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WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SPOILERS, SLATS, AND THRUST REVERSERS CAN MOVE
QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO
PERSONS AND DAMAGE TO EQUIPMENT.
(1) Pressurize elevator hydraulic systems A and B. To pressurize them, do this task: Elevator
Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
SUBTASK 27-31-00-860-151
(2) Make sure the flaps are in the full up position.
SUBTASK 27-31-00-860-106
(3) Make sure the control column is in the neutral position.
SUBTASK 27-31-00-760-001
(4) Make sure that these circuit breakers are closed:
CAPT Electrical System Panel, P18-1
Row Col Number Name
E 5 C01009 ADIRU LEFT DC
E 7 C01007 ADIRU LEFT AC
CAPT Electrical System Panel, P18-2
Row Col Number Name
E 5 C01204 SMYD-1 CMPTR DC
E 6 C01205 SMYD-1 SNSR EXC AC
F/O Electrical System Panel, P6-1
Row Col Number Name
B 4 C01207 SMYD-2 SNSR EXC AC
B 5 C01206 SMYD-2 CMPTR DC
C 14 C01008 ADIRU RIGHT AC
C 17 C01010 ADIRU RIGHT DC
E. Operational Test - Elevator Tab Control System
GUN ALL; AIRPLANES WITH THE 10 SECOND TIME DELAY ELEVATOR TAB CONTROL VALVE
SUBTASK 27-31-00-730-014
(1) Do the operational test - elevator tab control system:
(a) Move and hold the control column full aft.
1) Make sure that the elevator tabs move down.
(b) Move and hold the control column full forward.
1) Make sure that the elevator tabs move up.
(c) Release the control column.
(d) Cycle the control column and return it to neutral.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 504
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN ALL; AIRPLANES WITH THE 10 SECOND TIME DELAY ELEVATOR TAB CONTROL VALVE
(Continued)
(e) Open this circuit breaker and install safety tag:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 8 C01464 FLIGHT CONTROL ELEV TAB VLV RIGHT
(f) Set the flaps to the 5 degree position.
(g) Move and hold the control column full forward.
1) Make sure that the left elevator tab is below the elevator and the right elevator tab is
above the elevator.
(h) Remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 8 C01464 FLIGHT CONTROL ELEV TAB VLV RIGHT
1) Make sure there is an 8-12 second time delay before the right elevator tab begins to
move.
(i) Cycle the control column full forward and full aft.
1) Make sure that both elevator tabs move in the same direction as the elevators.
GUN ALL
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-860-107
(1) Set the flaps to the full up position.
SUBTASK 27-31-00-860-108
(2) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
------------------------- END OF TASK ---------------------------
TASK 27-31-00-710-802
4. Elevator Control Column Override - Operational Test
A. General
(1) Use this task to do a quick check of the elevator control column override assembly.
B. References
Reference Title
27-31-00-800-801 Elevator Hydraulic System A and B - Pressurization (P/B 201)
27-31-00-840-801 Put the Elevator Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
C. Location Zones
Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 505
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
D. Procedure
SUBTASK 27-31-00-860-101
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SPOILERS, SLATS, AND THRUST REVERSERS CAN MOVE
QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO
PERSONS AND DAMAGE TO EQUIPMENT.
(1) Do this task: Elevator Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
SUBTASK 27-31-00-710-006
(2) Do an operational test of the elevator control column override:
(a) Override Test of the First Officer’s Control Column:
1) Push the captain’s and first officer’s control columns forward.
2) Hold the captain’s control column forward (against the forward stop).
3) Pull the first officer’s control column aft.
　
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本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊2(132)