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F/O Electrical System Panel, P6-1
Row Col Number Name
D 13 C00120 WEATHER RADAR RT
SUBTASK 27-62-00-700-005
(14) Move the No. 2 thrust lever to the fully forward position.
(a) Make sure the speed brake lever moves to the DOWN position.
(b) Make sure the spoilers move to the retracted position.
(c) Make sure the ARMED and the DO NOT ARM lights are off.
SUBTASK 27-62-00-860-201
(15) Release the ENABLE/VERIFY switch and the toggle switch.
SUBTASK 27-62-00-860-202
(16) Set the rotary switch on the antiskid/autobrake control unit to the NORM position.
SUBTASK 27-62-00-860-203
(17) Move the No. 2 thrust lever back to the idle position.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-62-00-860-204
(18) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-1
Row Col Number Name
D 13 C00120 WEATHER RADAR RT
F/O Electrical System Panel, P6-2
Row Col Number Name
B 14 C01070 FLIGHT CONTROL AUTOSLAT DC 2
C 14 C01068 FLIGHT CONTROL AUTOSLAT DC 1
F/O Electrical System Panel, P6-3
Row Col Number Name
D 15 C01401 LANDING GEAR AIR/GND RELAY
SUBTASK 27-62-00-860-205
(19) Do this task: Put the Speed Brake Hydraulic systems A and B Back to the Condition Before
the Pressurization, TASK 27-62-00-840-801.
------------------------- END OF TASK ---------------------------
TASK 27-62-00-820-807
13. Speed Brake Antiskid Inoperative Test
(Figure 507)
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-62-00-800-801 Speed Brake Hydraulic Systems A and B Pressurization (P/B 201)
27-62-00-840-801 Put the Speed Brake Hydraulic systems A and B Back to the
Condition Before the Pressurization (P/B 201)
B. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
118 Electrical and Electronics Compartment - Right
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
C. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
D. Prepare for the Test
SUBTASK 27-62-00-860-064
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
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EFFECTIVITY
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SUBTASK 27-62-00-860-065
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Do this task: Speed Brake Hydraulic Systems A and B Pressurization,
TASK 27-62-00-800-801.
SUBTASK 27-62-00-860-066
(3) Open these circuit breakers and install safety tags:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 14 C01070 FLIGHT CONTROL AUTOSLAT DC 2
C 14 C01068 FLIGHT CONTROL AUTOSLAT DC 1
SUBTASK 27-62-00-860-067
(4) Move the thrust levers No. 1 and 2 to the idle position.
SUBTASK 27-62-00-860-068
(5) Make sure the airplane is on its landing gear or compress the right main gear strut a minimum
of 5 inches (127 mm).
NOTE: This will open the ground spoiler interlock valve.
SUBTASK 27-62-00-860-069
(6) Make sure the ground spoilers are in the down position.
SUBTASK 27-62-00-860-070
(7) Make sure the speed brake lever is in the DOWN position.
SUBTASK 27-62-00-860-211
WARNING: MAKE SURE THAT YOU OPEN THE CIRCUIT BREAKER FOR THE WEATHER RADAR
SYSTEM. THE FORWARD MOVEMENT OF A THRUST LEVER CAN CAUSE THE
AUTOMATIC OPERATION OF THE SYSTEM. THE OPERATION OF THIS SYSTEM CAN
CAUSE SERIOUS INJURY TO PERSONS AND DAMAGE TO EQUIPMENT IN THE AREA
OF THE NOSE RADOME.
(8) Open this circuit breaker and install safety tag:
F/O Electrical System Panel, P6-1
Row Col Number Name
D 13 C00120 WEATHER RADAR RT
SUBTASK 27-62-00-860-071
(9) Move one of the thrust levers to the full forward position to retract the speed brake actuator.
SUBTASK 27-62-00-860-072
(10) Move the thrust lever to the idle position.
SUBTASK 27-62-00-010-002
(11) Open this access panel:
Number Name/Location
117A Electronic Equipment Access Door
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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