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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
S 212-025
(2) Do a detailed visual inspection of all ceiling panels equipped with video monitors.
(a)
Inspect latches, stops, potting inserts and all fasteners.
(b)
Inspect latches, stops, potting inserts and all fasteners.
S 212-026
(3) Continue the following inspection if any cabin damage was found in the above Cabin Inspection including the ceiling panels, central overhead bins, or the video monitors (if installed). If no damage was found, no further cabin inspection is required and it is not necessary to continue this Cabin Inspection.
(a)
If ceiling panels without video monitors are found dislodged or damaged: Check for proper latching and installation. Repair as necessary.
(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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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
LANDING-GEAR-DOWN OVERSPEED CONDITION - MAINTENANCE PRACTICES
_____________________________________________________________ (CONDITIONAL INSPECTION)
________________________
1. General_______
A. The structural examination in this subject is applicable if the landing gear is extended in flight at speeds more than the permitted maximum placard speed.
TASK 05-51-07-212-001
2. Landing Gear Down Overspeed Condition, Conditional Inspection_____________________________________________________________
A. References
(1)
32-12-00/001, Main Gear Doors
(2)
32-22-00/001, Nose Gear Doors
B. Examine the Main Gear Door Areas
S 212-002
(1)
Examine the doors, hinges, linkage and linkage support structure, and the fairing panels. Look for distortion, cracks, misalignment, displacement, and fastener hole elongation or tear-out. Also look for fasteners that have pulled out or are not there, and other evidence of distress (Ref 32-12-00).
S 212-003
(2)
Examine the systems that are installed in the wheel wells for evidence of distress.
C. Examine the Nose Gear Door Area
S 212-004
(1)
Examine the doors, hinges, linkage and linkage support structure, and the fairing panels. Look for distortion cracks, misalignment, displacement, and fastener hole elongation or tear-out. Also look for fasteners that have pulled out or are not there, and other evidence of distress (Ref 32-22-00).
S 212-005
(2)
Examine the systems that are installed in the wheel well for evidence of distress.
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