NOTE: Examine the strut mid-spar carefully.
____
 c) Bulkheads and webs. 2) Examine the areas of all four struts as follows: a) Mid-spar attachment areas:
 -Strut mid-spar fittings
 -
Spring beam mid pivot area

 -
Spring beams

 -Fuse pins
 -Lugs
 -Side links (inspection required on Strut number 1 and Strut number 3 only)
 -Attachment hardware
 -All other structure in this area. b) Diagonal brace area:
 -Lugs
 -Fuse pin (upper pin only)
 -Bushings.
 c) Upper Link areas:

 -Upper link assembly
 -Strut attach fitting
 -Wing attach fitting, including upper skin attachments
 -Bushings
 -Fuse pins
 -Lugs
 -Wing leading edge beam located above each engine strut
 -Strut to wing fairing
 -All other structure in this area.
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 d) Examine all engine mounts and the adjacent structure.
 S 212-061
 (12) Examine the areas that follow and look for signs of fuel or other types of fluid leakage:
 (a)  
The wing

 (b)  
The nacelles

 (c)  
The horizontal stabilizer

 (d)  
The external surfaces of the fuselage.

 (e)  
All of the wheel wells of the landing gear.

 S 222-062
 (13) When flight load accelerations are more than the flight manual limits, and the last inspections showed signs of much damage, check the airplane alignment.
 NOTE: The Alignment Check Procedure is in the Structural Repair
____
 Manual.

 S 712-063
 (14)
 Make sure the handling systems for the containers/pallets in the cargo compartments operate correctly.

 (a)  
Do a check of the restraint system in all of the cargo compartments.

 (b)  
Visually examine the items that follow: 1) The side guides 2) The seat tracks 3) The pallet locks 4) The rollers (where installed) that do not move freely.

 (15)
 Examine landing gear doors for damage.

 (16)
 Examine the landing gear uplocks for damage.

 S 212-064
 S 212-065
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 S 212-066
 (17)
 Examine the inspection and blowout doors on the lower surface of the wing and engine pylons.

 S 212-067

 (18)
 Examine all of the inspection and access doors on the lower side of the body (from body stations 470 to 2200).

 S 212-068

 (19)
 Examine the wingtip fairings.

 D.  Examine the Airplane Structure After Stall (Beyond Initial Buffet or Stick Shaker)
 S 042-069
 WARNING: DO THE DEACTIVATION PROCEDURE FOR THE TRAILING EDGE FLAP
_______ ACTUATION SYSTEMS. FLAP ACTUATION SYSTEMS MUST NOT BE OPERATED DURING THIS INSPECTION. FAILURE TO OBEY THIS WARNING CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1)  Do the deactivation procedure for the trailing edge flap system (AMM 27-51-00/501).
 S 042-070
 WARNING: DO THE DEACTIVATION PROCEDURE FOR THE LEADING EDGE FLAP
_______ ACTUATION SYSTEMS. FLAP ACTUATION SYSTEMS MUST NOT BE OPERATED DURING THIS INSPECTION. FAILURE TO OBEY THIS WARNING CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (2)  Do the deactivation procedure for the leading edge flap system (AMM 27-81-00/501).
 S 492-071
 WARNING: DO NOT GO INTO THE WING LEADING EDGE AREAS BEFORE YOU INSTALL
_______ THE SAFETY LOCKS. THE LEADING EDGE FLAPS WILL RETRACT IN 7 SECONDS. PUT LOCKS ON ALL LEADING EDGE FLAPS THAT ARE EXTENDED. THIS WILL PREVENT INJURY TO PERSONS FROM ACCIDENTAL FLAP OPERATION.
　
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