P2012
AIRCRAFT MAINTENANCE MANUAL
Wheel System hole elongation, corrosion and warpage. Remove corrosion and
blend out small nicks using fine (400 grit) sandpaper. Replace
brake disc if worn below wear limits detailed in ClevelandManual
AWBCMM0001 latest issue. Coning of disc in excess of 0.015 inch
(0.381 mm) is cause of replacement.
Cleveland Manual
AWBCMM0001
latest issue
32-40 Brake and
Wheel System
(MLG)
Check wheel nuts to be sure they are properly installed and have
not worked loose. Bolt threads should be flush to 1-1/2 threads
extending beyond the nut. Nuts should be on the side of wheel
opposite the brake disc (outboard side of wheel), except in those
cases where spline nuts and bolts are used to secure wheel halves.
Annually see
Cleveland Manual
AWBCMM0001
latest issue
32-40 Brake and
Wheel System
(NLG)
Check wheel nuts to be sure they are properly installed and have
not worked loose. Bolt threads should be flush to 1.5 threads
exteding beyond the nut.
Annually see
Cleveland Manual
AWBCMM0001
latest issue
ATA Aircraft
Zone
Maintenance Task Frequency
A B C D E
STABILIZER
55-00 Vertical Tail Inspect vertical stabilizer for surface damage or irregularities (skin
cracks, distortion, dents, corrosion) and structural defects (loose or
missing rivets).
X
(*)
55-00 Vertical Tail Check attachment points between vertical stabilizer and tail cone.
(Refer to ATA and ATA and )
X
55-00 Vertical Tail Inspect rudder for surface damage or irregularities (skin cracks,
distortion, dents, corrosion), loose or missing rivets, hinges and
bearings damage and excessive wear, free play.
X
(*)
55-00 Vertical Tail Inspect the rudder for condition and security of installation. Check
travel limit for condition and security.
X
55-00 Vertical Tail Visually inspect rudder for condition, security and operation. Check for
rudder full travel operation.
X
55-00 Vertical Tail Inspect rudder trim for surface damage or irregularities (skin cracks,
distortion, dents, corrosion) (Refer to ATA and ATA ). Check for
hinges loosening, travel limits and correct operation.
X
ATA Aircraft
Zone
Maintenance Task Frequency
A B C D E
STABILIZER
55-00 Vertical
Tail
Inspect the vertical stabilizer rear spar for corrosion and integrity.
(Refer to ATA )
X
05-20-00
Page 7
5
th
Edition - Rev. 0
2022, Jan 14
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