S 725-363
(3)
Do the steps that follow to make sure the control column and the aft quadrant override operate correctly:
(a)
Install the aft quadrant rigging block (elevator is at neutral) in the first officer's aft quadrant to hold the quadrant in the neutral position (Fig. 511).
NOTE: Rig pins are not applicable blocking tools.
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MAINTENANCE MANUAL
(b) Install a control column lock in the first officer's control
column (Fig. 512).
(c) Put a 6-inch (150 mm) strip of adhesive tape vertically on the
right elevator index plate (Fig. 505).
(d) Make a mark on the tape that shows the up direction.
(e) Make a mark where the upper surface of the right elevator
trailing edge would extend to the tape.
(f) Use the control wheel adapter equipment to attach the force
gage to the captain's control column at the finger reference
point (Fig. 505).
(g) Slowly pull the control column aft until there is a force of
70 | 1 pounds (311 | 4 newtons).
(h) Make a mark on the tape at the right elevator up position.
(i) Let the control column go to the neutral position.
(j) Use the force gage to slowly push the captain's control column
forward until there is a force of 70 | 1 pounds
(311 | 4 newtons).
(k) Make a mark on the tape at the right elevator down position.
(l) Let the control column go to the neutral position.
(m) Make sure that the elevator up and down position marks are less
than 0.50 inch (12.7 mm) away from the right elevator reference
position mark.
(n) Do the steps that follow if travel in the up or down direction
is more than 0.50 inch (12.7 mm):
1) Make sure that the aft quadrant is held in the neutral
position and cannot move.
2) Make a mark at the elevator trailing edge position on the
tape again.
3) Use the force gage as specified above to make marks at the
elevator up and down positions again.
4) Make sure the elevator up and down position marks are less
than 0.50 inch (12.7 mm) away from the right elevator
reference position mark.
(o) Measure and make a mark on the tape that is 2.10 inch
(53.3 mm) above the upper mark.
(p) Measure and make a mark on the tape that is 2.10 inch
(53.3 mm) below the lower mark.
(q) Remove the tape from the right elevator index plate and put it
on the left elevator index plate.
(r) Make sure the middle mark on the tape is in line with the upper
surface of the left elevator trailing edge.
(s) Use the force gage to slowly pull the captain's control column
aft until the left elevator goes above the highest mark on the
tape.
(t) Make sure that the control column force is 70 to 90 pounds
(311-400 newtons).
(u) Let the control column go to the neutral position.
(v) Slowly push the captain's control column forward until the left
elevator trailing edge goes below the lowest mark on the tape.
(w) Make sure that the control column force is 70 to 90 pounds
(311-400 newtons).
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A
757 MAINTENANCE MANUAL
(x)
Let the control column go to the neutral position.
E.
Put the Airplane Back to Its Usual Condition
S 025-426
(1)
Remove the aft quadrant rigging block from the first officer's aft quadrant.
S 025-427
(2)
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本文链接地址：757 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 3(57)
