B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 1RC1
49VU COM/VHF/1 2RC1 G09 FOR 1RC2
121VU COM NAV/VHF/2 2RC2 L04
R FOR 1RC3
R 121VU COM NAV/VHF/3 2RC3 L05
4. Procedure
_________
(Ref. Fig. 401/TASK 23-12-33-991-001)
Subtask 23-12-33-420-050
A. Installation of the VHF Transceiver
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Remove the blanking caps from the electrical connectors (1).
(4)
Make sure that the electrical connectors (1) are clean and in the correct condition.
(5)
Install the VHF transceiver (5) on its rack (2).
(6)
Push the VHF transceiver (5) on its rack (2) to connect the electrical connectors(1).
(7)
Engage the nuts (3) on the lugs (4) and tighten.
Subtask 23-12-33-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 1RC1 2RC1 FOR 1RC2 2RC2
1EFF : ALL 1 23-12-33Page 405 1 1 Feb 01/99 1 1 1CES 1
FOR 1RC3
2RC3
Subtask 23-12-33-740-050
C. Do the BITE test of the VHF system (Ref. TASK 23-12-00-740-001) NOTE : As an alternative procedure, you can do this operational test
____
without the CFDS (Ref. TASK 23-12-00-710-001).
5. Close-up
________
Subtask 23-12-33-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R (2) Close the access door 824 (Ref. TASK 52-41-00-410-002).
(3) Remove the access platform(s).
1EFF : ALL 1 23-12-33Page 406 1 1 Feb 01/02 1 1 1CES 1
RADIO MANAGEMENT - DESCRIPTION AND OPERATION
____________________________________________
1.
General
_______ The radio management panels (RMP) centralize radio communication (VHF, HF) frequency control. They can also serve as backups of the flight management and guidance computers (FMGC) for radio navigation frequencies control (VOR, DME, ILS, ADF(if installed)). The aircraft is equipped with three RMPs which are identical and interchangeable.
2.
Component Location
__________________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
(Ref. Fig. 001)
R **ON A/C 106-149, 218-299, 301-399, 401-499,
(Ref. Fig. 001A)
**ON A/C ALL
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
-------------------------------------------------------------------------------1RG1 RMP-COM/NAV FREQ SEL, 1 11VU 211 831 23-13-13 1RG2 RMP-COM/NAV FREQ SEL, 2 11VU 211 831 23-13-13 1RG3 RMP-COM FREQ SEL, 3 20VU 211 831 23-13-13 3CA1 MCDU-1 11VU 211 831 22-82-12 3CA2 MCDU-2 11VU 211 831 22-82-12
1EFF : ALL 1 23-13-00Page 1 1 1 Aug 01/05 1 1 1CES 1
Radio Management - Component Location
Figure 001
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-13-00Page 2 1201-217, 1May 01/05 1 1 1CES 1
Radio Management - Component Location
Figure 001A
R 1EFF : 106-149, 218-299, 301-399, 401-499, 1 23-13-00Page 3 1 1 Aug 01/05 1 1 1CES 1 3. System Description
__________________
(Ref. Fig. 002, 003)
The radio management system is linked to:
-
The VHF and HF radio-communication equipment (Ref. 23-12 and 23-11)
-
The VOR, DME, ADF (if installed) and ILS radio-navigation equipment (Ref. 34-55, 34-51, 34-53 and 34-36)
-
The Flight Management and Guidance Computers (FMGC) (Ref. 22-83)
-
The Centralized Fault-Display Interface-Unit (CFDIU) (Ref. 31-32)
-
The Landing Gear Control and Interface Unit (LGCIU) (Ref. 32-31).
4.
Electrical Power Supply
_______________________ (Ref. Fig. 004) The RMP1 is supplied with 28VDC from the 28VDC ESS bus 4PP (sub-busbar 401PP) through 3A circuit breaker 2RG1 on the overhead panel 49VU (in the cockpit). The RMP1 is supplied by the emergency system. The RMP2 is supplied with 28VDC from the 28VDC bus 2PP (sub-busbar 204PP) through 3A circuit breaker 2RG2 on the rear circuit breaker panel 121VU (in the cockpit). The RMP3 is supplied with 28VDC from the 28VDC bus 1PP (sub-busbar 103PP) through 3A circuit breaker 2RG3 on the rear circuit breaker panel 121VU (in the cockpit). 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM Communications 通讯1(82)
