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flight, inspect the control systems and control surface attachments for damage.
2.5 Where external control surface locks or restricting devices have been removed
as prescribed by paragraphs 2.2 and 2.3 of this section, or where an aircraft is
to be flown for the first time following maintenance work involving the
aircraft’s control surfaces or control surface systems, the pilot in command
must, immediately before taxiing for the purpose of taking off, test the flight
controls to the full limit of their travel and make such other tests as are
necessary to ensure that those controls are functioning correctly.
Note: Paragraph 244 (1) (a) of the Civil Aviation Regulations 1988 requires that immediately
before taking-off on any flight, the pilot in command of an aircraft must test the flight
controls on the ground to the full limit of their travel and make such other tests as are
necessary to ensure that those controls are functioning correctly.
3 SECURITY OF DOORS AND HATCHES
Immediately before taxiing for the purpose of taking off on any flight, the pilot
in command must ensure that all doors, escape hatches and loading hatches are
properly secured.
4 PRECAUTIONS BEFORE SOLO FLIGHT IN AIRCRAFT FITTED WITH
DUAL CONTROLS
The pilot in command of an aircraft fitted with dual controls, which is to be
flown solo, must ensure that safety harness and any other articles or equipment
which may foul the controls are safely secured; if the second control column is
readily detachable, it must be removed.
5 FUEL SYSTEM INSPECTION
5.1 The operator and pilot in command must ensure that the following inspections
and tests for the presence of water in the fuel system of the aircraft are made:
(a) either:
(i) if:
(A) the aircraft manufacturer’s data specifies the manner in which
inspections and tests for the presence of water in the aircraft’s
fuel system are to be made; and
Issue 7: 8 December 2004
Amdt No. 204
-3- SECTION 20.2
Issue 7
(B) the data has been approved under regulation 42M of the Civil
Aviation Regulations 1988 as part of the aircraft’s system of
maintenance;
an inspection and test in accordance with the approved data; or
(ii) in any other case — before the start of each day’s flying, and after
each refuelling, with the aircraft standing on a reasonably level
surface, drain a small quantity of fuel from each fuel tank into a clear
transparent container and check by an approved method for the
presence of water;
(b) on such aircraft types which may be specified by CASA, extend the
foregoing inspection to fuel system filters and collector boxes. It is
recommended that all aircraft fuel system filters and collector boxes be
checked for water contamination at frequent intervals.
Note: It is important that checks for water contamination of fuel drainage samples be
positive in nature and do not rely solely on sensory perceptions of colour and smell, both
of which can be highly deceptive. The following methods are acceptable:
1. Place a small quantity of fuel into the container before taking samples from tank or
filter drain points. The presence of water will then be revealed by a visible surface of
demarcation between the two fluids in the container.
2. Check the drainage samples by chemical means such as water detecting paper or
paste, where a change in colour of the detecting medium will give clear indication of
the presence of water.
3. In the case of turbine fuel samples, tests should also include inspection for persistent
cloudiness or other evidence of the presence of suspended water droplets, which will
not necessarily be detected by methods mentioned in notes 1 and 2. Should any doubt
exist of the suitability of the fuel, the checks specified in the aircraft Operators
Maintenance Manual should be followed. It is advisable to allow turbine fuel a
reasonable period of stagnation before drawing test samples from fuel drain points;
this allows settling of suspended water which is a slower process in turbine fuel than
in aviation gasoline.
5.1A In relation to a refuelling that is a hot refuelling in accordance with section
20.10 or section 20.10.1, the operator and pilot in command of an aircraft are
not required to carry out inspections and tests in accordance with paragraph
5.1. This does not effect the requirement to do so before the start of each day’s
flying.
5.2 If, at any time, a significant quantity of water is found to be present in an
aircraft fuel system, the operator and pilot in command must ensure that all
traces of it are removed from the fuel system, including the fuel filters, before
　
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