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needs of that person in the procedures to be followed in the event of emergency
evacuation of the aircraft. The briefing should include which emergency exit to use and
when to move to the exit. The person giving the briefing should also enquire as to the
most appropriate manner of assisting the handicapped person so as to prevent pain or
injury to that person.
173
Civil Aviation Safety Authority Australia
PRE-FLIGHT PLANNING AIRCRAFT SAFETY
09/2001
2
VFR
SECTION
CAO 20.2 AIR SERVICE OPERATIONS - SAFETY PRECAUTIONS
BEFORE FLIGHT
REMOVAL OF LOCKING AND SAFETY DEVICES
Prior to take-off, the pilot in command of an aircraft shall ensure that all control
surface locks, undercarriage pins and locks, and any other devices used for restricting
movement or preventing operation of any part of an aircraft or its equipment when
not in flight or taxi-ing are removed.
Where external control surface locks, undercarriage pins and locks, or other external
locking or restricting devices have been fitted, they shall, except where otherwise
approved by CASA, be removed prior to commencement of taxi-ing for the purpose of
taking off. They shall be removed only by the pilot in command or the co-pilot, or by
a person instructed in this function and authorised to perform it by the owner, hirer,
operator or pilot in command.
Where external control surface locks, undercarriage pins and locks, or other external
locking or restricting devices are removed by a person other than the pilot in command
or co-pilot:
• Removal shall only be effected as directed by the pilot in command.
• The locks, pins and other external devices shall be exhibited to the pilot in command
from a position which will enable him to readily determine that all pins, locks and
devices are being displayed.
• During the hours of darkness the owner, hirer, operator or pilot in command shall
ensure that adequate lighting is provided to enable the pilot in command to see the
articles displayed.
• When the pilot in command is satisfied that all locking devices have been removed
and displayed he or she shall give an agreed form of acknowledgement to the
person effecting removal.
When an aircraft has been parked, taxied or towed in winds exceeding 35 knots and
the control systems and surfaces have not been effectively restrained either by a
person in the cockpit or by approved control surface gust locks, the pilot in command
or an appropriately licensed maintenance engineer shall, before flight, inspect the
control systems and control surface attachments for damage.
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 shall, immediately before
taxi-ing 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.
174
Civil Aviation Safety Authority Australia
PRE-FLIGHT PLANNING SAFETY
PRECAUTIONS
09/2001
2
PRE-FLIGHT
SECTION
Note: Civil Aviation Regulation 244 (1)(a) requires that immediately before taking-off
on any flight, the pilot in command of an aircraft shall 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.
SECURITY OF DOORS AND HATCHES (CAO 20.2)
Immediately before taxi-ing for the purpose of taking off on any flight, the pilot in
command shall ensure that all doors, escape hatches and loading hatches are properly
secured.
PRECAUTIONS BEFORE SOLO FLIGHT IN AIRCRAFT FITTED WITH DUAL
CONTROLS (CAO 20.2)
The pilot in command of an aircraft fitted with dual controls, which is to be flown solo,
shall 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
shall be removed.
FUEL SYSTEM INSPECTION (CAO 20.2)
The operator and pilot in command shall ensure that the following inspections and
tests for the presence of water in the fuel system of the aircraft are made:
• either:
A. if
- 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
- the data has been approved under regulation 42M as part of the
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