S 212-037
(4) Wing Inspection
(a)
Examine the side-of-body ribs in the area of the rear spar.
(b)
Look at the rear spar to make sure that it is not permanently bent or twisted (between the fuselage and the outboard fuel tank).
S 212-038
(5) Engine Nacelle Inspection
(a) Do the inspection procedure for the dragged engine nacelles (AMM 05-51-10/201).
S 722-039
(6) Flight Control Inspection
(a) Make sure the flight control cables are correctly adjusted (AMM 27-00-01/201).
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(b) Make sure the flight controls move freely.
C. Cabin Inspections
S 212-047
(1) Continue the following inspection if any cabin damage was found in the Phase I Cabin Inspection including the ceiling panels, central overhead bins, or the video monitors. 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 lavatory tie rod attachments for damage consisting of breakage, cracks, and deformation. Inspect the tie rods for evidence of buckling or rupture.
(f)
Examine the lavatory floor fittings for damage consisting of breakage, cracks, and deformation.
(g)
Examine the lavatory floor fittings for damage consisting of breakage, cracks, and deformation.
(h)
Examine galley tie rod attachments for damage consisting of breakage, cracks, and deformation. Inspect the tie rods for evidence of buckling or rupture.
(i)
Examine the galley floor fittings for damage consisting of breakage, cracks, and deformation.
(j)
Examine closet tie rod attachments for damage consisting of breakage, cracks, and deformation. Inspect the tie rods for evidence of buckling or rupture.
(k)
Examine the closet floor fittings for damage consisting of breakage, cracks, and deformation.
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D. Put the airplane back to it's usual condition.
S 422-041
(1) Install the components you removed if they are servicable, or install replacement parts.
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SEVERE OR UNUSUAL TURBULENCE, STALL, BUFFETING, OR EXCEEDING DESIGN SPEED
_________________________________________________________________________ CONDITION - MAINTENANCE PRACTICES (CONDITIONAL INSPECTION)
__________________________________________________________
1. General_______
A. The structural examination in this subject is applicable after a severe or unusual turbulence or buffet condition. It also applies to stalls (after the initial buffet or stick shaker condition), or if the airplane speed is more than the design speed.
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