1200 FT
PWS WARNING PWS ALERTS ENABLED WHEN AUTO WHEN RADIO ALTIMETER SCALING BEGINS < 1200
400 FT 370 FT
PWS CAUTIONS INHIBITED RADIO ALTIMETER < 400 FT
50 FT PWS WARNINGS INHIBITED RADIO ALTIMETER < 50 FT
RUNWAY
GROUND
1.2 nm
APPROACH
Predictive Windshear System Operation
Figure 7

L09479
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH PWS ACTIVE ú

 34-43-00
 ú ú 08 Page 39 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 5)  The antenna scan pattern varies depending on the mode of operation. Above 1500 to 2300 feet, when the system is placed into a weather/windshear scan pattern, and no windshear is detected, the antenna scan pattern is as follow: a) Clockwise weather scan, with | 90 degrees of azimuth
 coverage and processing for weather.
 b)  Counterclockwise windshear scan, with full | 90 degrees of azimuth cover, but with windshear processing limited to the | 45-degree sector.
 6)  When the system is in a weather/windshear scan pattern, and the system detects a windshear event, the antenna scan pattern is as follows: a) Clockwise weather scan, from | 90 degrees. b) Counterclockwise windshear scan, from +90 degrees
 to -45 degrees, with windshear processing between | 45 degrees. c) The next clockwise scan is -45 degrees to +45 degrees, to validate windshear.
 d)  The next counterclockwise scan is from +45 to -90 degrees, to validate windshear. No processing occurs between -45 and -90 degrees.
 e)  Clockwise weather scan, -90 degrees to +90 degrees. The sequence is repeated as long as windshear event is detected.
 7) If a windshear event is not validated, the system reverts to the weather/windshear scan pattern first described.
 (f) PWS Flight Compartment Effects (Figure 9). 1) Windshear caution and warnings are displayed or annunciated on the navigation display (ND), primary flight display, captain's and first officer's warning speakers and the two master caution and warning lights. See Figure 9.
 2)  For both PWS cautions and warning alerts, a PWS ICON is shown on the WXR display. The size of the icon is proportional to the geographical size, but not in intensity, of the windshear event it represents.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 34-43-00
 ALL  ú ú 12 Page 40 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

POSITION  DIRECTION  RADAR SCAN  PAINT SWEEP  ANGLE (DEGREES)  TIME (SECONDS) 
SWEEP 1  L-R  BOTH WXR DATA UPDATED  BOTH WXR PAINTED  -90 TO +90  4 
SWEEP 2  R-L  BOTH WXR DATA UPDATED  BOTH WXR PAINTED  +90 TO -90  4 
SWEEP 3  L-R  BOTH WXR DATA UPDATED  BOTH WXR PAINTED  -90 TO +90  4 
SWEEP 4  R-L  BOTH WXR DATA UPDATED  BOTH WXR PAINTED  +90 TO -90  4 

NORMAL WXR SCAN PATTERN

POSITION  DIRECTION  RADAR SCAN  PAINT SWEEP  ANGLE (DEGREES)  TIME (SECONDS) 
SWEEP 1  L-R  BOTH WXR DATA UPDATED  BOTH WXR WITH ICON PAINTED  +90 TO -90  4 
SWEEP 2  R-L  UPDATED BOTH PWS DATA  BOTH PWS ICONS PAINTED  +90 TO -60  3 
SWEEP 3  L-R  BOTH WXR DATA UPDATED  BOTH PWS ICONS PAINTED  +60 TO -60  2 
SWEEP 4  R-L  BOTH PWS DATA UPDATED  BOTH PWS ICONS PAINTED  +60 TO -90  3 

WXR AND PWS SCAN PATTERN - TAKEOFF
PWS SWEEP

COLLECTION = |45`
Antenna Scan During Weather and Windshear Operation Figure 8 (Sheet 1)
L09482
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH PWS ACTIVE ú

 34-43-00
 ú ú 11 Page 41 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 導航 NAVIGATION 2(98)