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1) Use the force gauge, COM-1557 to make sure the force required to keep the control
column at this position is 36 - 45 pounds (160 -200 newtons).
(q) Move the captain’s control column slowly forward until the elevator trailing edge is at 1.15 -
1.25 inches (29.2 - 31.7 mm) from the neutral position, and hold (Figure 523).
1) Use the force gauge, COM-1557 to make sure the force required to keep the control
column at this position is 17.0 - 27.5 pounds (75.6 - 122.3 newtons).
(r) Move the captain’s control column slowly forward until the elevator trailing edge is at 4.75 -
4.85 inches (120.6 - 123.2 mm) from the neutral position, and hold (Figure 523).
1) Use the force gauge, COM-1557 to make sure the force required to keep the control
column at this position is 44 - 53 pounds (196 - 236 newtons).
(s) Set the FLT CONTROL A switch to the ON position.
CAUTION: DO NOT INCREASE THE PRESSURE TO MORE THAN 6 PSIG (474 KNOTS KCAS)
DURING THE TEST. IF THE PRESSURE IS MORE THAN 6 PSIG, IT CAN CAUSE
DAMAGE TO THE ELEVATOR FEEL COMPUTER.
(t) Operate the regulator, SPL-1742 or air data model test set, COM-1914 to increase the
pressure to 2.42 - 2.52 psig (16.7 - 17.3 kPa) (315 knots).
(u) Move the captain’s control column slowly aft until the elevator trailing edge is at 1.15 - 1.25
inches (29.2 - 31.7 mm) from the neutral position, and hold (Figure 523).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 596
Feb 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
1) Use the force gauge, COM-1557 to make sure the force required to keep the control
column at this position is 28 - 44 pounds (125 - 196 newtons).
(v) Move the captain’s control column slowly forward until the elevator trailing edge is at 1.15 -
1.25 inches (29.2 - 31.7 mm) from the neutral position, and hold.
1) Use the force gauge, COM-1557 to make sure the force required to keep the control
column at this position is 30 - 46 pounds (133 - 205 newtons).
(w) Set the FLT CONTROL B switch to the OFF position.
(x) Move the captain’s control column slowly aft until the elevator trailing edge is at 1.15 - 1.25
inches (29.2 - 31.7 mm) from the neutral position, and hold.
1) Use the force gauge, COM-1557 to make sure the force required to keep the control
column at this position is 28 - 44 pounds (125 - 196 newtons).
(y) Move the captain’s control column slowly forward until the elevator trailing edge is at 1.15 -
1.25 inches (29.2 - 31.7 mm) from the neutral position, and hold.
1) Use the force gauge, COM-1557 to make sure the force required to keep the control
column at this position is 30 - 46 pounds (133 -205 newtons).
(z) Set the FLT CONTROL B switch to the ON position.
(aa) Set the FLT CONTROL A switch on the forward overhead panel, P5 to the OFF position.
(ab) Move the captain’s control column slowly aft until the elevator trailing edge is at 1.15 - 1.25
inches (29.2 - 31.7 mm) from the neutral position, and hold.
1) Use the force gauge, COM-1557 to make sure the force required to keep the control
column at this position is 28 - 44 pounds (125 - 196 newtons).
(ac) Move the captain’s control column slowly forward until the elevator trailing edge is at 1.15 -
1.25 inches (29.2 - 31.7 mm) from the neutral position, and hold.
1) Use the force gauge, COM-1557 to make sure the force required to keep the control
column at this position is 30 - 46 pounds (133 - 204 newtons).
(ad) Set the FLT CONTROL A and B switches to the OFF position.
(ae) Operate the regulator, SPL-1742 or air data model test set, COM-1914to decrease the
pressure to 0.0 psig (0.0 kPa) (0 knots).
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-730-013
(1) Do a test of the autopilot authority in the elevator rigging test. To do this test, do this task:
Elevator Rigging Test, TASK 22-11-00-820-802.
SUBTASK 27-31-00-080-009
(2) At the two pitot probes on the vertical fin, do the following:
(a) Remove the pressure lines from the air data model test set, COM-1914 or regulator,
SPL-1742 from the pitot probes.
(b) Remove the seal from the drain hole in each pitot probe.
SUBTASK 27-31-00-430-003
(3) Inside the aft unpressurized compartment, do the following:
(a) If you used the regulator, SPL-1742, or equivalent, for the test, do the following:
1) Disconnect the pressure gage lines of the regulator, SPL-1742, or equivalent, from the
drain holes of the pitot lines.
(b) If you used the air data model test set, COM-1914 for the test, do the following:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
　
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