757 MAINTENANCE MANUAL
 E. Structural Damage Procedure
 S 212-028
 (1)  When you find internal or external structural damage, refer to the Structural Repair Manaul (SRM) for the repair.
 F. Put The Airplane Back To Its Usual Condition
 S 412-021
 (1)  Install all of the components you removed if they are servicable, or install replacement parts.
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APU COMPARTMENT STADOORS

Lower Fuselage Inspection
Figure 201

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WL 210
180
BL

45.7
DAMAGE TO WEB STA 1720BL

26.7 BL
9.2
STA 1720 - Rear Pressure Bulkhead Inspection
Figure 202

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 OVERWEIGHT LANDING - MAINTENANCE PRACTICES
__________________________________________ (CONDITIONAL INSPECTION)
________________________
 1.  General_______
 A. Overweight Landing
 (1)  Landing at a weight that is more than the maximum-design-landing weight (MLW).
 B. The Inspections
 (1)  The inspections are divided into two phases, Phase 1 and Phase 2. Phase 1 has 5 inspection groups (Main Landing Gear and Support Structure, Nose Landing Gear, Fuselage, Wing, and Nacelle) and Phase 2 has 6 (the same 5 inspection groups as Phase 1 plus Flight Controls)
 (a)  
Do the Phase 1 Inspection before the next flight if an overweight landing occurred.

 (b)  
Do the Phase 2 Inspection before the next flight if damage is found in the Phase 1 Inspection.

 NOTE: Only the inspection groups where you found damage in the
____ Phase 1 Inspection are necessary to be examined in the Phase 2 Inspection. (Example: Damage to the nose landing gear and fuselage in Phase 1; only do the Nose Landing Gear and Fuselage Inspection in Phase 2). If you do part or all of the Phase 2 inspection, you must do the Flight Control Inspection in Phase 2.
 C. Inspection, Repairs, and Replacements
 (1)  When this procedure tells you to "examine" a part, look for these conditions:
 (a)  
Cracks

 (b)  
Structure that pulled apart

 (c)  
Loose paint (paint flakes)

 (d)  
Twisted parts (distortion)

 (e)  
Bent parts

 (f)  
Wrinkles or buckles in structure

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