(W, A)  should be path and speed stable on approach. Gates are placed on the 3 Degree Reference Line or FMC Approach Glidepath Angle Line: . at 1000 feet above field elevation(W). . at 500 feet above field elevation(A). Decision gates that are below the missed approach waypoint altitude will not be displayed. 

 Flight path vector (W)  Fixed length line indicates current flight path angle and rotates about the point of the triangle. Angle of the line is dependent on the vertical speed and ground speed of the airplane. 
MCP selected  Dashed line indicates the selected vertical speed 

 vertical speed  as a target angle when the MCP V/S mode is 

 vector (M)  selected. Extends to the edge of the background display and rotates about the point of the triangle. 

Copyright . The Boeing Company. See title page for details.
10.41.16  June 1, 2005

Flight Instruments, Displays -PFD/ND Navigation Displays 737 Flight Crew Operations Manual
SYMBOL  NAME  REMARKS 

 Range to target speed dot (G)  Indicates where the airplane will achieve the FMC or MCP target speed. If the airplane is within 5 knots of the target speed the dot will be blanked. If the airplane increases 10 knots or more faster than the target speed the dot will reappear. Displayed at the end of the Flight Path Vector as an unfilled dot if the target speed will not be achieved within the vector length. 
NOLLA 2500  Waypoint altitude constraint: active (M), inactive (W)  At Altitude example. 
NOLLA 2500A  Waypoint altitude constraint: active (M), inactive (W)  At or Above Altitude example. 
NOLLA 2500B  Waypoint altitude constraint: active (M), inactive (W)  At or Below Altitude example. 
FL200B FL180A NOLLA  Waypoint altitude constraint: active (M), inactive (W)  Block Altitude example. 

Copyright . The Boeing Company. See title page for details.
June 1, 2005  10.41.17
Flight Instruments, Displays -PFD/ND Navigation Displays

Look-Ahead Terrain
SYMBOL  NAME  MODE  REMARKS 

 Terrain display (R, A, G, M)  MAP, MAP CTR, VOR, APP  Displays terrain data from the GPWS terrain data base. Color and density vary based on terrain height vs. airplane altitude. Refer to Chapter 15, Warning Systems. 

YD651 - YD655

 Terrain obstacle (R, A, G)  MAP, MAP CTR, VOR, APP  Obstacles are displayed from the GPWS data base and use the same display criteria as the terrain display. 
OBSTACLE  Obstacle annunciation (R, A)  All  Obstacle caution alert active (A), obstacle warning alert active (R). 

YD651 - YD655
TERR 060 030  Terrain mode annunciation (C) Terrain elevation (R,A,G)  MAP, MAP CTR, VOR, APP  Terrain display enabled (manual or automatic display). Terrain elevation displayed in hundreds of feet showing highest 
and lowest displayed terrain. 
Colors correspond to terrain 
display. 
Terrain elevation not displayed 
when terrain data unavailable. 

YA613 - YC413, YK101 - YK104
TERR  Terrain mode annunciation (C)  MAP, MAP CTR, VOR, APP  Terrain display enabled (manual or automatic display). 

TERR TEST  Terrain test mode annunciation (C)  All  GPWS operating in self-test mode. 
TERRAIN  Terrain annunciation (R, A)  All  Look-ahead terrain caution alert active (A), look-ahead terrain warning alert active (R). 

Copyright . The Boeing Company. See title page for details.
10.41.18  June 1, 2005

Flight Instruments, Displays -PFD/ND Navigation Displays 737 Flight Crew Operations Manual
SYMBOL  NAME  MODE  REMARKS 
TERR FAIL  Terrain status annunciations (A)  All  Look-ahead terrain alerting and display have failed. 
TERR POS  Terrain status annunciations (A)  All  Look-ahead terrain alerting and display unavailable due to position uncertainty. 
TERR INHIBIT  Terrain status annunciations (A)  All  GPWS terrain inhibit switch in TERR INHIBIT position. 
TERR RANGE DISAGREE  Terrain range status annunciations (A)  MAP, MAP CTR, VOR, APP  Terrain output range disagrees with selected EFIS control panel range. 
MAP/TERRRANGE DISAGREE  Terrain range status annunciations (A)  MAP, MAP CTR  Terrain output range and map display output range disagree with selected EFIS control panel range. 

Copyright . The Boeing Company. See title page for details.
June 1, 2005  10.41.19
Flight Instruments, Displays -PFD/ND Navigation Displays 737 Flight Crew Operations Manual

Predictive Windshear
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737NG機組操作手冊Flight Crew Operations Manual FCOM 3(47)