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Civil Aviation Safety Authority August 2003
(6) Inspect the electrical components and interwiring of the following flight control
systems:
(a) the trim and flap system;
(b) the lift dump and spoiler system;
(c) the lift augmenting system.
(7) Inspect the electrical components and interwiring of the fuel distribution and
dump system.
(8) Inspect the electrical components and interwiring of the main and auxiliary
hydraulic systems.
(9) Inspect the electrical components and interwiring of the following ice and rain
protection systems:
(a) the anti/de-ice systems;
(b) the ice detection and indication systems.
(10) Inspect the systems and components that give audible or visual warnings.
(11) Inspect the electrical components and interwiring of the following landing gear
systems:
(a) the extension and retraction systems;
(b) the wheels, brakes and anti-skid system;
(c) the nose wheel steering system;
(d) the position and warning system;
(e) the anti-retract system.
(12) Inspect lights in or on the following areas:
(a) the flight compartment, the passenger compartment and the cargo and
service compartment;
(b) the exterior and emergency systems.
(13) Inspect the electrical components and interwiring of pneumatic systems.
(14) Inspect the electrical or electronic control panels, equipment racks and junction
boxes.
(15) Inspect the electrical components and interwiring of passenger, crew and cargo
doors.
(16) Inspect the electrical components and interwiring of the propeller control and
anti/de-ice systems.
(17) Inspect the electrical harnesses, excluding the ignition harness.
(18) Inspect the electrical components and interwiring of the engine fuel and engine
control systems.
(19) Take the following action in relation to the ignition:
(a) inspect the electrical power supplies;
(b) inspect the booster coils, vibrator systems and high energy ignition systems;
(c) inspect the switching, including by performing an insulation check of the
magneto switch leads.
(20) Inspect the engine starting system.
Section 4—The Instruments
(1) Check the external and internal required placards.
NOTE: Reference should be made to the aircraft flight manual and airworthiness
directives for the required placards.
(2) Take the following action in relation to the auto-flight system:
(a) inspect the autopilot or the automatic flight control system, including the
flight director and stability control augmentation;
Civil Aviation Regulations 1988 Scheds — 19
Amended CAR – 2nd Ed Legal Services Group
August 2003 Civil Aviation Safety Authority
(b) inspect the yaw damper system;
(c) inspect the speed-attitude correction system, including the auto-trim and
mach-trim.
(3) Inspect the flight control surface indication systems.
(4) Inspect the fuel pressure and quantity indication systems.
(5) Inspect the hydraulic power indication system.
(6) Inspect the ice protection indication system.
(7) Take the following action in relation to indicating and recording systems:
(a) inspect the instrument and control panels;
(b) inspect the independent instrument systems, including the inclinometers,
indicators and clocks;
(c) inspect the recorders, including the flight data recorders, performance or
maintenance recorders.
(8) Take the following action in relation to navigation systems:
(a) inspect the flight environment data system, including:
(i) the central air data system; and
(ii) the pitot/static system, including instruments; and
(iii) the stall warning system;
(b) inspect the attitude and direction systems, including:
(i) the magnetic compass; and
(ii) the vertical attitude gyro system; and
(iii) the directional gyro system, including the magnetic referenced
systems; and
(iv) the electronic flight instrument system and multi-function displays;
(c) inspect the independent position determining systems, including:
(i) the inertial navigation and reference systems; and
(ii) the ground proximity warning systems;
(d) inspect the flight management system, including the flight management and
performance management systems.
(9) Take the following action in relation to oxygen systems:
(a) inspect the crew, passenger and portable systems;
(b) inspect the indicating systems.
(10) Inspect the pneumatic indicating systems, including the pressure gauge and
warning indicators.
(11) Take the following action in relation to the instrument pressure or vacuum system:
(a) inspect the distribution system, including the filters, manifolds, regulating
valves, check valves and plumbing;
　
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