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"CONTINUE" after you do the instructions that show on the CDU display.
1) INDEX
2) MAINT
3) DFCS
4) EXTENDED MAINTENANCE
5) RIGGING
6) ELEVATOR
7) CONTINUE
(d) Do the instructions that show on the CDU and push the LSK adjacent to these selections:
1) CONTINUE
2) ELEV RIG
(e) Make sure the BITE display values on the A and B sides are in the limit as shown below:
NOTE: During the BITE test, if the "CONTINUE" shows, then push the LSK that is adjacent
to "CONTINUE" after you do the instructions that show on the CDU display.
(f) Make sure that the mach trim actuator voltage is 0.00 +/- 0.20 VAC.
(g) Make sure that the flaps are in the full up position.
(h) Make sure that the values for the A side are between the limits that show on the CDU
display.
1) Test 51.03 MT ACT POS (VAC) limits: -0.20 to 0.20
(i) Push the INIT/REF key.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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(j) Cycle the pilot control column (full forward, full aft) to ensure elevator has full travel.
(k) Make sure the captain’s control column is at the neutral position.
(l) Make sure the right elevator trailing edge position is +/- 0.06 inch (1.5 mm) (+/-0.10 deg.)
with index plate.
NOTE: Use a straight edge on top of the elevator to make a line to the index plate.
SUBTASK 27-31-00-860-115
(2) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
SUBTASK 27-31-00-480-013
(3) Install the tool, SPL-1749 on both elevator PCU pistons.
NOTE: Make sure that the tool, SPL-1749 is installed correctly to prevent damage to the
lockwire.
SUBTASK 27-31-00-970-002
(4) Measure the distance that the PCU pogo clevis moves away from the end of the tube when
checking for extension.
SUBTASK 27-31-00-860-116
(5) Move the captain and first officer’s control column aft until all four elevator PCU pogos extend
approximately 0.3 inches (8 mm).
NOTE: Total column force will be approximately 140 pounds (623 newtons).
SUBTASK 27-31-00-860-117
(6) Remove the force on the control columns slowly.
SUBTASK 27-31-00-080-010
(7) Remove the tool, SPL-1749 from both elevator PCU pistons.
SUBTASK 27-31-00-860-118
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SPOILERS, SLATS, AND THRUST REVERSERS CAN MOVE
QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO
PERSONS AND DAMAGE TO EQUIPMENT.
(8) Do this task: Elevator Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
SUBTASK 27-31-00-860-119
(9) Cycle the pilot control column (full forward, full aft) to make sure the elevator has full travel.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-860-121
(1) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
SUBTASK 27-31-00-010-041
(2) Install this access panel:
Number Name/Location
318BR Tailcone Access Door
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-31-00-410-024
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
737-600/700/800/900
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Aileron/Elevator Power Control Unit (PCU) Input Rod Functional Test Tool
Figure 516/27-31-00-990-815
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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TASK 27-31-00-710-803
26. Elevator Power-Off Flight - Test
(Figure 520)
GUN 101-122
NOTE: See Figure 517.
GUN 156, 201-204, 206 PRE SB 737-55A1080
NOTE: See Figure 518.
GUN 001-099, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
NOTE: See Figure 519.
GUN ALL
A. General
(1) The flight test is necessary because the maintenance action can affect the flight characteristics
　
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