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WARNING: CAREFULLY REMOVE THE LEADING EDGE SLAT ACTUATOR LOCKOUT SET FROM
THE LEADING EDE SLATS. THE LEADING EDGE SLATS CAN MOVE QUICKLY. THIS
CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(10) Do this task: Leading Edge Flap and Slat Locks Removal, TASK 27-81-00-080-801.
SUBTASK 27-81-41-720-001
(11) Do this task: Leading Edge Flap and Slat Timing Test in Primary Mode,
TASK 27-81-00-700-802.
SUBTASK 27-81-41-710-002
(12) Do this task: Leading Edge Flap and Slat System Standby Actuation Operational Test ,
TASK 27-81-00-710-801.
SUBTASK 27-81-41-710-001
WARNING: MAKE SURE ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE FLIGHT CONTROL
SURFACES, THE THRUST REVERSERS, AND THE LANDING GEAR. THESE
COMPONENTS CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER.
THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(13) To pressurize hydraulic system B, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
(a) Operate the leading edge slats through a minimum of two cycles to bleed air from the
system.
NOTE: Leave the slats in the extended position.
(b) Make sure there are no hydraulic leaks from the slat actuator assembly [2] or the hydraulic
lines [29], [30] or [53], [54] with [40] and [41].
WARNING: MAKE SURE PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING EDGE
FLAPS AND SLATS. THE FLAPS AND SLATS WILL RETRACT. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(c) Move the flap control lever to the UP position to retract the leading edge slats.
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(d) To remove power from hydraulic system B, do this task: Hydraulic System A or B Power
Removal, TASK 29-11-00-860-805.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-81-41-860-011
(1) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 15 C01081 HYDRAULIC SYSTEM PTU VALVE CONT 1
A 16 C01085 HYDRAULIC SYSTEM PTU VALVE CONT 2
SUBTASK 27-81-41-940-001
(2) Install the applicable access panels:
(a) For the left wing, close these access panels:
Number Name/Location
521DB Lower Leading Edge Access Panel - Slat Station
71.38
521EB Lower Leading Edge Access Panel - Slat Station
98.95
521KB Lower Leading Edge Access Panel - Slat Station
188.12
521LB Lower Leading Edge Access Panel - Slat Station
216.76
521RB Lower Leading Edge Access Panel - Slat Station
307.75
521SB Lower Leading Edge Access Panel - Slat Station
337.62
521XB Lower Leading Edge Access Panel - Slat Station
435.91
521YB Lower Leading Edge Access Panel - Slat Station
467.98
(b) For the right wing, close these access panels:
Number Name/Location
621DB Lower Leading Edge Access Panel - Slat Station
71.38
621JB Lower Leading Edge Access Panel - Slat Station
188.14
621KB Lower Leading Edge Access Panel - Slat Station
216.71
621QB Lower Leading Edge Access Panel - Slat Station
307.75
621RB Lower Leading Edge Access Panel - Slat Station
337.62
621WB Lower Leading Edge Access Panel - Slat Station
435.91
621XB Lower Leading Edge Access Panel - Slat Station
467.98
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SUBTASK 27-81-41-410-003
(3) Close the applicable access doors:
(a) For the right wing, close this access panel:
Number Name/Location
621EB Defuel Access Panel - Slat Station 95.15
------------------------- END OF TASK ---------------------------
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Leading Edge Slat Actuator Preload Adjustment
Figure 402 (Sheet 1 of 2)/27-81-41-990-803
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Leading Edge Slat Actuator Preload Adjustment
Figure 402 (Sheet 2 of 2)/27-81-41-990-803
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737-600-700-800-900 飞机维护手册7 AIRCRAFT MAINTENANCE MANUA(87)
