(b)  
Examine the nose landing gear outer cylinder at the trunnion-fitting area and the drag brace and linkage. 1) Look for cracks, paint that has flaked, and bent parts. 2) Look for fasteners that have pulled out, or for fasteners

 that are not there.
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 (c)  Examine the nose landing gear wheels and tires for damage or cracks. 1) If any landing gear wheels are removed because of a blown
 tire, do the steps that follow (AMM 05-51-54):
 a) Examine the nose wheel structure for cracks.
 b) Examine the nose wheel bearings for smooth operation
 (no roughness).
 (d)  
Check for wheel misalignment.

 (e)  
Examine the nose landing gear shock strut at the top and bottom ends for signs of hydraulic fluid leakage.

 NOTE: A small quantity of hydraulic fluid on the inner
____
 cylinder is satisfactory.

 (f)  
Examine the nose landing gear outer cylinder for distortion, cracks, paint that has flaked, or other types of damage.

 (g)  
Examine bolted connections, specifically trunnions (attaching upper end of outer cylinder and upper end of upper drag brace), and both upper and lower drag brace segments, attach lugs, and pins.

 (h)  
Examine lock links, torsion links, and torsion link joints including the apex joint. Ensure all joints including nuts, retaining pins, and cotter pins are secure.

 S 212-003
 (3)  Fuselage:
 (a)  Examine the upper and lower fuselage skin panels forward and aft of the wing for buckles, wrinkles or damage.
 NOTE: Permanent wrinkles frequently occur on the lower side of
____
 the fuselage skins aft of STA 727.

 (b)  If you found wrinkles on the skin panels and you did not know they were there before, make an internal inspection.
 NOTE: If the wrinkles were there before, make a careful
____ inspection of the wrinkles for cracks.
 (c)  Examine the keel beam chords, stiffeners, webs and splices at station 663 thru 727A for distortion, buckled or damaged panels and loose fasteners. 1) Make sure the fasteners are installed in the correct
 positions.
 S 212-004
 (4)  Wing:
 (a)  Examine the strut-to-wing fairing panels on the upper and lower nacelle for buckling, cracks and loose fasteners. 1) Make sure the fasteners are installed in the correct
 positions.
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 (b)  Examine the wing leading edge-fairing for displacement, fastener hole elongation or tear-out, skin cracks, and loose fasteners. 1) Make sure the fasteners are installed in the correct
 positions.
 S 212-020
 (5)  Cabin Inspections
 (a)  
Do a visual inspection of all ceiling panels for dislodging and evidence do to impact damage.

 (b)  
Do a visual inspection of all ceiling overhead bins for evidence of looseness and impact damage.

 (c)  
Do a detailed visual inspection of all ceiling panels equipped with video monitors.

 (d)  
Inspect latches, stops, potting inserts and all fasteners.

 TASK 05-51-51-202-005
 3.  Phase II Inspection___________________
 A.  Examine the Airplane Structure
 S 582-006
 (1)  
Lift the airplane on jacks at the wing and fuselage jack points (AMM 07-10-00).

 S 862-007

 (2)  
Retract and then extend the main and nose landing gear with the normal system (AMM 32-32-00 and AMM 32-33-00) to make sure there is no interference, misalignment, or distortion.

 S 862-008

 (3)  
Retract and then extend the main and nose landing gears with alternate manual system (AMM 32-34-00 and AMM 32-35-00) to make sure there is no interference, misalignment, or distortion.
　
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