Document ID: chunk:federal_register_of_legislation:F2024C00887:schedule:5:p8
Version: federal_register_of_legislation:F2024C00887
Segment Type: schedule
Provision Reference: sch 5 (pt 8/11)
Character Range: 323543–326602

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.
(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