Document ID: chunk:federal_register_of_legislation:F2024C00887:schedule:5:p10
Version: federal_register_of_legislation:F2024C00887
Segment Type: schedule
Provision Reference: sch 5 (pt 10/11)
Character Range: 329170–332435

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;
 (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;
 (b) inspect the indicating system, including the pressure gauge and warning system.
(12)  Inspect the engine indicating systems, including fuel flow, temperature and pressure.
(13)  Take the following action in relation to the engine indicating systems:
 (a) inspect the power indicating system;
 (b) inspect the temperature indication system;
 (c) inspect the integrated engine instrument system.
(14)  Inspect the oil indicating systems, including quantity, pressure and temperature.
(15)  Inspect the water injection indicating system.

Section 5  The radio system
(1)  Check the interior and exterior required placards including frequency charts.
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 communication and navigation systems:
 (a) inspect the accessible interwiring, plugs and sockets;
 (b)