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(iii) supervise any necessary evacuation of the aircraft;
(d) while the fuel is loaded:
(i) the aircraft’s “fasten seat belt” signs are turned off; and
(ii) the aircraft’s “no smoking” signs are turned on; and
(iii) the aircraft’s emergency lights (if any) are armed;
(e) while the fuel is loaded, there is at least 1 cabin attendant on duty in the
aircraft:
(i) for every 72 passengers on board the aircraft; or
(ii) for every passenger zone in the aircraft in which there are
passengers;
whichever is more;
Issue 7: 8 December 2004
Amdt No. 213
SECTION 20.9 -4-
Issue 7
(f) while the fuel is loaded, there is at least 1 cabin attendant on duty by at
least 1 exit door of each of the aircraft’s passenger zones in which there
are passengers;
(g) all cabin attendants who are on duty in the aircraft while the fuel is loaded:
(i) are prepared for an immediate evacuation; and
(ii) supervise the passengers during the loading; and
(iii) ensure that the aisles and exits are unobstructed during the loading;
(h) the areas outside the aircraft that would be used if the aircraft were
evacuated are kept clear while the fuel is loaded;
(i) the fuel is loaded using a system which gets the fuel from its container
into the aircraft’s fuel tank without exposing it to the air;
(k) if the aircraft’s engine is running — a member of the aircraft’s flight crew
is on duty on its flight deck;
(l) the operator’s operations manual sets out:
(i) the responsibilities of members of the operating crew who are on
duty in the aircraft while fuel is loaded; and
(ii) procedures for complying with the requirements of this paragraph.
4.2.3 Subject to paragraph 4.2.4, the operator of an aircraft with a maximum seating
capacity of less than 20 must ensure that fuel is not loaded on to the aircraft
while passengers are on board, or entering or leaving, the aircraft.
4.2.4 The operator of an aircraft with a maximum seating capacity of less than 20
may allow fuel that is not:
(a) avgas; or
(b) an aviation turbine grade which does not contain an anti-static additive;
to be loaded on to the aircraft while a passenger is on board if:
(c) the passenger’s medical condition is such that he or she cannot leave the
aircraft without assistance; and
(d) the conditions set out in paragraph 4.2.2 are satisfied.
4.2.5 If:
(a) fuel is being loaded onto an aircraft in accordance with paragraph 4.2.2 or
4.2.4; and
(b) either:
(i) fuel vapour is found inside the aircraft; or
(ii) for any other reason it is not safe to continue loading the fuel;
the aircraft’s operator must ensure that the loading of the fuel stops
immediately.
4.3 Aircraft Safety Precautions during Fuelling Operations
4.3.1 All engines in the aircraft, including any auxiliary power units, shall be
stopped with their ignition switches in the ‘OFF’ position, except where CASA
is satisfied that the operation of such an engine or auxiliary power unit will not
present a hazard and where a statement to that effect, together with any special
conditions for operation, is included in the aircraft Operations Manual.
Issue 7: 8 December 2004
Amdt No. 213
-5- SECTION 20.9
Issue 7
4.3.2 When an external electrical supply is used, the connections between that
supply and the aircraft electrical system shall be made and securely locked
before the fuelling operation is connected and shall not be disconnected until
the operation has been completed, except that connectors, which provide
control to ensure effective engagement before external power can be supplied
to the aircraft, need not be locked.
4.3.3 A person shall not, and the pilot in command and the operator shall take
reasonable steps to ensure that a person does not, during fuelling operations:
(a) operate or perform maintenance work on the aircraft’s radar equipment
except that where the fuel is kerosene, operation or maintenance may be
carried out provided the radar transmitter is de-activated; or
(b) except where the fuel involved is kerosene, carry out maintenance on any
electrical, electronic or radio systems within the aircraft or operate such
equipment other than the aircraft’s interior lighting or electrical apparatus
necessary for the fuelling process.
4.3.4 The aircraft and all items of fuelling equipment (including drums, funnels and
other loose items of equipment, where used) shall be connected in such a way
as to ensure that they are of the same electrical potential and, where a suitable
earth point is available at the fuelling site, both the aircraft and the equipment
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