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7 CASA may, having regard to the type of helicopter, 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.
8 A gyro-magnetic type of remote indicating compass installed to meet the
requirements of subparagraph 1 (c) (ii) and 2 (c) (ii) of this Appendix may be
considered also to meet the requirement for a heading indicator specified in
subparagraph 1 (h) or 2 (h) of this Appendix, provided that such installation
complies with the power supply requirements of paragraph 4 of this Appendix.
9 CASA may, having regard to the type of helicopter, and the flight presentation,
response and acuity standard of the instrument concerned, approve the use of
attitude indicators which have a dial presentation of less than 5 inches, in lieu
of the indicators specified at paragraphs 1 (g), 2 (g) and 5 of this Appendix.
-21- SECTION 20.18
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
APPENDIX VIII
INSTRUMENTS REQUIRED FOR NIGHT V.M.C. FLIGHT IN
HELICOPTERS EXCEPT WHILE ENGAGED IN AGRICULTURAL
OPERATIONS
1 The flight and navigational instruments required are:
(a) an airspeed indicating system; and
(b) a sensitive pressure altimeter; 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; and
(e) an outside air temperature indicator; and
(f) an attitude indicator (artificial horizon); and
(i) standby attitude indicator; or
(ii) turn indicator; and
(g) a heading indicator (directional gyroscope); and
(h) a slip indicator; and
(i) a vertical speed indicator; and
(j) means of indicating whether the power supply to the gyroscopic
instruments is working satisfactorily.
2 For operations onto vessels or platforms at sea by night an instantaneous
vertical speed indicator is required in place of the vertical speed indicator
specified at paragraph 1 (i) of this Appendix.
3 The attitude indicator and standby attitude indicator or turn indicator as
specified in paragraph 1 (f) of this Appendix, shall have separate and
independent power sources.
4 A gyro-magnetic type of remote indicating compass installed to meet the
requirements of subparagraph 1 (c) (ii) of this Appendix may be considered
also to meet the requirement for a heading indicator specified in subparagraph
1 (g) of this Appendix, provided that such installation complies with the power
supply requirements of paragraph 3 of this Appendix.
SECTION 20.18 -22-
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
APPENDIX IX
INSTRUMENTS REQUIRED FOR HELICOPTERS ENGAGED IN NIGHT
V.M.C. AGRICULTURAL OPERATIONS
1 The flight and navigational instruments required are:
(a) an airspeed indicating system; and
(b) a sensitive pressure altimeter; 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; and
(e) an outside air temperature indicator; and
(f) an attitude indicator (artificial horizon); and
(g) a vertical speed indicator; and
(h) a slip indicator; and
(i) a means of indicating whether the power supply to the gyroscopic
instrument is working satisfactorily.
-23- SECTION 20.18
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
APPENDIX X
INSTRUMENTS REQUIRED FOR MANNED FREE BALLOONS AND HOT
AIR AIRSHIPS FOR FLIGHT BY DAY UNDER THE VISUAL FLIGHT
RULES
1 The flight and navigational instruments required for flight under the visual
flight rules by day are:
(a) an altimeter, with a readily adjustable pressure datum setting scale
graduated in hectopascals; and
(b) a timepiece, which may be carried on the person of the pilot, that is
accurate to and readable to the nearest minute for the duration of the
flight; and
(c) a vertical speed indicator; and
(d) in the case of a hot air airship that has a maximum permissible forward
airspeed less than that attainable with the engine(s) operating at full
power, an instrument capable of indicating when the maximum speed is
reached; and
(e) in the case of a hot manned free balloon or hot air airship, an envelope
temperature indicator; and
(f) in the case of a hot air manned free balloon or a hot air airship, a free air
temperature indicator or an air temperature indicator that provides
　
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