NOTE: You can examine the forward side if you use the
____ access holes in the sidewalls of the nose wheel well. You can examine the aft side of the bulkhead at station
 294.5 from the electronics compartment.
 1)  Make sure the fasteners are installed in the correct positions.
 (e)  Examine the wheel well of the nose landing gear for buckling, flaking paint, cracks, and loose fasteners. 1) Make sure the fasteners are installed in the correct
 positions.
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 (f)  
Make sure there are no loose fasteners in the web of the nose wheel well near the trunnion support fittings. 1) Make sure the fasteners are installed in the correct

 positions.

 (g)  
Examine the keel beam chords, stiffeners, webs and splices at station 540 thru 727A for distortion, buckled or damaged panels and loose fasteners. 1) Make sure the fasteners are installed in the correct

 positions.

 (h)  
Examine the external surface of the fuselage for fuel or other fluid leaks.

 (i)  
Remove the upper wing-to-body fairing forward of the aft fairing.

 (j)  
Examine the trunnion support fitting at body station 706 for the main landing gear for cracks and bolt distortion. 1) Make sure the fasteners are installed in the correct

 positions.

 (k)  
If you found wrinkles on the skin panels that were not there before, make an internal inspections.

 NOTE: Permanent wrinkles frequently occur on the lower
____ side of the fuselage skin aft of STA 727. If the wrinkles were there before, you must make a careful inspection for cracks.
 S 212-011
 (7)  Wings:
 (a)
Examine the wings, nacelles, and upper and lower nacelle strut-to-wing fairing for fuel or other fluid leaks.

 (b)
Examine the wing ribs along the aft side of the rear spar, WBL

 92.5 and 114.0 for cracks.

 (c)  
Examine the upper and lower trailing edge panels and the airplane structure for damage.

 NOTE: Make sure you examine the area near the main landing
____
 gear beam carefully.

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 (d)  
Examine the inboard and outboard trailing edge flaps, flap tracks, drive screws, linkages and fairings for sheared rivets and structure damage.

 (e)  
Examine the inboard and outboard spoilers for sheared rivets and structure damage.

 (f)  
Examine the flap track bolts on the outboard trailing edge flap for crankshafting when the flaps touch the ground.

 (g)  
Examine the flap track bolts on the inboard trailing edge flap for crankshafting when the flaps touch the ground.

 S 212-012
 (8)  
Do the task to make an inspection of the engine after a hard landing (AMM 72-00-00/601).

 S 212-017

 (9)  
Do an inspection of the forward and aft engine mounts on the engine (AMM 71-21-00/601).

 S 212-018

 (10)
 Do an inspection of the aft flange on the turbine frame
 (AMM 72-56-00/601).

 S 212-013

 (11)
 Do the task to make an inspection of a engine nacelle when it touches the ground (AMM 05-51-61).

 S 212-014

 (12)
 Examine the flight controls to make sure the movement of travel is free and the cable tension is satisfactory.

 S 832-015

 (13)
 Do a check of the rigging for the steering mechanism of the nose landing gear (AMM 32-51-00).

 B. Cabin Inspections
 S 212-021
 (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.
　
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