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(d) If one or more of the fuse pins are damaged, do the steps that follow: 1) Examine the lugs and fittings of the fuse pins that are
found to be damaged.
2) Examine the landing gear beam and look to see if it is
twisted or bent.
3) Examine the drag struts.
4) Examine the side struts and downlocks (parts that hold the
side strut in the correct position). 5) Examine all gear bolts and pins and their attachment lugs.
(e)
If a tire burst (i.e., the tire came apart during a takeoff or landing) do the steps that follow: 1) Remove and examine the wheel structure 2) Remove and examine the brake assembly 3) Examine the axles.
(f)
If one or more of the conditions that follow occurred; remove, disassemble, and examine all parts of the shock strut (AMM 32-11-01/401). 1) The shock strut pressures were sufficiently low to cause
damage. 2) The hydraulic fluid levels were sufficiently low to cause damage. 3) You found damage to one or more of the parts during your inspection of the landing gear.
(g)
Make sure the main landing gear retracts and extends correctly (AMM 32-32-00/501).
(h)
Lower the airplane from the jacks (AMM 07-11-01/201).
S 212-039
(2) Nose Landing Gear Inspection
(a)
Make sure the shock strut pressures are normal and the hydraulic fluids are at the correct levels (AMM 12-15-02/301).
(b)
Lift the nose of the airplane with jacks (AMM 07-11-01/201).
(c)
Examine the upper and lower drag struts.
(d)
Examine the forward and aft lock links (parts that hold the drag strut in the correct position).
(e)
Examine all gear bolts, pins, and their attachment lugs.
(f)
Remove the wheel and tire assembly and examine the axle.
(g)
If one or more of the conditions that follow occurred; remove, disassemble, and examine all parts of the shock strut (AMM 32-21-01/401). 1) If the shock strut pressures were sufficiently low to cause
damage.
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MAINTENANCE MANUAL
2) The hydraulic fluid levels were sufficiently low to cause damage. 3) You found damage to one or more of the parts during your inspection of the nose landing gear.
(h)
Make sure the steering system is adjusted and operates correctly (AMM 32-51-00/501).
(i)
Make sure the nose landing gear retracts and extends correctly (AMM 32-34-00/501).
(j)
Lower the nose of the airplane from the jacks
(AMM 07-11-01/201).
S 212-040
(3) Fuselage Inspection
NOTE: If you find external damage to the fuselage, always examine
____
the adjacent internal structure.
(a)
Examine the lower fuselage structure. Examine carefully the area below the body floor beams, immediately aft of the wing center section. Also examine carefully the top of the fuselage in the areas near the wing front and rear spar.
(b)
Examine the wing-to-fuselage joints, and wheel well bulkheads and sidewalls.
(c)
Examine the external structure in the wheel well area of the nose landing gear.
(d)
Examine the fuselage skin joints above the landing gear beam.
(e)
If the lower fuselage (body sections 46 and 48) shows signs that it hit the runway, examine the areas that follow: 1) APU firewall 2) APU drain 3) APU door 4) Drain mast 5) Lower fuselage skin, stringers, frames, and shear ties 6) Aft pressure bulkhead.
S 212-041
(4) Wing Inspection
(a)
Examine the side-of-body ribs in the area of the rear spar.
(b)
Look at the rear spar to make sure that it is not permanently bent or twisted (between the fuselage and the outboard fuel tank).
S 212-042
(5) Engine Nacelle Inspection
(a) Do the inspection procedure for the dragged engine nacelles (AMM 05-51-10/201).
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