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available for use if an emergency occurs during the refuelling.
6 FUEL LOADING
6.1 The quantity of fuel to be loaded must be decided before hot refuelling is
commenced.
6.2 A closed or open refuelling system may be used for hot refuelling.
6.3 If an open system of refuelling is used, there must be a means of quickly
cutting off the fuel supply at the point of entry into the fuel tank of the
aeroplane.
6.4 Before the aeroplane’s fuel filler cap is removed, the refuelling equipment and
the aeroplane must be earthed and connected so as to ensure they are of the
same electrical potential.
7 RADIO TRANSMISSIONS
7.1 While hot refuelling is taking place, radio transmissions from the aeroplane
must be restricted to the greatest extent practicable.
7.2 While hot refuelling is taking place, an HF transmitter or radar equipment on
the aeroplane must not be operated.
Issue 2: 8 December 2004
Amdt No. 215
SECTION 20.10.1 -4-
Issue 2
8 INSPECTION AND TESTING OF FUEL SYSTEM
8.1 The operator of an aeroplane engaged in aerial work operations must ensure to
the greatest extent practicable that, on completion of each hot refuelling of the
aeroplane, the pilot in command inspects and tests the aeroplane’s fuel system
for the presence of water.
8.2 The pilot in command of an aeroplane, engaged in aerial work operations or
private operations, that has been hot refuelled must, on completion of each hot
refuelling of the aeroplane, inspect and test the aeroplane’s fuel system for the
presence of water.
8.3 Paragraphs 8.1 and 8.2 do not apply to an aeroplane engaged in aerial work
operations:
(a) if the aeroplane has, for a continuous period of not more than 5 hours time
in service, been engaged in operations during which hot refuelling has
taken place; and
(b) if:
(i) the fuel used by the aeroplane is supplied by a person:
(A) who has a fuel quality audit program; and
(B) whose regular audit reports are checked by the operator; or
(ii) in the case where the fuel used by the aeroplane is supplied by a
person who does not have a fuel quality audit program — the
operator has a system for monitoring the quality of the fuel used by
the aeroplane.
8.4 Paragraph 8.2 does not apply to an aeroplane engaged in private operations if
the requirements set out in subparagraphs 8.3 (a) and (b) are satisfied and
approval in writing is given by CASA.
Issue 2: 8 December 2004
Amdt No. 215
CIVIL AVIATION ORDERS
PART 20
SECTION 20.11
Issue 11
EMERGENCY AND LIFE SAVING EQUIPMENT AND PASSENGER
CONTROL IN EMERGENCIES
SUBSECTIONS
1 Application
2 Definitions
3 Maintenance of emergency and
lifesaving equipment
5 Flotation equipment for
overwater flights
6 Signalling equipment
6A Portable megaphones
7 Survival equipment
8 Accessories for water
operations
9 Illumination of emergency exits
10 Emergency procedures
11 Assignment of emergency
duties
12 Crew member proficiency in
the execution of emergency
procedures
13 Cabin attendants
14 Briefing of passengers
15 Demonstration of emergency
evacuation procedures
Appendixes II, III and IV
1 APPLICATION
This section applies to all Australian registered aircraft, except where
otherwise specified in these Orders.
2 DEFINITIONS
In this section, unless a contrary intention appears:
handicapped person means a person requiring special attention because
illness, injury, age, congenital malfunction, or other temporary or permanent
incapacity or disability makes that person unable without special facilities or
assistance to utilise air transport facilities and services as effectively as persons
who are not so affected.
land aircraft means all aircraft other than amphibious aircraft when operating
on water, helicopters equipped with fixed flotation equipment when operating
on water, seaplanes and flying boats.
portable megaphone means a portable battery-powered megaphone that meets
the performance standards set out in paragraph 6A.5.
Issue 11: 8 December 2004
Amdt No. 216
SECTION 20.11 -2-
Issue 11
3 MAINTENANCE OF EMERGENCY AND LIFESAVING EQUIPMENT
An operator must ensure that emergency and lifesaving equipment, carried or
installed in an aircraft to meet the requirements of this section, is maintained in
such condition that it will satisfactorily perform its design function.
5 FLOTATION EQUIPMENT FOR OVERWATER FLIGHTS
5.1 Life Jackets
5.1.1 Aircraft shall be equipped with 1 life jacket for each occupant when the aircraft
　
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