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庞巴迪环球5000公务机机组操作手册 Bombardier Global-飞行仪表(35)

时间:2011-11-10 10:29来源:蓝天飞行翻译 作者:公务机
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The FMS lateral deviation is a conventional CDI scale. The lateral deviation scale varies with the FMS approach sensitivity as follows:
.
±5 NM when the lateral scale factor is not valid

.
±2 NM when the FMS approach sensitivity is set.


The FMS lateral deviation is displayed when the primary navigation source is FMS. The FMS lateral deviation is not displayed in TO or GA modes.
Volume 2 Flight Crew Operating Manual Rev 7, Dec 01, 2005

VOR Lateral Deviation
The VOR lateral deviation scale is a conventional CDI scale. The VOR CDI is displayed when the primary navigation source is VOR. The VOR CDI is not displayed in TO or GA mode.

GF1110_089a
Marker Beacon
The marker beacon annunciation is displayed below the airplane reference and blinks when passing the outer, middle and inner marker beacons.
DME/FMS Distance Readout
The DME/FMS distance is located below the navigation source indication. The range is limited from 0 through 4096 NM with a resolution of 1 NM above 100 NM and of 0.1 NM below 100 NM.
The distance information is associated with the primary navigation source indication as follows:
.
VOR 1 or LOC 1 = DME 1 readout

.
FMS 1 = FMS readout

.
VOR 2 or LOC 2 = DME 2

.
FMS 2 = FMS readout


DME HOLD Annunciation
The DME HOLD annunciation is indicated by an “H”displayed at the left of the DME/FMS distance readout. It is displayed when the navigation source is VOR/LOC and DME HOLD has been selected
Rev 7, Dec 01, 2005 Flight Crew Operating Manual Volume 2
FLIGHT INSTRUMENTS
 
Waypoint ID
The waypoint identification consists of a maximum of 6 letters located below the DME/FMS distance readout. Depending on the navigation source selection, it displays the identifier of the DME radio frequency selected by the pilot or the next FMS waypoint. The waypoint identification is flashing when the it is overflown.
Marker Beacon Annunciation
DME HOLD
Annunciation DME/FMS

Waypoint Distance Readout Identification
Wind Data
The wind direction is displayed in vector format using a rotary arrow at the lower right side of the airspeed tape.
The wind speed is displayed as a digital readout. The wind speed readout is enabled with wind greater than 6 kt and is disabled when below 4 kt or when weight-on-wheels is applied.
GPWS Annunciations
The GPWS warning annunciations are located above the airplane reference. The windshear caution annunciation WNDSHR CAUTION is annunciated without a box below the airplane reference symbol.
The annunciations are displayed in the following priority:
Windshear Warning . WINDSHEAR
Command . PULL UP
Ground Proximity . GND PROX
Windshear Caution . WNDSHR CAUTION
GF1110_090a
Volume 2 Flight Crew Operating Manual Rev 7, Dec 01, 2005
 
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