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In the case of a non-RPT aircraft, RPT aircraft engaged in cargoonly
operations, and RPT aircraft below 3500KG MTOW, where
the alternate aerodrome is served by PAL, there is no requirement
for a responsible person on the ground to be in attendance, but the
aircraft must be equipped with:
a. dual VHF; or
b. single VHF and HF communications and carries 30 minutes
holding fuel to allow for the alerting of ground staff in the event
of a failure of the aircraft’s VHF communication.
72.4.5 The alternate requirements of paras 72.4.1 to 72.4.4 inclusive
need not be applied if the aircraft carries holding fuel for first light
plus 10 minutes at the destination.
72.4.6 An alternate aerodrome nominated in accordance with the requirements
in paras 72.4.2 and 72.4.3 need not have standby
power or standby portable runway lighting.
72.4.7 A responsible person under para 72.4.2 is one who has been instructed
in, and is competent to display, the standard runway lighting
with portable lights.
72.4.8 Partial Runway Lighting Failure. At a controlled aerodrome, in
the event of failure of one electrical circuit on a runway equipped
with interleaved circuitry lighting, pilots will be notified of a doubled
spacing of runway edge lights; ie, from 60M to 120M spacing.
When such a failure occurs at night, pilots must apply the following
requirements to an approach to land:
a. In VMC:
No restriction.
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b. In Less Than VMC:
The prevailing visibility must be equal to, or greater than, the
published minimum for the instrument approach procedure
being used for an aircraft’s arrival multiplied by a factor of 1.5.
73. SUITABILITY OF AERODROMES
73.1 General
A pilot in command must plan the flight to comply with the following
conditions for the use of an aerodrome, including an alternate
aerodrome:
a. an aircraft must not take off or land at a place not suitable for the
purpose under Regulation 92(1) and, if engaged on an international
flight, at a place not designated as an international aerodrome
or international alternate aerodrome;
b. an aircraft must not take off or land at an aerodrome at night
unless the following lighting is operating:
(1) for a PVT, AWK or CHTR aircraft: runway edge lighting,
threshold lighting, illuminated wind direction indicator,
obstacle lighting (when specified in local procedures);
(2) for an RPT aircraft: the aerodrome lighting specified in (1)
above plus taxiway lighting and apron floodlighting, all
lighting to be electric;
Note: In the event that an illuminated wind direction indicator is
not available, aircraft may continue to operate if wind velocity information
can be obtained from an approved observer.
c. an aircraft must not take off or land at an aerodrome when the
surface or strength of the manoeuvring area is unsuitable for
operations of the aircraft type.
Note: For emergency landings see para 73.4.1 Note 2.
73.2 Runway Width
73.2.1 Regulation 235A of the Civil Aviation Regulations specifies the
minimum runway width required for aeroplanes.
73.2.2 Interpretation:
a. An aeroplane’s reference field length is:
(1) in the case of an aeroplane to which section 20.7.1B of
the Civil Aviation Orders applies – the balanced field
length, or
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(2) in the case of any other aeroplane – the take-off distance
that the aeroplane requires for take-off in accordance
with sub-para b. below:
b. For the purposes of sub-para a. (1) and (2) above, the balanced
field length or take-off distance that an aeroplane requires for
take-off is the balanced field length or take-off distance that, according
to its flight manual, the aeroplane requires:
(i) on a level runway,
(ii) at maximum take-off weight,
(iii) in still air,
(iv)at sea level, and
(v) in standard atmospheric conditions.
c. An aeroplane’s code number is the number set out in column 1
of Table 1 opposite the range of distances in column 2 of the
Table that includes the aeroplane’s reference field length.
d. To work out an aeroplane’s code letter:
(1) determine its wing span and outer main gear wheel span;
and
(2) then determine:
(i) which letter in column 3 of Table 1 is opposite the
range of wing spans in column 4 of the Table that
includes the aeroplane’s wing span; and
(ii) which letter in column 3 of the Table is opposite the
range of outer main gear wheel spans in column 5 of
　
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