-Furthermore, the ground station provides a Morse identification.
1EFF : ALL 1 34-51-00Page 1 1 1 May 01/05 1 1 1CES 1
DME - Component Location
Figure 001
1EFF : ALL 1 34-51-00 Page 2
1 1 Feb 01/98
1 1
1CES 1
B. System Architecture (Ref. Fig. 002) The DME comprises two independent systems. Each system consists of: - one DME interrogator 2SD1 (2SD2), - one DME antenna 3SD1 (3SD2), - one dual VOR/DME Radio Magnetic Indicator (VOR/DME RMI) 11FN. The components given after can control the DME system: (Ref. Fig. 003)
-
the CAPT (F/O) Audio Control Panel (ACP) 2RN1 (2RN2) and the Audio Management Unit (AMU) 1RN for audio controls,
-
the Multipurpose Control and Display Unit 1(2) (MCDU) 3CA1 (3CA2), the Radio Management Panel 1(2) (RMP) 1RG1 (1RG2), and the Flight Management and Guidance Computer 1(2) (FMGC) 1CA1 (1CA2) for frequency/course selection,
-The MCDU and the Centralized Fault Display Interface Unit (CFDIU) 1TW
for test causes.
The DME data are shown on:
-
the CAPT and F/O Primary Flight Displays (PFD),
-
the CAPT and F/O Navigation Displays (ND),
-
the VOR/DME RMI,
-
the MCDU(s) (maintenance data).
C. Utilization Technical Data
(1) Data display
(Ref. Fig. 004)
(a)
On the PFDs With ILS/DME collocated stations, the ILS/DME distance is shown in magenta in the L lower corner of the PFD (Item 1). These data come into view when you push the ILS pushbutton switch located on the EFIS control section of the Flight Control Unit (FCU).
(b)
On the NDs The VOR/DME distance is shown in green in the L lower corner of the ND for DME system 1 (Item 2), and in the R lower corner of the ND for DME system 2 (Item 3) when:
-
you set the mode selector switch on the EFIS control section of the FCU to ROSE (ILS, VOR, NAV) or ARC,
-
you set the ADF/VOR/OFF switch to VOR.
In addition, when you push the VOR-D pushbutton switch on the
EFIS control section of the FCU, this causes:
display of the VOR/DME and DME ground stations which are not
already included in the flight plan, with the mode selector
switch in ROSE NAV and ARC positions:
-a circle for the DME station,
-circle plus cross symbol for the VOR/DME station.
R 1EFF : 001-049, 101-105, 151-199, 1 34-51-00Page 3 1 1 May 01/05 1 1 1CES 1
DME - Block Diagram Figure 002
R 1EFF : 1 1 1CES 001-049, 051-099, 101-105, 151-199, 1 111 34-51-00 Page 4 May 01/05
DME - Block Diagram Figure 002A
R 1EFF : 1 1 1CES 106-149, 201-299, 301-399, 401-499, 1 111 34-51-00 Page 5 Aug 01/05
INTENTIONALLY BLANK
1 1
34-51-00Page 6
1 1 Feb 01/99R 1 1
1CES 1
DME - Control and Indicating
Figure 003
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 34-51-00Page 7/8 1 1 May 01/05 1 1 1CES
1
DME - Control and Indicating
Figure 003A
R 1EFF : 106-149, 201-299, 301-399, 401-499, 1 34-51-00Page 9/10 1 1 Aug 01/05 1 1 1CES
1
DME - Data and Fault Displays
Figure 004
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 34-51-00Page 11 1 1 May 01/05 1 1 1CES 1
(c) On the VOR/DME RMI
Two windows are available for indication of both distances from
the DME 1 and DME 2 (Item 4) when the VOR/DME stations are
collocated.
When the DME or RMI monitoring circuits detect a fault, the
corresponding display window (Item 5) is blanked.
In case of No Computed Data (NCD) (out-of-range station) the
windows show white horizontal dashed lines (Item 6).
In addition, the LEDs on the face of the DME interrogator
indicate the status of the DME system.
(2) Audio control
The DME interrogator applies its audio output to the audio
integrating system. This system controls and directs the output to
the headsets and/or the loudspeakers. The pilot can control the DME
audio signals by pressing the VOR pushbutton switch on the ACP and
adjusting the related potentiometer to the correct audio level.
In case of collocated ILS/DME ground stations and when the ILS
pushbutton switch is pressed on the EFIS control section of the FCU,
the pilot can control the DME audio signal through the ILS pushbutton
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM NAVIGATION 導(dǎo)航4(78)
