MAINTENANCE MANUAL
Page 05-16
Effectivity: All
Issue 2 | Rev. 1
SCHEDULED INSPECTION AFTER 100 FH OR ANNUAL INSPECTION
Page: 6 of 12
Ref. Prescribed works Made by Checked by
32-41 Check wheels for cracks, permanent deformations;
replace if damaged.
32-41 Check valve for condition around the hole in the rim.
Beware of cutting the valve when the tire slippage.
32-41 Check bearings for condition, free rotation and play.
Brakes
32-42 Check attachment of brake system plastic hoses to
the main landing gear leg.
32-42 Check brake pads for condition, equal and symmetry
abrasion; replace pads as required. Min. admissible
thickness of brake pad is 0,5 mm (S5 10-03 01 / S5
10-03 02 brakes) or 2,54 mm (Matco brakes).
32-42 Check brake disc for condition, wear and overheating.
Min. admissible thickness of brake disc is 3,2 mm
(S5 10-03 01 / S5 10-03 02 brakes) or 3,3 mm
(Matco brakes)
12-10 Check brake system for leaks; add brake fluid and
bleed the system if a brake pedal has soft movement.
Lower the airplane.
5. WING
57-10
57-20
57-30
Check wing structure / skin for condition, loosened
rivets, deformation, cracks, corrosion and some other
damage; contact airplane manufacturer if any
damage were found.
57-20
33-40
Check wing tips including position / strobe light for
condition and attachment.
57-10 Check integral tank riveted joints for leakage.
28-10 Check fuel tank drain valve for condition and
function.
27-10 Check control system joints inside the wing for
security.
34-10 Check stall speed warning sensor for condition.
Check wires for integrity and grounding.
Notes:
Date: ........................................ Signature: ........................................