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757
MAINTENANCE MANUAL
SUPPORT FITTING MAIN LANDING GEAR BEAM INBOARD
SEE E SEE B SEE INBOARD STABILIZING LINK A
MAIN LANDING GEAR BEAM SEE D REAR WING SPAR
SEE F INBD
SEE C FWD
BEAM OUTBOARD SUPPORT FITTING MAIN LANDING GEAR OUTBOARD STABILIZING LINK
Main Landing Gear Beam End Fittings and Stabilizing Links
Figure 202 (Sheet 1)
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C82665
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757 MAINTENANCE MANUAL
INBOARD 7. FORWARD STABILIZING LINK FUSE PIN
FITTING
INBD
A FWD
7. AFT FUSE PIN
STABILIZING LINK INBOARD
FITTING
FWD
OUTBDB
Main Landing Gear Beam End Fittings and Stabilizing Links Figure 202 (Sheet 2)
C82675
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MAINTENANCE MANUAL
FITTING
OUTBOARD STABILIZING LINK
FWD
8. FORWARD FUSE PIN
INBD
C
FITTING
8. AFT FUSE PIN
OUTBOARD STABILIZING LINK
INBD FWD
D
Main Landing Gear Beam End Fittings and Stabilizing Links
Figure 202 (Sheet 3)
C82685
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757
MAINTENANCE MANUAL
MAIN LANDING GEAR BEAM
INBOARD SUPPORT FITTING
INBD
FWD
Main Landing Gear Beam End Fittings and Stabilizing Links
Figure 202 (Sheet 4)
C82668
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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 212-036
(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 thats 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.
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