Tecnam P2012 - Page 63

P2012
AIRCRAFT MAINTENANCE MANUAL
32-10
32-20
Landing gear Visually inspection and cleaning NLG
X
32-10
32-20
Landing gear MLG removal, check the MLG and MLG fitting contact surfaces
for corrosion, cleaning, MLG installation, sealing the joint.
X
32-10
32-20
Landing gear NLG removal, check the NLG and NLG fitting contact surfaces
for corrosion, cleaning, NLG installation.
X
32-10
32-20
Landing gear NLG and MLG greasing at greasing points.
X
32-10
32-20
Landing gear Visually check NLG shimmy damper hydraulic fluid leakage.
X
32-00 Landing gear Visually inspect nose gear steering control and travels.
X
32-00 Landing gear Visually inspect rudder pedals and steering leverage for
operation, condition and cracks (ref to ATA 51-30)
X
(*)
32-00 Landing gear Visually inspect tires for cuts, worn spots, bulges, on
the side walls, foreign objects in the threads
and threads condition (ref to ATA 51-30).
X
32-00 Landing gear Check tire pressure (ref to procedure included in ATA 32).
X
32-00 Landing gear Visually check the MLG and NLG wheels for
demage/deformation, refer to ATA 51-30
X
32-00 Landing gear Check for free play in wheel bearings. Examine wheels: check
for eventual cracks.
X
(*)
32-00 Landing gear Inspect the brakes line for damage and hydraulic fluid leakage.
Check line retaining clamps.
X
32-00 Landing gear Check parking valve for damage, leakage and proper installation.
Inspect parking brake handle, check for restricted movement,
interference or unusual loosening.
X
(*)
32-00 Landing gear Check oil levels in master cylinders. Check toe brakes for
operation and master cylinder and hoses for damage and
leakage in case of excessive brake oil consumption.
X
32-00 Landing gear MLG and NLG cleaning (external parts).
X
32-00 Landing gear Disassemble the wheels and check for cracks, corrosion, dents,
distortion and faulty bearings. Clean, check and repack wheel
bearings with grease. Refer to Maintenance manual (see
Cleveland Manual AWBCMM0001-21).
800 FH or
5 years (wof)
32-00 Landing gear Visually inspect the wheel axes. Look especially for corrosion
and cracks (ref to ATA 51-30).
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 32).
5000 landings
05-20-00
Page 25
5
th
Edition - Rev. 0
2022, Jan 14