R **ON A/C 051-099, 106-149, 204-299, 301-399, 401-499,
121VU AUTO FLT/FCU/2 9CA2 M21 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
R **ON A/C 062-099, 106-149, 204-299, 301-399, 401-499,
121VU ADIRS/ADIRU/2PWR/SHED 10FP N10 121VU ADIRS/ADIRU/3PWR/SWTG 9FP N09 121VU ADIRS/ADIRU/2/26VAC AND AOA 5FP2 N08 121VU ADIRS/ADIRU/3/26VAC AND AOA 5FP3 N07 121VU ADIRS/ADIRU/2/115VAC 4FP2 N06 121VU ADIRS/ADIRU/3/115VAC 4FP3 N05 121VU ADIRS/ADIRU/2/28VDC 6FP2 N04 121VU ADIRS/ADIRU/3/28VDC 6FP3 N03
R **ON A/C 051-099, 106-149, 204-299, 301-399, 401-499,
Subtask 34-13-00-865-098
D. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 105VU ELEC/CSM/G /EV AUTO/SPLY 7XE C01 121VU AUTO FLT/FAC2/28VDC 5CC2 M19
R 1EFF : 051-099, 106-149, 204-299, 301-399, 1 34-13-00Page A510 1401-499, 1Aug 01/05 1 1 1CES 1
4. Procedure
_________ Subtask 34-13-00-740-053
A. Read the CFDIU for the ADR INPUT STATUS NOTE : This test is for the system 1. For the systems 2 and 3, use the
____ indications between the parentheses. The actions and the results of this procedure occur on the MCDU used.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
Push the line key adjacent to the - the ADR 1(ADR 2)(ADR 3) page comes ADR 1(ADR 2)(ADR 3) indication. into view.
2.
Push the line key adjacent to the - the INPUT STATUS page 1/8 comes into
INPUT STATUS indication. view with the current on-the-ground status of the ADR1 (ADR2) (ADR3) parameters.
3.
Push the down arrow function key - the related pages come into view. to set the INPUT STATUS page 2/8 to 8/8.
4.
Push the line key adjacent to the - the test procedure stops. RETURN indication.
5.
Close-up
________ Subtask 34-13-00-410-062
A. Close Access
(1)
Install the protective cover on the battery power center 105VU.
(2)
Tighten the two screws.
(3)
Close the access door 822.
(4)
Remove the access platform(s).
R 1EFF : 051-099, 106-149, 204-299, 301-399, 1 34-13-00Page A511 1401-499, 1Aug 01/05 1 1 1CES 1 Subtask 34-13-00-860-086
B. Put the aircraft back to its initial configuration.
(1)
On the center pedestal, on the MCDU, push the line key adjacent to the RETURN indication until the MCDU MENU page comes into view.
(2)
Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).
(3)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
Subtask 34-13-00-865-099
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CC1, 5CC2
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___________________________
TASK 34-13-00-200-001
Visual Check of Pitot probes, Static ports and AOA sensors
1. Reason for the Job
__________________
R R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific 1 ACCESS PLATFORM 2M (6 FT)
No specific 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
34-10-00-170-001 Flushing of the Principal Total Pressure Lines 34-10-00-170-002 Flushing of the Principal Static Pressure Lines 34-10-00-170-003 Draining and Flushing of Standby Pneumatic Circuits 34-11-19-000-001 Removal of the Angle of Attack Sensor (3FP1, 3FP2,
3FP3) 34-11-19-200-001 Inspection Sensor Angle of Attack (3FP1, 3FP2, 3FP3) 34-11-19-400-001 Installation of the Angle of Attack Sensor (3FP1,
3FP2, 3FP3)
34-22-25-170-001 Draining and Flushing of the Standby Static and
Standby Total Pressure lines (ISIS)
1EFF : ALL 1 34-13-00Page 601 1 1 May 01/04 1 1 1CES 1 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 NAVIGATION 导航2(16)
