曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
or Standby Rudder Power Control Unit Deadband Test, TASK 27-21-00-700-818-002.
SUBTASK 27-21-24-710-002
(11) Do this task: Rudder Travel Test, TASK 27-21-00-700-817-001 or Rudder Travel Test,
TASK 27-21-00-700-817-002.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-21-24-410-001
(1) Install this access panel:
Number Name/Location
324DL Trailing Edge Access
SUBTASK 27-21-24-410-003
(2) If it is necessary, do this task: Hydraulic Reservoir Servicing, TASK 12-12-00-610-801.
------------------------- END OF TASK ---------------------------
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STANDBY RUDDER POWER CONTROL UNIT - INSPECTION/CHECK
1. General
A. This procedure contains these tasks:
(1) Standby Rudder Power Control Unit General Visual Inspection
(2) Standby Rudder Power Control Unit Detail Visual Inspection.
TASK 27-21-24-210-801
2. Standby Ruddder Power Control Unit (with Hydraulic Power on) General Visual Inspection
A. References
Reference Title
27-21-00-800-801 Rudder Hydraulic System A, B, or Standby Pressurization (P/B 201)
27-21-00-800-802 Remove Pressure from the Rudder Hydraulic Systems A, B, and
Standby (P/B 201)
B. Location Zones
Zone Area
325 Vertical Fin - Rudder
C. Access Panels
Number Name/Location
324DL Trailing Edge Access
D. Procedure
SUBTASK 27-21-24-010-003
(1) Open this access panel:
Number Name/Location
324DL Trailing Edge Access
SUBTASK 27-21-24-860-007
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, 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) Pressurize the Standby Hydraulic System, do this task: Rudder Hydraulic System A, B, or
Standby Pressurization, TASK 27-21-00-800-801.
SUBTASK 27-21-24-210-001
(3) Do a general visual inspection of the standby rudder power control unit.
SUBTASK 27-21-24-860-006
(4) Remove pressure from the Standby Hydraulic System, do this task: Remove Pressure from the
Rudder Hydraulic Systems A, B, and Standby, TASK 27-21-00-800-802.
SUBTASK 27-21-24-410-004
(5) Close this access panel:
Number Name/Location
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(Continued)
Number Name/Location
324DL Trailing Edge Access
------------------------- END OF TASK ---------------------------
TASK 27-21-24-210-802
3. Standby Ruddder Power Control Unit Detail Visual Inspection
A. Location Zones
Zone Area
325 Vertical Fin - Rudder
B. Access Panels
Number Name/Location
324DL Trailing Edge Access
C. Procedure
SUBTASK 27-21-24-010-004
(1) Open this access panel:
Number Name/Location
324DL Trailing Edge Access
SUBTASK 27-21-24-210-002
(2) Do a detail visual inspection of the standby rudder power control unit attachment points,
(Figure 601).
(a) Examine the attachment points for security and damage.
SUBTASK 27-21-24-410-005
(3) Close this access panel:
Number Name/Location
324DL Trailing Edge Access
------------------------- END OF TASK ---------------------------
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Standby Rudder Power Control Unit Visual Inspection
Figure 601/27-21-24-990-802
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RUDDER PEDALS - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the rudder pedals
(2) An installation of the rudder pedals.
B. This procedure is applicable for the captain’s rudder pedals and first officer’s rudder pedals.
TASK 27-21-31-000-801
2. Rudder Pedals Removal
(Figure 401, Figure 402)
A. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(86)
