(a)
P6 Panel
1) FLAP LOAD RELIEF
S 014-003
(2)
Remove the right stabilizer trim wheel from the control stand:
(a)
Remove the retaining nut from the stabilizer trim wheel.
(b)
Remove the stabilizer trim wheel from the shaft.
NOTE: Do not remove the shaft.
____
S 014-012
(3)
Remove the right upper door from the control stand:
(a)
Remove the screws from the upper right door.
(b)
Turn the upper door up until you can get access to the wires for the lightplate.
(c)
Remove the wires from the lightplate.
(d)
Remove the door.
(e)
Replace the nuts and washers on the lightplate studs.
S 024-004
(4)
Remove the flap 40-unit switches:
(a)
Remove the mounting nuts and washers from the switches.
(b)
Remove the switches from the mounting screws.
(c)
Remove the wires from the switch.
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A
737-300/400/500MAINTENANCE MANUAL
SEE A
UPPER RIGHT
DOOR
INBD FWD
RETAINING
RIGHT NUT
STABILIZER
TRIM WHEEL
FLAP 40-UNIT
SWITCHES MOUNTING NUT
AND WASHER
(2 LOCATIONS)
FLAP 40-UNIT SWITCHES
A
Flap 40-Unit Switches Installation
Figure 401
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A
737-300/400/500MAINTENANCE MANUAL
TASK 27-51-94-404-005
3. Flap 40-Unit Switches Installation (Fig. 401)__________________________________
A. References
(1)
27-51-94/501, Flap 40-Unit Switches
B.
Access
(1)
Location Zone
101, 102 Control Cabin
C.
Procedure
S 424-006
(1)
Install the flap 40-unit switches:
(a)
Attach the wires to the switches.
(b)
Install the switches on the mounting screws.
(c)
Install the washers and nuts on the mounting screws.
S 824-007
(2)
Do this task: "Flap 40-unit Switches Adjustment" (Ref 27-51-94/501).
S 724-008
(3)
Do this task: "Operational Test - Flap 40-unit Switches" (Ref 27-51-94/501).
S 414-009
(4)
Install the upper right door on the control stand:
(a)
Install the wires on the lightplate studs.
(b)
Install the door on the control stand.
(c)
Install the screws on the door.
S 414-010
(5)
Install the right stabilizer trim wheel on the control stand:
(a)
Put the stabilizer trim wheel on the shaft with the handle 90 | 15 degrees from the left trim wheel handle.
(b)
Install the retaining nut on the trim wheel.
S 864-011
(6)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
P6 Panel
1) FLAP LOAD RELIEF
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27-51-94
ALL ú ú 01 Page 403 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 5(7)
