(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) The shock strut pressures were sufficiently low to cause
damage.
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MAIN LANDING GEAR BEAM TRUNNION LINK REACTION LINK
AFT TRUNNION BEARING SEE A SEE C
SEE B
SEE D SEE A
DOWNLOCK LINK
INBD
FWD
LANDING GEAR ON LEFT WING
Main Landing Gear Fuse Pins
Figure 201 (Sheet 1)
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C76554
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MAINTENANCE MANUAL
2. FUSE PIN FORWARD TRUNNION SUPPORT FITTING
3. FUSE PIN (UPPER)
3. FUSE PIN (UPPER)
(LOWER) 3. FUSE PIN B
A (LOWER) 3. FUSE PIN
TRUNNION LINK
INBD
1. FUSE PIN DRAG STRUT A B BEARING FORWARD TRUNNION FWD
LINK TRUNNION A FORWARD TRUNNION SUPPORT FITTING
2. FUSE PIN
1. FUSE PIN TRUNNION LINK DEGREES) (ROTATED 90
DRAG
STRUT FORWARD
TRUNNION
BEARING
TRUNNION
A-A B-B SUPPORT FITTING
Main Landing Gear Fuse Pins
Figure 201 (Sheet 2)
C76600
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MAINTENANCE MANUAL
C
4. FUSE PIN DOWNLOCK SPINDLE
C
INBD
FWD DOWNLOCK LINK
B
DOWNLOCK
SPINDLE
4. FUSE PIN
DOWNLOCK LINK
C-C
Main Landing Gear Fuse Pins Figure 201 (Sheet 3)
C76615
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MAINTENANCE MANUAL
FORWARD REACTION LINK TRUNNION SUPPORT
D
TORQUE TUBE
SUPPORT
D
5. FUSE PIN
INBD
FWD
C
5. FUSE PIN
REACTION LINK
FORWARD TRUNNION
SUPPORT
REACTION
LINK
D-D
Main Landing Gear Fuse Pins
Figure 201 (Sheet 4)
C76624
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MAINTENANCE MANUAL
LANDING
GEAR BEAM
AFT TRUNNION
FITTING
6. FUSE PINS (AFT)
1
AFT TRUNNION BEARING
SHOCK STRUT OUTER CYLINDER
FWD INBD
D
1 AFT SHOWN, FORWARD FUSE PINS ARE HIDDEN
Main Landing Gear Fuse Pins Figure 201 (Sheet 5)
C76993
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本文链接地址：757 AMM 飞机维护手册 时间限制/维护检查(6)
