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F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-62-61-860-046
(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.
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SUBTASK 27-62-61-860-047
(2) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
------------------------- END OF TASK ---------------------------
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Ground Spoiler Interlock Valve Tool Setup
Figure 502/27-62-61-990-803
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TASK 27-62-61-400-806
4. Ground Spoiler Interlock Valve Proximity Sensor Functional Test
(Figure 501)
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)
29-11-00-860-805 Hydraulic System A or B Power Removal (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
SPL-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
D. Access Panels
Number Name/Location
112A Forward Access Door
E. Prepare for the Test
SUBTASK 27-62-61-860-024
(1) Remove system A and B hydraulic power. To remove, do this task: Hydraulic System A or B
Power Removal, TASK 29-11-00-860-805
SUBTASK 27-62-61-020-014
(2) Remove nut [5], washer [4], washer [3] and bolt [2] to disconnect lower slider assembly [6] from
the lug on the right landing gear strut.
SUBTASK 27-62-61-980-001
(3) Retract the lower slider assembly [6].
SUBTASK 27-62-61-480-002
(4) Install rig pin S/B-3 from the rig pin kit, SPL-1585 through the yoke of the interlock valve.
SUBTASK 27-62-61-860-025
(5) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
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SUBTASK 27-62-61-010-001
(6) Open this access door:
Number Name/Location
112A Forward Access Door
F. Ground Spoiler Interlock Valve Proximity Sensor Functional Test
SUBTASK 27-62-61-740-001
(1) Use the PSEU BITE to test the sensor.
(a) Push the ON/OFF switch on the PSEU BITE display.
(b) Push the down arrow until OTHER? is displayed.
(c) Push the YES switch to select OTHER?.
(d) Push the down arrow until SENSOR RIGGING? is displayed.
(e) Push the YES switch to select SENSOR RIGGING?.
(f) Push the down arrow until the sensor number (S1050) is displayed.
1) Make sure the PSEU display shows the sensor clearance within tolerance.
(g) Push the MENU switch.
(h) Push the down arrow until OTHER? is displayed.
(i) Push the YES switch to select OTHER?.
(j) Push the down arrow until I/O MONITOR is displayed.
(k) Push the YES switch to select I/O MONITOR.
(l) Push the down arrow until the sensor number (S1050) is displayed.
SUBTASK 27-62-61-080-001
(2) Remove rig pin S/B-3 from the rig pin kit, SPL-1585 from the interlock valve yoke.
SUBTASK 27-62-61-860-026
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
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737-600-700-800-900 飞机维护手册7 AIRCRAFT MAINTENANCE MANUA(22)
