B.
Access
(1)
Location Zone
205 Electronic Compartment
C.
Remove the Leading Edge Flaps and Slats Position Indication Module
S 864-004
(1)
Open these circuit breakers and attach DO-NOT-REMOVE tags:
(a)
P6 Panel
1) LE FLAP POS IND
S 024-003
(2) Remove the indication module from the shelf (AMM 20-10-07/201).
TASK 27-88-41-404-002
3. Leading Edge Flaps and Slats Position Indication Module Installation
____________________________________________________________________
A. References
(1)
AMM 20-10-07/201, E/E Rack-Mounted Components - Maintenance Practices
(2)
AMM 27-88-00/501, Leading Edge Flap and Slat Position Indication System
(3)
AMM 27-88-11/501 Leading Edge flap and Slat Proximity Sensor
(4)
AMM 27-88-41/501 Leading Edge Flaps and Slats Position Indication Module
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A
737-300/400/500MAINTENANCE MANUAL
LE DEVICES ANNUNCIATOR LE FLAP AND
PANEL
Leading Edge Flap and Slat Position Indication Module Installation
Figure 401
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A
737-300/400/500MAINTENANCE MANUAL
B. Access
(1)
Location Zone
205 Electronic Compartment
C.
Install the Leading Edge Flaps and Slats Position Indication Module
S 424-006
(1)
Carefully install the indication module on the equipment rack (AMM 20-10-07/201).
S 864-005
(2)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
P6 Panel
1) LE FLAP POS IND
S 714-008
(3)
AIRPLANES WITH POSITION INDICATION MODULE WITH OR WITHOUT BUILT-IN-TEST-EQUIPMENT; Do the operational test of the leading edge flap and slat position indicating system (AMM 27-88-00/501 or AMM 27-88-11/501 for modules without BITE. AMM 27-88-41/501 for modules with BITE).
S 744-010
(4)
AIRPLANES WITH POSITION INDICATION MODULE WITH
BUILT-IN-TEST-EQUIPMENT;
Do the built-in-test-equipment (BITE) test of the position
indication module (AMM 27-88-41/501).
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A
737-300/400/500MAINTENANCE MANUAL
LEADING EDGE FLAPS AND SLATS POSITION INDICATION MODULE - ADJUSTMENT/TEST
__________________________________________________________________________
1. General_______
A. This procedure contains two tasks. The first task is the operational test of the leading edge flaps and slats position indication module. The second task is the built-in-test-equipment (BITE) test of the position indication module.
TASK 27-88-41-715-003
2. Leading Edge Flaps and Slats Position Indication Module - Operational Test___________________________________________________________________________
A. References
(1)
AMM 24-22-00/201 Manual Control
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 6(167)
