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(AACU).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-62-00-860-125
(4) At the same time that you push and hold the ENABLE/VERIFY button, move the PRESS/TEST
toggle switch up to the TEST position on the AACU.
(a) Make sure the speed brake lever moves to the UP position.
(b) Make sure the ground and flight spoilers move to the up position.
(c) Make sure the SPEED BRAKE ARMED light stays on.
NOTE: The SPEED BRAKE DO NOT ARM light will come on momentarily if you do not
push the buttons at the same time.
SUBTASK 27-62-00-860-126
(5) Release the buttons.
(a) Make sure the SPEED BRAKE ARMED light is off.
(b) Make sure the SPEED BRAKE DO NOT ARM light comes on.
SUBTASK 27-62-00-860-177
(6) Move the No. 1 reverse thrust lever to the stowed position.
SUBTASK 27-62-00-860-127
(7) Move the No. 1 thrust lever forward.
(a) Make sure the speed brake control lever moves to the DOWN position.
(b) Make sure the ground and flight spoilers move to the full down position.
(c) Make sure the SPEED BRAKE DO NOT ARM light goes off.
(d) Make sure the SPEED BRAKE ARMED light comes on then goes off when the speed brake
control lever gets to the DOWN position.
SUBTASK 27-62-00-860-128
(8) Move the No. 1 thrust lever to the idle position.
SUBTASK 27-62-00-860-129
(9) Do the RTO test again with the No. 2 reverse thrust lever.
SUBTASK 27-62-00-860-192
(10) Move the TEST SELECTOR switch to the NORM position on the AACU.
SUBTASK 27-62-00-860-224
(11) Check the engine 1 reverser light on the P5 panel. If it is on, do this task: Thrust Reverser
Engine Accessory Unit (EAU) Test, TASK 78-31-00-700-804-F00.
NOTE: The engine 1 reverser light can come on while doing Speed Brake RTO Test if there is
a pressure drop in the Hydraulic System A.
(12) Move the engine ignition switches from CONTINUOUS to OFF.
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-62-00-860-130
(1) 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.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Oct 10/2006
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SUBTASK 27-62-00-860-131
(2) 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
SUBTASK 27-62-00-010-005
(3) Close this access panel:
Number Name/Location
117A Electronic Equipment Access Door
------------------------- END OF TASK ---------------------------
TASK 27-62-00-820-810
16. Speed Brake Extended Light Test
A. General
(1) Ignore the illumination of the SPEED BRAKE ARMED and SPEED BRAKE DO NOT ARM Lights
during this test.
B. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (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)
32-09-00-860-801 Put the Airplane in the Air Mode (P/B 201)
32-09-00-860-802 Return the Airplane to the Ground Mode (P/B 201)
C. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
D. Speed Brakes Extended Light Test
SUBTASK 27-62-00-860-132
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-62-00-860-133
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 27-62-00-860-134
(3) Open these circuit breakers and install safety tags:
　
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