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permissible to placard as unserviceable only the function(s) which are unserviceable.
10.3 The holder of an Air Operator’s Certificate authorising a regular public
transport operation must:
(a) have a minimum equipment list or lists for the aircraft used to conduct
those operations; and
(b) include each list in the operations manual for the aircraft to which that list
applies.
10.4 The holder of an Air Operator’s Certificate authorising charter operations:
(a) may have a minimum equipment list or lists for the aircraft used to
conduct those operations; and
(b) must include each list in the operations manual for the aircraft to which
that list applies.
-11- SECTION 20.18
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
APPENDIX I
INSTRUMENTS REQUIRED FOR FLIGHT UNDER VISUAL FLIGHT
RULES
(Limited to aircraft specified in subsection 3 paragraph 3.1)
1 The flight and navigational instruments required for flights under the Visual
Flight Rules are:
(a) an airspeed indicating system; and
(b) an altimeter, with a readily adjustable pressure datum setting scale
graduated in millibars; 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.
This may be carried on the person of the pilot or navigator.
2 In addition to the instruments required under paragraph 1, aircraft, other than
helicopters, engaged in charter or aerial work operations and operating under
the Visual Flight Rules, shall be equipped with:
(a) a turn and slip indicator (agricultural aeroplanes may be equipped with a
slip indicator only); and
(b) an outside air temperature indicator when operating from an aerodrome at
which ambient air temperature is not available from ground-based
instruments.
SECTION 20.18 -12-
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
APPENDIX II
INSTRUMENTS REQUIRED FOR:
(i) AEROPLANES ENGAGED IN REGULAR PUBLIC TRANSPORT
OPERATIONS; AND
(ii) AEROPLANES ENGAGED IN CHARTER OPERATIONS WHICH
HAVE A MAXIMUM TAKE-OFF WEIGHT GREATER THAN
5 700 KG
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 attitudes of 360 degrees of
pitch and roll is installed in accordance with subparagraph (k) of this
Appendix; and
(j) a means of indicating whether the power supply to those instruments
requiring power is working satisfactorily; and
(k) in turbo-jet aeroplanes having a maximum take-off weight greater than
5 700 kg and in turbo-prop aeroplanes having a maximum take-off weight
greater than 18 000 kg a third attitude indicator which:
(i) is powered from a source independent of the electrical generating
system; and
(ii) continues to provide reliable indications for a minimum of 30
minutes after total failure of the electrical generating system; and
(iii) is operative without selection after total failure of the electrical
generating system; and
(iv) is located on the instrument panel in a position which will make it
plainly visible to and usable by any pilot at his station; and
(v) is appropriately lighted during all phases of operation; and
(l) in turbo-jet aeroplanes with operating limitations expressed in terms of
Mach number, a Mach number indicator (Machmeter).
2 (a) For aeroplanes above 5 700 kg maximum take-off weight, the instruments
used by the pilot in command and which are specified in subparagraphs
-13- SECTION 20.18
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
1 (a), (b), (e) and (l) of this Appendix shall be capable of being connected
either to a normal or an alternate static source but not both sources
simultaneously. Alternatively the aeroplane may be fitted with 2
independent static sources each consisting of a balanced pair of flush static
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