraft with an inoperative transponder to
the airport of ultimate destination, including any intermediate
stops, or to proceed to a place where suitable repairs can be
made or both, the request may be made at any time.
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c. For operation of an aircraft that is not equipped with a
transponder, the request must be made at least one (1) hour
before the proposed operation.
7. TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM
(TCAS)
7.1 Aircraft fitted with a serviceable ACAS/TCAS, and with a crew
trained in its use, are permitted to operate that system while in
Australian airspace. All turbine-powered commercial transport
aeroplanes certified to carry more than 30 passengers, or which
　
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