曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

weight is set with the speed reference selector)
* V1 (decision speed)
* VR (rotation speed)
* Selected speed (indicates the airspeed manually set in the
IAS/MACH display on the DFCS mode control panel (MCP)
or the FMC computed airspeed when the IAS/MACH window
is blank)
* V2 (single engine climb speed)
* V2+15 (single engine climb speed plus 15 knots)
* Flap maneuver speed (maneuver speed for flap position
shown. It does not show for 30 or 40 units of flap.)
* Flaps up speed (shows after zero fuel weight is set in the
CDU and takeoff gross weight is calculated, or after takeoff
gross weight is set with the speed reference selector)
* Airspeed bug at 80 knots (this shows during preflight and is
removed when the flaps start to retract).
Approach/Landing
This data can show on the PFD speed tape during approach:
* REF (landing reference speed VREF is set on the CDU
APPROACH REF page or set with the speed reference
selector)
* VREF+15 (this shows after VREF is set)
FMCS - DISPLAYS - CDS - AIRSPEED INDICATION
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.99
D633A101-SHZ1 Oct 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-047
* Flap maneuver speed (maneuver speed for flap position
shown).
FMCS - DISPLAYS - CDS - AIRSPEED INDICATION
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.100
D633A101-SHZ1 Oct 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-047
FMCS - DISPLAYS - CDS - AIRSPEED INDICATION
FMCS - DISPLAYS - CDS - AIRSPEED INDICATION
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.101
D633A101-SHZ1 Oct 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-047
General
The FMCS provides the navigation data for the MAP mode
displays on the common display system (CDS). There are two
types of navigation data, dynamic data and background data.
Dynamic data changes as a function of time while background
data is stationary data that does not move as a function of time.
The FMCS formats and transmits the data (FMC bus 08 and
FMC bus 09) to show the airplane position with respect to the
flight plan and vertical profile. The CDS controls symbol color,
size, and brightness.
Map Mode
The map mode shows the progress of the flight and is the
normal display the crew uses for navigation in flight. This
display may show in either the expanded mode or the centered
mode. The display is dynamic and moves as the airplane
moves.
Symbol Definitions
This data is shown:
* Active waypoint distance (distance to go to the active
waypoint. White)
* Active waypoint ETA (estimated time of arrival for the active
waypoint. White)
* T/C altitude profile point (top of climb position in the active
route. Green)
* T/D altitude profile point (top of descent position in the active
route. Green)
* E/D altitude profile point (end of descent position in the
active route. Green)
* S/C altitude profile point (step climb position in the active
route. Green)
* Speed profile point (deceleration point in the active route.
Green)
* Active waypoint (next waypoint in the active route. Magenta)
* Range to altitude arc (range at which the airplane will reach
the MCP altitude. Green)
* Trend vector (predicted position of airplane at the end of 30,
60 or 90 second intervals. White)
* Inactive waypoint (waypoint other than the active waypoint in
the active route. White)
* Vertical deviation scale (vertical deviation from the
calculated descent profile. Scale is white and pointer is
magenta)
* Map options (options selected on the EFIS control panel.
Cyan)
* Wind data (wind speed and direction. White)
* Map source (source of dynamic and background data.
Green)
* Navaids (navigation stations within the selected map area.
Cyan)
* Off route waypoints (waypoints within the selected map area
but not in the active route. Cyan)
* Airports (airports within the selected map area. Cyan)
* Route data (altitude constraints and ETAs for the waypoint in
the active route. Magenta or white)
* Track angle (airplane track. White).
FMCS - DISPLAYS - CDS - MAP DISPLAY
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.102
D633A101-SHZ1 Oct 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737NGAMM4(16)