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////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
LOCKING HYDRAULIC ACTUATOR (RIGHT SIDE)
SEE B LOCKING HYDRAULIC ACTUATOR (LEFT SIDE) FWD SEE
A 3. FEEDBACK LVDT ELECTRICAL CONNECTORS
2. UPPER RETRACT
HYDRAULIC LINE1. UPPER FLEX
SHAFT TORQUE BOX (REF)
9. TUBE NUT
FWD
GIMBAL RING
13. STOP
BRACKET
11. LOCKING HYDRAULIC ACTUATOR
4. GIMBAL RING
10. ACTUATOR LOCK RETAINER
PROXIMITY SENSOR 9. TUBE NUT
SEE C
8. EXTEND
5. LOWER RETRACT HYDRAULIC
HYDRAULIC LINE LINE
7. LOWER FLEX 6. LOCK
SHAFT LEVER
LOCKING HYDRAULIC ACTUATOR
(LEFT SIDE)
A
Locking Hydraulic Actuator Installation
Figure 402 (Sheet 1)
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3. FEEDBACK LVDT CONNECTORS ELECTRICAL
4. GIMBAL RING RETAINER 2. UPPER RETRACT HYDRAULIC LINE
GIMBAL RING 1. UPPER FLEX SHAFT
6. LOCK LEVER
TORQUE BOX (REF) 8. EXTEND HYDRAULIC LINE
9. TUBE NUT
5. LOWER RETRACT HYDRAULIC LINE 10. ACTUATOR SENSOR PROXIMITY LOCK
9. TUBE NUT SEE C
FWD 7. LOWER FLEX SHAFT 11. LOCKING ACTUATOR HYDRAULIC
LOCKING HYDRAULIC ACTUATOR (RIGHT SIDE) SEE D
B
Locking Hydraulic Actuator Installation
Figure 402 (Sheet 2)
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C76403
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
12. FEEDBACK LVDT
10. ACTUATOR LOCK SEE D PROXIMITY SENSOR TORQUE BOX (REF)
6. LOCK LEVER
FLEXSHAFT (REF)
RETRACT HYDRAULIC LINE (REF)
18. DEPLOY PROXIMITY
13. PROXIMITY SENSOR
SENSOR WIRE
14. WIRE
15.
BOLT
CLAMPS
16.
WASHER (2)
17.
NUT (3 LOCATIONS)
C
FULL RETRACT 0.060
POSITION 0.030
1
FEEDBACK FULL EXTENDSTOP POSITIONBOLT
0.060
0.030 FEEDBACK
STOP
1 BOLT
STOP 11. LOCKING STOP 11. LOCKING
BRACKET HYDRAULIC BRACKET HYDRAULIC
ACTUATOR ACTUATOR
RETRACTED POSITION EXTENDED POSITION
LOCKING HYDRAULIC ACTUATOR FEEDBACK CHECK (BOTTOM VIEW)
D
1
ALL DIMENSIONS ARE IN INCHES
Locking Hydraulic Actuator Installation
Figure 402 (Sheet 3)
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S 844-014-N00
CAUTION:_______IMMEDIATELY CLEAN ALL OF THE HYDRAULIC FLUID THAT FALLS. THE HYDRAULIC FLUID CAN CAUSE CONTAMINATION OF THE AIRPLANE OR THE ENGINE.
(7) Drain the hydraulic fluid from the actuator system (Fig. 403).
(a)
Put an applicable container below the lower hydraulic actuator
(7) to catch the hydraulic fluid (Fig. 403).
(b)
Loosen the flexhose couplings for the extend line and retract line at the strut hydraulic connection.
NOTE: This is done to let air into the actuator system at a
____ high point to drain the hydraulic fluid.
(c)
Remove the sync lock (8) from the lower non-locking hydraulic actuator (7) (Fig. 403) (AMM 78-34-13/401).
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本文链接地址：747-400 AMM 飞机维护手册 EXHAUST 2(35)
