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747-400 MAINTENANCE MANUAL
MAGENTA
RED
MESSAGE MODE ANTENNA TILT MESSAGE TEST PASS MESSAGE HALF RANGE MESSAGE TEST WXR TEST +15 20 YELLOW GREEN FAIL TEST FAIL MESSAGES FAIL RT ANT CON ATT WEAK WXR
ND TEST PASS DISPLAY ND TEST FAIL DISPLAY 1
WX TEST PASS/ DEFECTIVE WXR TEST
TEST FAIL LRU(S) CONDITION PATTERN
(YELLOW) (CYAN)
WXR TEST BLANK TEST PASSED ON
WXR FAIL T/R RECEIVER/TRANSMITTER FAULT OFF/ON
WXR FAIL ANT ANTENNA FAULT OFF
WXR FAIL CTL CONTROL PANEL FAULT OFF
WXR FAIL ATT ATTITUDE INPUT FAULT ON
WXR FAIL WEAK CALIBRATION FAULT ON
ND TEST PASS/TEST FAIL MESSAGES
1 DISPLAY SHOWS TEST PATTERN REMOVED FOR CERTAIN R/T FAULTS. SOME R/T FAULTS WILL NOT REMOVE TEST PATTERN
Weather Radar Test Displays and PWS Test Sequence Figure 501 (Sheet 1)
K24571
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
VISUAL AND AURAL TEST MESSAGES TEST TIMING 0-2 SECONDS 2-12 SECONDS
ND (AMBER) WINDSHEAR OFF OFF
ND & PFD WINDSHEAR (RED) OFF ON
LIGHT MASTER WARNING OFF ON
UPPER EICAS WINDSHEAR SYS (ADVISORY) ON OFF
LOWER EICAS WINDSHEAR PRED (STATUS) ON OFF
AURAL DISPLAY MONITOR RADAR WINDSHEAR AHEAD, WINDSHEAR AHEAD
DISPLAY TEST PATTERN TEST PATTERN
Weather Radar Test Displays and PWS Test Sequence
Figure 501 (Sheet 2)
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H81001
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747-400 MAINTENANCE MANUAL
TASK 34-43-00-745-170
3. Ground Test - Weather Radar System__________________________________
A. General
(1)
The ground test does an analysis of the self-test results from the R/T monitor circuits. A PASS or FAIL message shows on the CDU.
(2)
To perform this ground test the weather radar must be in a radiate mode. See the Prepare for the Test steps below for the radiate restrictions.
(3)
If it is necessary to test the weather radar system in a non-radiate mode, the self test part of the weather radar operational test must be performed.
B. References
(1)
24-22-00/201, Manual Control
(2)
34-21-00/201, Inertial Reference System
C. Access
(1) Location Zones
221 Control Cabin, Left
222 Control Cabin, Right
D. Prepare for the Test
S 865-119
(1)
Supply electrical power (AMM 24-22-00/201).
S 865-181
(2)
Close these circuit breakers:
(a) P7 Overhead Circuit Breaker Panel
1) 7C7 WXR L RT
2) 7C19 WXR R RT
S 865-172
(3)
Set the WXR switch/indicator on the captain's and first officer's EFIS control panels to the on position.
S 865-165
(4)
Set the SYS switch on the WXR control panel to one of these positions:
(a) 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 導(dǎo)航 NAVIGATION 2(111)
