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SUBTASK 27-62-71-860-011
(3) Put the SPOILER A and B switches in the ON position.
SUBTASK 27-62-71-610-001
(4) Fill the hydraulic reservoirs if it is necessary. To fill, do this task: Hydraulic Reservoir
Servicing, TASK 12-12-00-610-801.
------------------------- END OF TASK ---------------------------
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TASK 27-62-71-000-802
4. Inboard Ground Spoiler Acutator Test
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-61-00-840-801 Put the Spoiler Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
27-62-00-800-801 Speed Brake Hydraulic Systems A and B Pressurization (P/B 201)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
COM-1691 Protractor - Digital, Vertical or Horizontal
(Part #: KS5549, Supplier: 75245, A/P Effectivity: 737-ALL)
C. 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
D. Prepare for the Test
SUBTASK 27-62-71-860-012
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-62-71-860-013
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 27-62-71-480-002
(3) Install the protractor, COM-1691 on the inboard ground spoilers 6 and 7.
SUBTASK 27-62-71-820-002
(4) Adjust the protractor, COM-1691 to zero.
E. Inboard Ground Spoiler Actuator Functional Test
SUBTASK 27-62-71-020-004
(1) Move the speed brake lever to the UP position to lift the spoilers.
SUBTASK 27-62-71-020-005
(2) Make sure the spoilers No. 6 and 7 are 52 +/-2 degrees up from the retracted position.
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SUBTASK 27-62-71-020-006
(3) Make sure the ground spoilers No. 6 and 7 align in the limit of 2 degrees.
SUBTASK 27-62-71-020-007
(4) Move the speed brake lever to the DOWN position to lower the spoilers.
SUBTASK 27-62-71-820-003
(5) Make sure the spoilers move to the fully retracted position.
SUBTASK 27-62-71-410-001
(6) Put the Airplane Back to Its Usual Condition
(a) Do this task: Put the Spoiler Hydraulic systems A and B Back to the Condition Before
the Pressurization, TASK 27-61-00-840-801.
(b) Remove the protractor, COM-1691 from the spoilers No. 6 and 7.
------------------------- END OF TASK ---------------------------
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OUTBOARD GROUND SPOILER - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the outboard ground spoilers referred to as .
(2) An installation of the outboard ground spoilers.
(3) A functional test of the outboard ground spoilers.
B. This procedure is applicable to the left and right outboard ground spoilers.
TASK 27-62-91-000-801
2. Outboard Ground Spoiler Removal
(Figure 401)
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-51-00-860-803 Extend 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)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
　
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