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737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-62-71
Page 402
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Ground Spoiler Actuator Installation
Figure 401 (Sheet 1 of 2)/27-62-71-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-62-71
Page 403
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Inboard Ground Spoiler Actuator Installation
Figure 401 (Sheet 2 of 2)/27-62-71-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-62-71
Page 404
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-62-71-400-801
3. Inboard Ground Spoiler Actuator Installation
(Figure 401)
A. References
Reference Title
12-12-00-610-801 Hydraulic Reservoir Servicing (P/B 301)
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)
27-62-00-820-804 Ground Spoiler Adjustment (P/B 501)
27-62-00-840-801 Put the Speed Brake Hydraulic systems A and B Back to the
Condition Before the Pressurization (P/B 201)
27-62-00-840-802 Put the Speed Brake Systems A and B Back to the Condition Before
the Pressure Removal (P/B 201)
B. Consumable Materials
Reference Description Specification
D00633 Grease - Aircraft General Purpose BMS3-33
C. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
7 Pin 27-62-71-01-195 GUN ALL
16 Pin 27-62-71-01-195 GUN ALL
17 Actuator 27-62-71-01-225 GUN ALL
D. Location Zones
Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
552 Left Wing - Spoiler No. 6
652 Right Wing - Spoiler No. 7
E. Actuator Installation
SUBTASK 27-62-71-420-001
(1) Install the actuator [17]:
(a) Remove the caps from the hydraulic ports of the actuator [17].
(b) Put the actuator [17] in its position and make sure the hydraulic lines [10] align with the
fittings.
(c) Connect the actuator [17] rod end to the inboard ground spoiler [1]:
1) Apply grease, D00633 to the bolt [2].
2) Install bolt [2] with the head outboard, washer [3], bushing [4], washer [5], nut [6], and
pin [7].
3) Tighten nut to 450-690 pound-inches (50.8-78.0 newton-meters).
(d) Connect the actuator [17] to the structure:
1) Apply grease, D00633 to the bolt [2].
2) Install bolt [11] with the head outboard, washer [12], bushing [13], washer [14], nut [15],
and pin [16].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-62-71
Page 405
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
3) Tighten nut to 450-690 pound-inches (50.8-78.0 newton-meters).
SUBTASK 27-62-71-420-002
(2) Connect the hydraulic lines [10] to the actuator [17]:
(a) Remove the plugs from the hydraulic lines [10].
(b) Connect the hydraulic lines [10] to the actuator [17].
(c) Tighten the hydraulic fittings.
SUBTASK 27-62-71-860-006
(3) Do this task: Put the Speed Brake Systems A and B Back to the Condition Before the
Pressure Removal, TASK 27-62-00-840-802.
SUBTASK 27-62-71-860-007
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.
(4) Do this task: Speed Brake Hydraulic Systems A and B Pressurization,
TASK 27-62-00-800-801.
SUBTASK 27-62-71-870-001
(5) Move the speed brake control lever through its full cycle to bleed the spoiler actuators.
SUBTASK 27-62-71-700-001
(6) Make sure there are no leaks at the hydraulic lines.
SUBTASK 27-62-71-860-008
(7) Do the adjustment of the outboard ground spoiler acutator. To adjust it, do this task: Ground
Spoiler Adjustment, TASK 27-62-00-820-804.
SUBTASK 27-62-71-820-001
(8) Do this task: Inboard Ground Spoiler Acutator Test, TASK 27-62-71-000-802.
F. Put the Airplane Back to Its Usual Condition.
SUBTASK 27-62-71-860-009
(1) Do this task: Retract the Trailing Edge Flaps, TASK 27-51-00-860-804.
SUBTASK 27-62-71-860-010
(2) 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.
　
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