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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.
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.
16
Civil Aviation Safety Authority Australia
GENERAL
09/2001
1
REFUELLING
SECTION
PILOT RESPONSIBILITIES
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:
• 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
• 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.
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 shall be effectively
connected to that point:
• where the fuelling operation is performed by a barge to a seaplane, the barge shall
be effectively connected to the aircraft in such a way as to ensure that the barge,
the fuelling equipment and the aircraft are at the same electrical potential.
All footwear worn by aircraft servicing personnel and persons operating fuelling
equipment shall be of a non-sparking type and such persons shall not carry any
matches, cigarette lighters or other objects which could represent an ignition hazard.
Except where automatic shut-off devices limit the capacity of an aircraft fuel tank,
the operator and the pilot in command shall ensure that sufficient airspace remains
in each fuel tank to allow for anticipated fuel expansion.
When a fuelling operation on an aircraft has been completed, the pilot in command
and the operator of the aircraft shall ensure that all fuel and oil tank caps are securely
refitted.
Aircraft oil tanks shall not be drained or filled when the aircraft is inside a hangar
or other building unless the oiling equipment used complies with the provisions of
Appendix I of CAO 20.9.
SAFETY PRECAUTIONS EXTERNAL TO AN AIRCRAFT DURING FUELLING
OPERATIONS
The area in which fuelling operations are carried out shall be clearly placarded as a
`No Smoking’ area and the limits of this area shall be a sealed building or at least 15
metres (50 ft) from the aircraft or ground fuelling equipment.
Where mobile fuelling equipment is used, the equipment shall be so placed that it can
be rapidly moved in the event of fire.
17
Civil Aviation Safety Authority Australia
GENERAL
09/2001
1
REFUELLING
SECTION
PILOT RESPONSIBILITIES
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:
• smoke or use a naked flame within 15 metres (50 ft) of the aircraft and ground
fuelling equipment;
• except in the case of aircraft, operate an internal combustion engine or any
electrical switch, battery, generator, motor or other electrical apparatus within 15
metres (50 ft) of the aircraft’s fuel tank filling points or vent outlets, and ground
fuelling equipment unless the engine, switch, generator, motor or apparatus
complies with the provisions of Appendix I to this Order and has been inspected.
Two or more fire extinguishers of approved type and capacity shall be positioned
within 15 metres (50 ft) but not less than 6 metres (20 ft) from the aircraft and the
fuelling equipment except where two or more fire extinguishers are carried on the
fuelling equipment. Where so carried the fire extinguishers shall be fitted with quick
release brackets, be readily available from either side of the equipment and be located
　
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