S 865-A10
 (42) While the switches are held down, slowly push the control column forward until the stabilizer stops.
 NOTE: Do this step while the stabilizer indicated position is
____ between 5.0 and 15.5 units of trim.
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MAINTENANCE MANUAL

 S 225-A11
 (43)
 Measure the angle of travel of the control column from the neutral position to the point where the stabilizer stops. The angle of travel should be 3.5 to 4.0 degrees.

 S 865-A12

 (44)
 Let the control column go to the neutral position.

 S 865-A13

 (45)
 Hold the stabilizer-trim control-wheel-switches down (airplane nose up) until the stabilizer stops.

 S 865-A14

 (46)
 Move the first officer's stabilizer-trim control-wheel-switches up (airplane nose down).

 (a)
Make sure the stabilizer moves.

 S 865-A15
 (47) While the switches are held up, slowly pull the control column aft until the stabilizer stops.
 NOTE: Do this step while the stabilizer indicated position is
____
 between 5.0 and 15.5 units of trim.

 S 225-A16
 (48)
 Measure the angle of travel of the control column from the neutral position to the point where the stabilizer stops. The angle of travel should be 2.2 to 2.7 degrees.

 S 865-A17

 (49)
 Release the stabilizer-trim control-wheel-switches.

 S 865-A18

 (50)
 Let the control column go to the neutral position.

 S 865-A19

 (51)
 Put the RIGHT STAB TRIM SHUTOFF switch on the P10 panel to CUTOUT.

 (52)
 Put the CENTER STAB TRIM SHUTOFF switch on the P10 panel to NORM.

 S 865-A21

 (53)
 Move the first officer's stabilizer-trim control-wheel-switches up (airplane nose down).

 (a)
Make sure the stabilizer moves.

 S 865-A20
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A
757
MAINTENANCE MANUAL

 S 865-A22
 (54) While the switches are held up, slowly pull the control column aft until the stabilizer stops.
 NOTE: Do this step while the stabilizer indicated position is
____
 between 5.0 and 15.5 units of trim.

 S 225-A23
 (55)
 Measure the angle of travel of the control column from the neutral position to the point where the stabilizer stops. The angle of travel should be 2.2 to 2.7 degrees.

 S 865-A24

 (56)
 Let the control column go to the neutral position.

 S 865-A25

 (57)
 Hold the stabilizer-trim control-wheel-switches up (airplane nose down) until the stabilizer stops.

 S 865-A26

 (58)
 Release the stabilizer-trim control-wheel-switches.

 S 095-A27

 (59)
 Remove the elastic cord from around the lower ends of the captain's switch actuating arms. This will allow the captain's stabilizer-trim cutoff switches to operate.

 S 095-678

 (60)
 Remove the adapter equipment and protractor kit from the captain's control wheel (Fig. 505).

 S 865-A28

 (61)
 Pull the first officer's control column 3 to 4 inches (76-101 mm) aft and hold in position.

 S 865-A29

 (62)
 At the same time, push the captain's control column 3 to 4 inches (76-101 mm) forward and hold in position.

 S 865-A30

 (63)
 Move the captain's stabilizer-trim control-wheel-switches down (airplane nose up).

 (a)
Make sure the stabilizer moves.

 S 865-A31
 (64)
 Move the captain's stabilizer-trim control-wheel-switches up (airplane nose down).

 (a)
Make sure the stabilizer moves.
　
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