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737-300/400/500MAINTENANCE MANUAL
(b) If central overhead stowage bins are found with impact damage
or are loose, or if ceiling panels equipped with video monitors
are found with broken lateches: repair as necessary.
(c) Inspect all tie rods of affected zones for evidence of buckling
or rupture. If any defect is found, replace as necessary.
(d) Examine lavatory tie rod attachments for damage consisting of
breakage, cracks, and deformation. Inspect the tie rods for
evidence of buckling or rupture.
(e) Examine the lavatory floor fittings for damage consisting of
breakage, cracks, and deformation.
(f) Examine galley tie rod attachments for damage consisting of
breakage, cracks, and deformation. Inspect the tie rods for
evidence of buckling or rupture.
(g) Examine the galley floor fittings for damage consisting of
breakage, cracks, and deformation.
(h) Examine closet tie rod attachments for damage consisting of
breakage, cracks, and deformation. Inspect the tie rods for
evidence of buckling or rupture.
(i) Examine the closet floor fittings for damage consisting of
breakage, cracks, and deformation.
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737-300/400/500MAINTENANCE MANUAL
TIRE TREAD LOSS OR TIRE BURST - MAINTENANCE PRACTICES (CONDITIONAL INSPECTION)
______________________________________________________________________________
1. General
_______
A. One task is supplied in this procedure. The task is tire tread loss or tire burst conditional inspection.
B. When a landing gear tire loses a tread or a tire bursts, a careful examination of some areas is required. These examinations look for damage and/or blockage caused by pieces of the tire.
C. Damage caused by the tire pieces can be seen as rubber and/or bitumen marks on the surface of the structure.
TASK 05-51-54-212-023
2. Tire Tread Loss or Tire Burst Conditional Inspection
____________________________________________________
A. References
(1) AMM 32-45-00/601, Tires and Wheels
B. Procedure
S 212-015
(1) Examine these areas for damage, delamination or local separation, and soft spots due to core crush:
NOTE: To find delamination or local separation areas tap the
____ surface with a coin. To find areas of core crush, push on the surface.
(a)
Wing Upper and Lower Inboard Fixed Trailing Edge Panel
(b)
Inboard Trailing Edge Flaps and Fairings
(c)
ADF Antenna
(d)
Lower Fuselage Wing-to-Body Fairing Panels
S 212-016
(2)
Examine the inboard trailing edge flaps for tire fragments lodged in linkages or in flap carriages (main and foreflap sequence carriages).
S 212-017
(3)
Examine the trailing edge flap jackscrews, actuating linkages and rods for damage and blockage due to pieces of the tire.
S 212-018
(4)
Examine the landing gear wheel well areas for damage and obstruction from pieces of the tire.
NOTE: Carefully examine the hydraulic plumbing, flap drive torque
____ tubes, and control cables and mechanisims for damage or distortion.
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