B. Procedure
S 864-023
(1) Open this circuit breaker and attach a DO-NOT-CLOSE tag:
(a) P6 Load Control Center - Right
1) WEATHER RADAR R/T
S 034-008
(2) Disengage the quick-release fasteners on the WXR control panel.
S 034-075
CAUTION: CAREFULLY REMOVE THE CONTROL PANEL FOR THE AFT OR FORWARD
_______ ELECTRONICS CONTROL STAND. THIS WILL PREVENT DAMAGE TO THE ELECTRICAL CABLES AT THE REAR OF THE CONTROL PANEL.
(3)
Pull the WXR control panel carefully out from the control stand to get to the electrical connector.
S 034-010
(4)
Disconnect the airplane electrical connector from the WXR control panel.
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737-300/400/500MAINTENANCE MANUAL
S 024-003
(5)
Remove the WXR control panel.
S 034-011
(6)
Put the dust caps on the WXR control panel and the airplane electrical connector.
TASK 34-41-91-404-073
3. Weather Radar Control Panel Installation
________________________________________
A. References
(1)
24-22-00/201, Manual Control
(2)
34-41-02/501, Weather Radar Systems
B. Access
(1) Location Zone
101/102 Control Cabin, LH
C. Procedure
S 864-034
(1) Make sure this circuit breaker is open with a DO-NOT-CLOSE tag attached:
(a) P6 Load Control Center - Right
1) WEATHER RADAR R/T
S 434-012
(2) Connect the airplane electrical connector to the WXR control panel.
S 424-076
CAUTION: CAREFULLY INSTALL THE WXR CONTROL PANEL INTO THE AFT OR FORWARD
_______ ELECTRONIC CONTROL STAND. THIS WILL PREVENT DAMAGE TO THE ELECTRONIC CABLE AT THE REAR OF THE WXR CONTROL PANEL.
(3) Install the control panel in the aft or forward electronics control stand.
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A 737-300/400/500MAINTENANCE MANUAL
(4) S 434-014Engage the quick-release fastener on the WXR control panel.
(5) S 864-046Remove the DO-NOT-CLOSE tag and close this circuit breaker: (a) P6 Load Control Center - Right 1) WEATHER RADAR R/T
(6) S 714-065Do the operational test of the weather radar system (Ref 34-41-02/501).
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1.
2.
3.
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737-300/400/500MAINTENANCE MANUAL
GROUND PROXIMITY WARNING SYSTEM - DESCRIPTION AND OPERATION
___________________________________________________________
General
_______
A. The ground proximity warning system (GPWS) provides the pilots with aural and visual warning of potentially dangerous flight paths relative to the ground. The GPWS processes radio altitude information from the No. 1 low range radio altimeter (LRRA), mach signal and altitude rate information from the central air data computer (CADC), glide slope deviation information from VOR/ILS system and landing gear and landing flap position signals to provide warnings of the following hazards:
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本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊 導(dǎo)航 NAVIGATION 3(99)
