MCP Selected Vertical Speed (V/S)
Displays the selected vertical speed as a dashed target angle line when the MCP V/S mode is selected.
Vertical Flight Path Vector
Indicates current flight path angle as a function of vertical speed and ground speed. The length of the vector is fixed at one half of the VSD range.
Range to Target Speed Dot (RTSD)
Indicates where the airplane will achieve the FMC or MCP target speed.
.
dot is blanked within 5 knots of target speed.
.
dot reappears if speed increases 10 knots or more faster than target speed.
.
replaced with an unfilled dot at vector end if target speed will not be
achieved within length of the vertical flight path vector line.
3-Degree Reference Line
Displayed for approaches that do not have a designated approach angle.
.
dashed line extends 10 NM for situational awareness.
.
anchored to the runway threshold.
.
for reference only, line may intersect terrain.
Decision Gates
Displayed on the FMC approach glidepath angle line or 3 degree reference line at 500 feet and 1000 feet above field elevation.
Runway
Represents the selected runway.
Copyright . The Boeing Company. See title page for details.
10.11.56 March 28, 2005
Flight Instruments, Displays -PFD/ND – Displays
Vertical Situation Display (VSD) - Terrain Background
Terrain Profile Line
Represents the highest terrain within the enroute swath.
.
highest points of the terrain below and ahead of the airplane.
.
terrain is depicted so the true altitude separation between the airplane and
terrain is shown.
.
terrain behind the airplane is drawn equal to the terrain at the current
position.
.
VSD terrain uses the same color coding that is used to depict EGPWS
terrain on the lateral map:
.
green: terrain 250-500 feet or more below the airplane.
.
amber: terrain from 250-500 feet below to 2000 feet above the
airplane.
.
red: terrain more than 2,000 feet above the airplane.
Vertical Support Lines
Vertical terrain vectors placed at constant intervals along the terrain profile line.
Copyright . The Boeing Company. See title page for details.
Flight Instruments, Displays -PFD/ND – Displays
737 Flight Crew Operations Manual
Navigation Displays – Approach Mode Expanded and Center Approach Modes
YC153, YC154
7
1 152 080o/12 160 GS TAS MAGHDG 090 ILS 1 110.10 CRS 055 DME 13.5
8
2
40
9
10 3
ADF 1 VOR 2
KXYZ ELN DME28.5
EXPANDED APPROACH MODE
GS152 TAS160 ILS 1 IALT
4
080o/12 CRS 055
11
DME 13.5
HDG
MAG 090
103 12
5
ADF 1 VOR 2
6
KXYZ ELN DME28.5
CENTER APPROACH MODE
Copyright . The Boeing Company. See title page for details.
10.11.58 March 28, 2005
Flight Instruments, Displays -PFD/ND – Displays
737 Flight Crew Operations Manual
YA613 - YA809, YC411 - YK104
7
GS152 TAS 160 ILS 1 110.10
MAG
090
CRS055
080o/12 HDG DME13.5
1 82
40
9
WX+T
+15
VAR
10 3
ADF 1 VOR 2
KXYZ ELN DME28.5
EXPANDED APPROACH MODE
GS152 TAS160 ILS 1 IALT
4
080o/12 CRS 055
11
DME 13.5
HDG
090
MAG
103 12
5
ADF 1 VOR 2
6
KXYZ ELN DME28.5
CENTER APPROACH MODE
Copyright . The Boeing Company. See title page for details.
June 1, 2005 10.11.59
Flight Instruments, Displays -PFD/ND – Displays 737 Flight Crew Operations Manual
Wind Direction/Speed/Arrow Selected Heading Bug Selected Course Pointer Groundspeed/True Airspeed Airplane symbol VOR/ADF Selection/Ident or Frequency/VOR DME Current Heading Magnetic/True Reference Track Line Localizer Deviation Indication and Scale Reference ILS Frequency or Ident/Course/DME Glideslope Pointer and Scale
Copyright . The Boeing Company. See title page for details.
10.11.60 March 28, 2005
Flight Instruments, Displays -PFD/ND – Displays
737 Flight Crew Operations Manual
Navigation Displays – VOR Mode Expanded and Center VOR Modes
YC153, YC154
7
GS315 TAS 312 VOR 2 116.80
090
MAG CRS055
350o/15 HDG DME13.5
1 82
40
9
10
TO
3
ADF 1 VOR 2
KXYZ ELN DME13.5
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