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(c) engine bay fuel strainer controls;
(d) oil cooler shutter and cowl flap;
(e) turbocharger.
(12) Take the following action in relation to the propeller:
(a) inspect the propeller for static track;
(b) inspect the propeller hub, spinner and backplate;
(c) inspect the wooden propeller attachment bolts;
(d) inspect the blades;
(e) inspect the counterweights;
(f) lubricate the propeller hub;
(g) service the propeller hub with air.
(13) Take the following action in relation to the turbocharger:
(a) remove the heat shield and inspect the turbocharger housing for cracks and
oil leaks from the inlet and outlet ports;
(b) inspect the compressor and turbine wheel;
(c) inspect the rotating assembly bearing for end float;
(d) inspect the turbocharger mount;
(e) inspect the transition assembly, the induction and exhaust components and
the clamps;
(f) inspect the upper deck pressure manifold and hoses;
(g) lubricate the waste gate linkages and the butterfly valve;
(h) inspect the flexible oil lines;
(j) inspect the controllers and actuators;
(k) inspect the compressor by-pass door;
(m) refit the heat shield.
(14) Take the following action in relation to the refitting of the cowls:
(a) check that no tooling, rags or other foreign objects remain in the
compartment;
(b) inspect the latches and fasteners for correct tension;
(c) inspect the inlet and cooling air ducting;
(d) inspect the landing and taxi light wiring;
(e) inspect the cowl flap linkage and engine drain lines.
Civil Aviation Regulations 1988 Scheds — 17
Amended CAR – 2nd Ed Legal Services Group
August 2003 Civil Aviation Safety Authority
(15) Chock the wheels and check the brake operation, then set the park brake, start the
engine and take the following action to determine satisfactory performance in
accordance with the manufacturer’s recommendations:
(a) stabilise the engine temperatures and pressures;
(b) check the idle speed, mixture and the magneto switch operation at low
engine revolutions per minute;
(c) check the carburettor heat or alternate air operation;
(d) check the gyro or vacuum pressure indication;
(e) inspect the generator or alternator;
(f) check any unusual engine vibration or noises;
(g) check the engine response to throttle application;
(h) check each magneto and propeller governor for operation;
(j) check the static engine revolutions per minute, manifold pressure and fuel
flow;
(k) check the idle cut-off operation.
(16) After taking the action described above, remove the cowls, inspect the engine for
oil, fuel or other fluid leaks, then replace the cowls.
Section 3—The Electrical System
(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 air-conditioning system:
(a) inspect the distribution system electrical components and interwiring;
(b) inspect the heating and temperature control system;
(c) inspect the freon system electrical components and interwiring;
(d) inspect the air cycle system electrical components and interwiring.
(3) Take the following action in relation to the electrical power:
(a) inspect the AC generation system (including the generator, invertor,
regulator, interwiring, control relays and switching);
(b) inspect the AC distribution system;
(c) inspect the DC generation system (including the generator, regulator,
transformer or rectifier units, interwiring, control relays and switches);
(d) inspect the DC distribution system (including the busses, circuit breakers or
fuses, relays, switches and interwiring);
(e) inspect the starter generator;
(f) inspect the indication systems;
(g) inspect the batteries;
(h) inspect the external power system.
(4) Take the following action in relation to electrical equipment and furnishing:
(a) inspect the flight compartment (including any spare bulbs and fuses);
(b) inspect the passenger compartment (including any spare bulbs and fuses);
(c) inspect the buffet or galley electrical systems, the lavatory compartment
electrical systems and the cargo compartment electrical systems.
(5) Take the following action in relation to the following fire protection systems:
(a) inspect the engine fire detection system;
(b) inspect any other fire and smoke detection systems;
(c) inspect the engine fire extinguishing system;
(d) inspect any other fire extinguishing systems.
Scheds — 18 Civil Aviation Regulations 1988
Legal Services Group Amended CAR – 2nd Ed
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