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ports of which 1 is used for the instruments specified above. Instruments
and equipment other than flight instruments provided for use by the pilot
in command, shall not be connected to the normal static system that
operates the instruments of the pilot in command;
(b) for aeroplanes not above 5 700 kg maximum take-off weight, the
instruments specified in subparagraphs 1 (a), (b), (e) and (l) of this
Appendix shall be capable of being connected to either a normal or
alternate static source but not both sources simultaneously. Alternatively
the aeroplane may be fitted with a balanced pair of flush static ports.
3 The instruments specified in subparagraphs 1 (g), (h) and (i) of this Appendix
shall have duplicated sources of power supply.
4 CASA may, having regard to the type of aeroplane, approve an attitude
indicator incorporated in an automatic pilot system being 1 of the 2 attitude
indicators required by subparagraph 1 (g) of this Appendix.
5 A gyro-magnetic type of remote indicating compass installed to meet the
requirements of subparagraph 1 (c) (ii) of this Appendix may also be
considered to meet the requirement for a heading indicator specified in
subparagraph 1 (h) of this Appendix, provided that it has a duplicated power
supply.
6 For Visual Flight Rules flight, the following instruments may be unserviceable:
(a) the attitude indicator required by paragraph 1 (k);
(b) 1 of the attitude indicators required by paragraph 1 (g) provided that the
attitude indicator required by paragraph 1 (k) is serviceable or an attitude
indicator has been provided to meet the requirements of paragraph 1 (i)
and is serviceable;
(c) the turn and slip indicator or slip indicator and attitude indicator required
by paragraph 1 (i).
SECTION 20.18 -14-
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
APPENDIX III
INSTRUMENTS REQUIRED FOR AEROPLANES WITH A MAXIMUM
TAKE-OFF WEIGHT NOT GREATER THAN 5 700 KG ENGAGED
IN CHARTER OPERATIONS UNDER THE INSTRUMENT
FLIGHT RULES (EXCEPT NIGHT V.M.C.)
EXCLUDING FREIGHT ONLY CHARTER OPERATIONS
1 The flight and navigation instruments required are:
(a) an airspeed indicating system with means of preventing malfunctioning
due to either condensation or icing; and
(b) 2 sensitive pressure altimeters; and
(c) (i) a direct reading magnetic compass; or
(ii) a remote indicating compass and a standby direct reading magnetic
compass; and
(d) an accurate timepiece indicating the time in hours, minutes and seconds;
and
(e) a rate of climb and descent indicator (vertical speed indicator); and
(f) an outside air temperature indicator; and
(g) 2 attitude indicators (artificial horizons); and
(h) a heading indicator (directional gyroscope or equivalent approved by
CASA); and
(i) a turn and slip indicator except that only a slip indicator is required when a
third attitude indicator usable through flight attitude of 360 degrees pitch
and roll is installed; and
(j) a means of indicating whether the power supply to the gyroscopic
instruments is working satisfactorily; and
(k) in turbo-jet aeroplanes with operating limitations expressed in terms of
Mach number, a Mach number indicator (Machmeter).
2 The instruments specified in 1 (a), (b), (e) and (k) of this Appendix shall be
capable of being connected to either a normal or alternate static source but not
both sources simultaneously. Alternatively, they may be connected to a
balanced pair of flush static ports.
3 The instruments specified in 1 (g), (h) and (i) of this Appendix shall have
duplicated sources of power supply.
4 CASA may, having regard to the type of aeroplane, approve an attitude
indicator incorporated in an automatic pilot system as being 1 of the 2 attitude
indicators required by subparagraph 1 (g) of this Appendix.
-15- SECTION 20.18
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
5 A gyro-magnetic type of remote indicating compass installed to meet the
requirements of subparagraph 1 (c) (ii) of this Appendix may also be
considered to meet the requirement for a heading indicator specified in
subparagraph 1 (h) of this Appendix, provided it has a duplicated power
supply.
SECTION 20.18 -16-
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
APPENDIX IV
INSTRUMENTS REQUIRED FOR AEROPLANES ENGAGED IN:
(i) AERIAL WORK AND PRIVATE OPERATIONS UNDER THE
INSTRUMENT FLIGHT RULES (INCLUDING NIGHT V.M.C.); AND
(ii) CHARTER OPERATIONS UNDER NIGHT V.M.C; AND
(iii) INSTRUMENT FLIGHT RULES FREIGHT ONLY CHARTER
OPERATIONS IN AEROPLANES WITH MAXIMUM TAKE-OFF
WEIGHT NOT GREATER THAN 5 700 KG.
　
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