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(b) The captain’s stabilizer trim lightplate.
(c) The flap indicator lightplate.
(d) The speed brake lightplate.
SUBTASK 27-62-22-410-006
(16) Do this task: Captain’s and First Officer’s Seat Installation, TASK 25-11-01-400-801.
H. Put the Airplane Back to its Usual Condition:
SUBTASK 27-62-22-860-002
(1) Remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-1
Row Col Number Name
D 13 C00120 WEATHER RADAR RT
SUBTASK 27-62-22-860-003
(2) Remove the safety tags and close these circuit breakers:
CAPT Electrical System Panel, P18-1
Row Col Number Name
E 1 C00721 AUTOTHROTTLE DC 1
GUN 001-006, 155-157, 201-999
E 3 C01141 AUTOTHROTTLE DC 2
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EFFECTIVITY
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GUN 001-006, 155-157, 201-999 (Continued)
CAPT Electrical System Panel, P18-2
Row Col Number Name
GUN ALL
A 1 C00458 ENGINE 1 IGNITION RIGHT
A 3 C00153 ENGINE 1 IGNITION LEFT
A 4 C01390 ENGINE 1 ALTN PWR CHAN B
A 5 C01314 ENGINE 1 ALTN PWR CHAN A
B 1 C01316 ENGINE 1 START LEVER CHAN A
B 2 C01317 ENGINE 1 START LEVER CHAN B
B 4 C01003 ENGINE 1 THRUST REVERSER IND
B 5 C00276 ENGINE 1 THRUST REVERSER CONT
B 6 C01412 ENGINE 1 THRUST REVERSER INTLK
B 7 C01266 ENGINE 1 THRUST REVERSER SYNC LOCK
B 8 C01103 ENGINE 1 START VALVE
F/O Electrical System Panel, P6-2
Row Col Number Name
B 9 C00440 FLIGHT CONTROL AUTO SPEED BRAKE
F/O Electrical System Panel, P6-3
Row Col Number Name
E 5 C01320 ENGINE FUEL ENGINE 1 HPSOV CONT
E 6 C01395 ENGINE FUEL ENGINE 1 HPSOV IND
SUBTASK 27-62-22-860-004
(3) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 5 C01313 ENGINE 2 RUN/PWR
B 6 C01318 ENGINE 2 START LEVER CHAN A
B 7 C01319 ENGINE 2 START LEVER CHAN B
C 4 C00154 ENGINE 2 START VALVE
C 5 C01267 ENGINE 2 THRUST REVERSER SYNC LOCK
C 6 C01413 ENGINE 2 THRUST REVERSER INTLK
C 7 C00277 ENGINE 2 THRUST REVERSER CONT
C 8 C01004 ENGINE 2 THRUST REVERSER IND
D 4 C00459 ENGINE 2 IGNITION RIGHT
D 6 C00151 ENGINE 2 IGNITION LEFT
D 7 C01391 ENGINE 2 ALTN PWR CHAN B
D 8 C01315 ENGINE 2 ALTN PWR CHAN A
F/O Electrical System Panel, P6-3
Row Col Number Name
E 3 C01321 ENGINE FUEL ENGINE 2 HPSOV CONT
E 4 C01396 ENGINE FUEL ENGINE 2 HPSOV IND
SUBTASK 27-62-22-040-007
(4) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
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EFFECTIVITY
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SUBTASK 27-62-22-860-005
(5) Remove the DO-NOT-OPERATE tag from the engine start panel.
------------------------- END OF TASK ---------------------------
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AUTO SPEED BRAKE ACTUATOR - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the auto speed brake actuator.
(2) An installation of the auto speed brake actuator.
TASK 27-62-31-000-801
2. Auto Speed Brake Actuator Removal
(Figure 401)
A. References
Reference Title
27-62-00-800-802 Remove Pressure from the Speed Brake Hydraulic Systems A and B
(P/B 201)
B. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Access Panels
Number Name/Location
112A Forward Access Door
D. Prepare for the Removal
SUBTASK 27-62-31-860-001
(1) Do this task: Remove Pressure from the Speed Brake Hydraulic Systems A and B,
TASK 27-62-00-800-802.
SUBTASK 27-62-31-860-002
(2) Open this circuit breaker and install safety tag:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 9 C00440 FLIGHT CONTROL AUTO SPEED BRAKE
SUBTASK 27-62-31-860-003
(3) Put the speed brake lever in the DOWN position.
SUBTASK 27-62-31-010-002
(4) Remove the lower cover plate [21]:
(a) Remove the screws [19] and washers [20].
SUBTASK 27-62-31-010-001
(5) To get access the auto speed brake actuator assembly [16].
Open this access panel:
Number Name/Location
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737-600-700-800-900 飞机维护手册7 AIRCRAFT MAINTENANCE MANUA(4)
