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(b) if the skin is fabric, check the strength of the fabric;
(c) inspect the internal structures and spars;
(d) inspect the lift struts, interplane struts, jury struts, spreaders, chafing discs
and bracing wires;
(e) inspect the flight control surfaces, slats, spoilers, tabs, flaps, mass balance
weight attachments, hinge brackets, tracks and rollers;
(f) inspect the flight control system bellcranks, push pull rods, torque tubes,
cables, fairleads, turnbarrells and pulleys;
(g) inspect the wing and empennage to fuselage attachments and surrounding
structure;
(h) lubricate as necessary.
(3) Take the following action in relation to the fuselage:
(a) inspect the fuselage skin for evidence of wrinkles, buckles, sheared or loose
rivets, corrosion, disbonds and general damage;
(b) inspect the areas around cut-outs (such as windows and inspection apertures)
for cracks and inspect the sealing and fit of all doors and emergency exits;
(c) inspect the interior;
(d) inspect the strength of the fabric covering on surfaces;
(e) inspect the internal structure;
(f) inspect the locks, latches and hinges of doors, canopy, windows which may
be opened and direct vision windows;
(g) check that the windshields and windows are clean and free from crazing,
cracking, discoloration, delamination and scratches;
(h) inspect the seats, seat attachments, seat adjustment mechanisms, seat stops,
seat belts, safety harnesses and inertia reels;
(j) inspect the control wheels, control columns, rudder pedals, control levers,
control system bellcranks, push pull rods, torque tubes and cables;
(k) operate all trim controls through the complete range of travel and check
them for correct trim position indication;
(l) inspect the brake master cylinders, brake lines, reservoirs, parking brake
linkage and mechanical brake system operating mechanisms;
(m) check the cabin fire extinguisher for correct charge, legibility of operating
instructions and condition of locking pin or seal and ensure that the
extinguisher has not reached its expiry date;
(n) inspect the heating and fresh air system ducting and outlets and the airflow
control valves;
(p) inspect the emergency and flotation equipment and ensure that the
equipment has not reached its expiry date;
Scheds — 14 Civil Aviation Regulations 1988
Legal Services Group Amended CAR – 2nd Ed
Civil Aviation Safety Authority August 2003
(q) lubricate as necessary.
(4) Jack the aircraft so that the landing gear is clear of the ground and take the
following action:
(a) inspect the undercarriage attachment to the airframe;
(b) inspect the structural members, drag and side braces, compression members,
oleo struts, bracing struts and torque links;
(c) inspect the leaf or tube spring shock absorbing units and bungee rubber;
(d) inspect the flexible hoses;
(e) inspect the main wheels and tyres and the nose or tail wheels and tyres;
(f) clean the wheel bearings, check that they are free from scoring and
brinelling, re-lubricate them, re-install them and adjust the bearing pre-load;
(g) inspect the brake linings or pads and the brake drums or discs;
(h) inspect the brake lines and flexible hoses;
(j) inspect the nosewheel or tailwheel steering mechanism and the shimmy
dampener;
(k) inspect the landing gear retraction mechanism, the door and the door
operating linkage;
(l) carry out an operational check of the landing gear and doors and ensure that
the adjustment of downlocks, overcentre links, uplocks and spring tensions
are within the manufacturer’s specified limits;
(m) lubricate as necessary.
(5) Take the following action in relation to the fuel system:
(a) inspect the fuel tanks (where visible), lines, drains, vents, signs, filler caps,
filler cap securing chains or cables, filler cap seals and scupper drains;
(b) inspect the fuel selector valves;
(c) inspect the fuel selector valve operating linkage.
(6) Take the following action in relation to the hydraulic system:
(a) remove, clean, and refit the hydraulic system filter element, or if it is
unserviceable, install a new filter element;
(b) inspect the hydraulic system reservoirs, powerpack, accumulators, selector
valves, hand pump, pipelines and flexible hoses.
(7) Inspect the anti-icing and de-icing systems.
(8) Inspect the air-conditioning evaporator, condenser and compressor and the airconditioning
ducting, pipelines and units.
(9) Inspect the pressurisation control system and indication system.
(10) Take the following additional action if the aircraft is used in agricultural
operations:
(a) inspect the hopper, hopper lid and fasteners, baffles and internal braces;
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