Tecnam P2012 - Page 44

P2012
AIRCRAFT MAINTENANCE MANUAL
distortion and faulty bearings. Clean, check and repack wheel
bearings with grease. Refer to Maintenance manual (see Cleveland
Manual AWBCMM0001-21).
5 years (wof)
32-00 Landing gear Visually inspect the wheel axes. Look especially for corrosion and
cracks (Refer to ).
800 FH or 5 years
(wof)
32-00 Landing gear Disassemble and inspect the brake assemblies and examine the
parts (lining, disc and plates) for wear, cracks, warpage, corrosion,
elongated holes, etc. Refer to maintenance manual (see Cleveland
Manual AWBCMM0001-21).
800 FH or 5 years
(wof)
32-00 Landing gear NLG torque linkage arms replacement (refer to ATA ).
5000 landings
32-20 Landing gear NLG overhaul (Ref. ATA 32-20-00)
10000 landings
32-10 Landing gear MLG overhaul (Ref. ATA 32-10-00)
10000 landings
32-40 Brake and
Wheel System
Visually inspect for corrosion cracks or other visible damage. Check
inlet fitting bosses and anchor bolt lugs for cracks. Check inlet flares
on aircraft side of rigid hydraulic tubing for cracks, check for fluid
leaks.
Annually see
Cleveland Manual
AWBCMM0001
latest issue
32-40 Brake and
Wheel System
Check back plate attachment bolts for correct torque, no loosing
could occur.
Annually see
Cleveland Manual
AWBCMM0001
latest issue
32-40 Brake and
Wheel System
Check brake cylinder anchor bolts in torque plate bushings for
sloppiness.
Annually see
Cleveland Manual
AWBCMM0001
latest issue
32-40 Brake and
Wheel System
Visually check torque plate for corrosion, cracks, loose anchor bolt
bushings or other visible damage. Anchor bolt bushings must be flat
against torque plate surface.
Annually see
Cleveland Manual
AWBCMM0001
latest issue
32-40 Brake and
Wheel System
Inspect brake lining for edge chipping and surface deterioration.
Normal use will result in some edge chipping. A maximum of 10
percent surface loss is acceptable. Minor accumulation of metal
chips in lining is normal and not detrimental. Elongated rivet or pin
holes is cause for replacement. Smearing of lining material on the
brake disc which exceeds 30% of surface is cause for replacement.
Check wear: if it is < 2.54 mm (0.100 inch ) it must be replaced.
Annually see
Cleveland Manual
AWBCMM0001
latest issue
ATA Aircraft Zone Maintenance Task Frequency
A B C D E
LANDING GEAR
32-40 Brake and Inspect brake disc for cracks, excessive wear, or scoring, mounting
Annually see
05-20-00
Page 6
5
th
Edition - Rev. 0
2022, Jan 14