(d)  
If you find damage during steps (b) and (c), or if there was a hard landing and a high impact on the nose gear, examine it: 1) Remove the inner cylinder. 2) Examine the nose gear for distortion and cracks.

 (e)  
If you did not find damage during steps (b) and (c), do an inspection of these components at the first convenient opportunity after a hard landing or a high drag/side load landing: 1) The inner cylinder 2) The orifice support tube.

 (f)  
Examine the wheel well area for signs of fluid leaks near the landing gear.

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 S 712-015
 (5)  
Do a check of the adjustment of the steering mechanism of the nose landing gear (AMM 32-51-00/501).

 S 582-010

 (6)  
Lower the airplane off the jacks (AMM 07-11-11/201).

 C. Examine the Fuselage and Wing Areas
 S 212-011
 (1)  Examine the fuselage and wing areas as follows:
 (a)  
Remove the upper wing-to-body fairing immediately forward of the aft fairing (Refer to the operator's standard procedure).

 (b)  
The lower fuselage structure for skin buckling, flaking paint, cracks, and pulled or missing fasteners.

 NOTE: Examine closely in the area below the body crease from
____
 STA 727 to 100 inches aft.

 (c)  
Examine these components at STA 540 through STA 727A for distoriton, buckled or damaged panels, and pulled or missing fasteners: 1) The keel beam chords 2) The stiffeners 3) The webs and the splices.

 (d)  
Examine these components for buckling, distortion, flaking point, cracks and pulled or missing fasteners: 1) The wing to fuselage joints at STA 540 and 664 2) The upper fuselage structure between S-6 Left and S-6 Right

 at STA's 540, 664, and 727 3) The bulkheads at body STA 294.5 and 360, fuselage structure immediately outboard of the nose wheel well
 NOTE: You can do this inspection on the forward side
____ through the access holes in the sidewalls of the nose wheel well. Examine the aft side of the bulkhead at ATA 294.5 from the electronics compartment.
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 4) The wheel well of the nose landing gear and the web of the nose wheel well
 NOTE: Examine closely in the area of the trunnion support____ fittings.
 (e)  5) The body STA 706 trunnion support fitting for the main landing gear.Look for signs of fuel leaks, or other fluid leaks in the areas that follow:
 (f)  1) The wings 2) The nacelles 3) The engine struts 4) The external surface of the fuselage 5) The wheel well of the nose landing gear 6) The wheel wells of the main landing gear.Examine the top and lower fuselage skin panels forward and aft of the wing for buckles, wrinkles or tears.
 NOTE: Permanent wrinkles often occur on the lower side____
 fuselage skins aft of STA 727. An interior inspection is necessary if you find these wrinkles and they did not exist before the landing. If they did exist, examine the wrinkles carefully for cracks.
 (g)  Examine the wing ribs along the aft side of the rear spar at WBL 92.5 and 114.0 for cracks.
 (h)  Examine the upper and lower trailing edge panels and structure.
 NOTE: Examine closely the area of the main landing gear beam.____
 (i) (j) (k)  Examine these flight control components for sheared rivets and structure damage: 1) The inboard and outboard trailing edge flaps 2) The flap tracks 3) The drive screws for the flaps 4) The linkages and the fairings for the flaps 5) The inboard and outboard spoilers.Examine these flap components for crankshafting when it is possible the flaps touched the ground: 1) The flap track bolts of the outboard trailing edge flaps 2) The flap track bolts of the inboard trailing edge flapsInstall the upper wing-to-body fairing immediately forward of the aft fairing (Refer to the operator's standard procedure).
　
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