(6)
Carefully remove the pitot probe (5) from the fuselage.
(7)
Remove and discard the gasket (4).
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R R Pitot Probe Figure 401/TASK 34-11-15-991-001
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TASK 34-11-15-400-001 Installation of the Pitot Probe (9DA1, 9DA2, 9DA3) WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
CAUTION : MAKE SURE THAT:
_______
-
THERE IS NO SIGN OF CORROSION OR DAMAGE ON THE EQUIPMENT
-
THERE IS NO FOREIGN OBJECT IN THE EQUIPMENT TO PREVENT ANY DAMAGE IN THE SYSTEM.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
B. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
4 gasket 34-11-01 03 -040 R 4 gasket 34-11-01 03 -040A
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C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-720-005 Check of the Electrical Bonding of the Different Components (But not the Fluid Systems and the Components Installed on Composite materials)
30-31-00-710-001 Operational Test of the Probe Ice Protection 34-11-15-200-001 Inspection/Check of the Pitot Probe (9DA1,9DA2,9DA3) 34-11-15-710-001 Test of the Pitot Probe (9DA1, 9DA2, 9DA3) without
the CFDS R 34-11-15-991-001 Fig. 401
3. Job Set-up
__________
Subtask 34-11-15-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position at zone 125 to get access to pitot probes 1 and 3 and at zone 126 to get access to pitot probe 2.
(2)
Make sure that the access door are open:
FOR 9DA1, 9DA3
812
FOR 9DA2
822
1EFF : ALL 1 34-11-15Page 406 1 1 May 01/05 1 1 1CES 1 Subtask 34-11-15-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU COM NAV/RADAR/1 5SQ1 K13
R **ON A/C 051-099,
R 121VU COM NAV/RADAR/2 5SQ2 K14
R **ON A/C ALL
FOR 9DA1 49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 49VU ANTI ICE/PROBES/PHC/1 2DA1 D03 49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02
122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13 122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12
FOR 9DA2 122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14 122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13 122VU ANTI ICE/PROBES/2/PHC 2DA2 Y12 122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11
FOR 9DA3 122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16 122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16 122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15 122VU ANTI ICE/PROBES/3/STATIC 5DA3 Z14
4. Procedure
_________
(Ref. Fig. 401/TASK 34-11-15-991-001)
Subtask 34-11-15-420-050
A. Installation of the Pitot Probe (9DA1, 9DA2, 9DA3)
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
1EFF : ALL 1 34-11-15Page 407 1 1 May 01/05 1 1 1CES 1
(3)
Install the new gasket (4) . NOTE : A second person is necessary to hold the pitot probe from the
____
outer side of the aircraft.
(4)
Carefully install the pitot probe (5). NOTE : You must turn the sensor element (6) to the front of the
____
aircraft.
(5)
Tighten the two nuts (3) from the inner side of the fuselage.
(6)
Remove the blanking cap from the electrical connector (2).
(7) 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 NAVIGATION 導航1(74)
