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1 The flight and navigational instruments required are:
(a) an airspeed indicating system; and
(b) a sensitive pressure altimeter; and
(c) (i) 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,
except that this may be omitted if it is carried on the person of the pilot or
navigator; and
(e) a rate of climb and descent indicator (vertical speed indicator) for other
than night V.M.C. flights; and
(f) an outside air temperature indicator; and
(g) an attitude indicator (artificial horizon); and
(h) a heading indicator (directional gyroscope); and
(i) a turn and slip indicator except that only a slip indicator is required when a
second attitude indicator usable through flight attitudes of 360 degrees of
pitch and roll is installed; and
(j) means of indicating whether the power supply to the gyroscopic
instruments is working satisfactorily; and
(k) except for aeroplanes engaged in night V.M.C. flights, means of
preventing malfunctioning due to either condensation or icing of at least 1
airspeed indicating system.
2 The instruments specified in subparagraphs 1 (a), (b), (e) and (k) of this
Appendix shall be capable of being connected to either a normal or an alternate
static source but not both sources simultaneously. Alternatively, they may be
connected to a balanced pair of flush static ports.
3 Except for aeroplanes engaged in night V.M.C. private and aerial work
operations the instruments specified in subparagraphs 1 (g), (h) and (i) of this
Appendix shall have duplicated sources of power supply unless the turn and
slip indicator or the second attitude indicator specified in subparagraph 1 (i)
has a source of power independent of the power operating other gyroscopic
instruments.
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 (h) of this Appendix, provided that such installation complies with the power
supply requirements of paragraph 3 of this Appendix.
-17- SECTION 20.18
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
APPENDIX V
ELECTRIC LIGHTING EQUIPMENT FLIGHT UNDER THE INSTRUMENT
FLIGHT RULES AT NIGHT (INCLUDING NIGHT V.M.C.)
The electric lighting equipment is:
1 Instrument illumination
illumination for all instruments and equipment, used by the flight crew, that are
essential for the safe operation of the aircraft. The illumination shall be such
that:
(a) all illuminated items are easily readable or discernible, as applicable; and
(b) its direct or reflected rays are shielded from the pilot’s eyes; and
(c) its power supply is so arranged that in the event of the failure of the
normal source of power, an alternative source is immediately available;
and
(d) it emanates from fixed installations.
2 Intensity control
means of controlling the intensity of the illumination of instrument lights,
unless it can be demonstrated that non-dimmed instrument lights are
satisfactory under all conditions of flight likely to be encountered.
3 Landing lights
2 landing lights except that, in accordance with the provisions of regulation
308 of the Regulations, aircraft engaged in private and aerial work operations
and charter operations not carrying passengers for hire and reward are
exempted from this requirement provided that 1 landing light is fitted.
Note: A single lamp having 2 separately energised filaments may be approved as meeting the
requirement for 2 landing lights.
4 Passenger compartment lights
lights in all passenger compartments.
5 Pilots’ compartment lights
means of lighting the pilots’ compartment to provide illumination adequate for
the study of maps and the reading of flight documents.
6 Position and anti-collision lights
equipment for displaying the lights prescribed in regulation 196 of the
Regulations.
Note: In accordance of the provision of subregulation 195 (1) of the Regulations, position and
anti-collision lights shall be displayed at night and in conditions of poor visibility.
7 Emergency lighting
emergency lighting as specified in (Civil Aviation Regulations 1998) Part 39-
105 AD/General/4B Amdt 3 and a shock-proof electric torch for each crew
member at the crew member station.
SECTION 20.18 -18-
Issue 9
Issue 9: 8 December 2004
Amdt No. 222
APPENDIX VI
INSTRUMENTS REQUIRED FOR VISUAL FLIGHT RULES
　
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