-
Bit at logic 1: the equipment is installed
(b) Transmission of identification message Every component connected to the maintenance centralized system transmits an identification message to facilitate and shorten the test procedures. The identification code assigned to the AMU is 6A. This information is transmitted in 32-bit word form in compliance with ARINC 429 with label 377. Word structure is as follows:
b31 b30 b29 b19 b18 b15 b14 b11 b10 b9 b8 b1 -------------------------------------------------------------------------------| | | | | | | | | | P | 0 0 | 0 0 0 0 0 0 0 0 0 0 0 | 6 | A | 0 | 1 | LABEL 377 | | | | | | | | | | -------------------------------------------------------------------------------
**ON A/C ALL
F. Power-up Tests Initialization and Cockpit Repercussions
(1) Conditions of power-up tests initialization
-How long the computer must be de-energized: 1 s.
-A/C configuration:
. Whatever the A/C configuration on ground
R 1EFF : ALL 1 23-51-00Page A18 1 1 May 01/05 1 1 1CES 1
(2)
Progress of power-up tests
-Duration: 1 s.
-Cockpit repercussions directly linked to power-up test accomplishment (some other repercussions may occur depending on the A/C configuration but these can be disregarded):
-None
(3)
Results of power-up tests (cockpit repercussions, if any, in case of tests pass/tests failed).
-
Tests pass:
. None
-
Tests failed:
. None
1EFF : ALL 1 23-51-00Page A19 1 1 May 01/05R 1 1 1CES 1
AUDIO MANAGEMENT (INTEGRATING/ FLIGHT INTERPHONE/SELCAL/CALL)
_____________________________________________________________ DEACTIVATION/REACTIVATION
_________________________
TASK 23-51-00-040-001
Deactivation of the Radio PTT Switch (11RN, 12RN)
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
1. Reason for the Job
__________________
Refer to the MMEL TASK: 23-51-08
Communications
Side Stick Radio selector
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific end caps
No specific warning notice
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 27-96-00-710-003 Operational Test of the Side Stick Priority 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply
29-10-00-864-003 Depressurize the Blue Hydraulic System
1EFF : ALL 1 23-51-00Page 401 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
29-24-00-864-001 Depressurize the Yellow Hydraulic System
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
34-10-00-860-004 IR Alignment Procedure
R ESPM 204213 R 23-51-00-991-001 Fig. 401
3. Job Set-up
__________
Subtask 23-51-00-865-055
A. Open, safety and tag this(these) circuit breaker(s):
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM Communications 通訊2(127)
