Tecnam P2012 - Page 66

P2012
AIRCRAFT MAINTENANCE MANUAL
cracks, distortion, dents, corrosion) refer to ATA 51-30 ATA
51-70. Check for hinges loosening, travel limits and correct
operation. Hinges allowable wear is the following: -Axial ± 1.00
mm (± 0.04 in) -Radial ± 0.25 mm (± 0.01 in)
55-00 Tail Inspect stabilizer attachment fitting to fuselage for structural
integrity and holes for elongation.
X
55-00 Tail Inspect stabilizer attaching parts (front spar carry through) for
correct torque value.
X
(*)
55-00 Tail Inspect the stabilizer rear spar for corrosion and Integrity (refer to
ATA 51-30).
X
55-00 Tail Inspect elevator for surface damage or irregularities (skin cracks,
distortion, dents and corrosion), loosen or missing rivets, hinges
and bearings damage and excessive wear, free to move. Hinges
allowable wear is the following: -Axial ± 1.00 mm (± 0.04 in)
-Radial± 0.25 mm (± 0.01 in) Check for elevator full travel
operation.
X
(*)
55-00 Tail Check for elevator proper electrical bonding, refer to ATA 51-30.
X
55-00 Tail Inspect elevator tab for surface condition (damage or
irregularities), loose or missing rivets and security . Check for
elevator tab full travel operation.
X
55-00 Tail Remove tail cone aft fairings and check Elevator mounting plates
for absence of cracks, corrosion and dust, clean the area and
grease parts subject to rotation.
(*)
55-00 Tail Inspect fin rear spar for corrosion and integrity, refer to ATA
51-30.
X
55-00 Tail Rudder trim actuator operational check. Active trim motor by
knob in cabin and verify the surface movement in accordance
with selected position.
X
55-00 Tail Visually inspect tail skin, frame and stringer for damage, crack
and wear, refer to ATA 51-30.
(*)
55-00 Tail Inspect rear baggage compartment skin (external and internal),
frame and stringer and net attachments.
(*)
55-00 Tail Inspect the trim tab to measure the amount free play on the
X
05-20-00
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Edition - Rev. 0
2022, Jan 14