-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
- or on the panel 122VU, open the circuit breaker 3DA2
- or on the panel 122VU, open the circuit breaker 3DA3.
3.
Close the circuit breaker(s) that you opened before.
4.
On the overhead panel, on the PROBE/WINDOW HEAT section of the panel 25VU:
-release the AUTO pushbutton switch
5. Close-up________
Subtask 34-11-15-860-052
- on the panels 131VU and 132VU, theMASTER CAUT lights come on
-you can hear the single chime
- on the upper ECAM display unit the ANTI ICE F/O PITOT indication comes into view.
- on the panels 131VU and 132VU, theMASTER CAUT lights come on
-you can hear the single chime
- on the upper ECAM display unit the ANTI ICE STBY PITOT indication comes into view.
- on the panels 131VU and 132VU, theMASTER CAUT lights go off.
- on the upper ECAM display unit, the indication given above goes out of view.
- on the upper ECAM display unit, the MEMO page comes into view.
The ON legend goes off.
A. Put the aircraft back to its initial configuration.
(1)
On the center pedestal, on the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(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).
1EFF : ALL 1 34-11-15Page 503 1 1 Feb 01/98 1 1 1CES 1 PROBE - PITOT (9DA1,9DA2,9DA3) - INSPECTION/CHECK
_________________________________________________
TASK 34-11-15-200-001
Inspection/Check of the Pitot Probe (9DA1,9DA2,9DA3)
1.
Reason for the Job
__________________
Self Explanatory
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 access platform 1.6 m (5 ft. 3 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
34-11-15-000-001 Removal of the Pitot Probe (9DA1, 9DA2, 9DA3) (for corrective action) 34-11-15-400-001 Installation of the Pitot Probe (9DA1, 9DA2, 9DA3) (for corrective action)
**ON A/C 001-049, 051-099, 101-105, 151-199,
34-11-15-991-002 Fig. 601 R **ON A/C 106-149, 201-299, 301-399, 401-499,
34-11-15-991-002-B Fig. 601A
1EFF : ALL 1 34-11-15Page 601 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
3. Job Set-up
__________
Subtask 34-11-15-865-053
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 9DA1
49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02 FOR 9DA2 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14 FOR 9DA3 122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16
Subtask 34-11-15-860-054
B. Aircraft Maintenance Configuration
(1)
Put the access platform in position in Zone 125 to get access to the pitot probes 1 and 3 and in Zone 126 to get access to the pitot probe
2.
(2)
Remove the cover of the pitot probe.
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-105, 151-199,
(Ref. Fig. 601/TASK 34-11-15-991-002) R **ON A/C 106-149, 201-299, 301-399, 401-499,
(Ref. Fig. 601A/TASK 34-11-15-991-002-B)
1EFF : ALL 1 34-11-15Page 602 1 1 Aug 01/05 1 1 1CES 1
Pitot Probe Tip Configuration
Figure 601/TASK 34-11-15-991-002
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 34-11-15Page 603 1 1 May 01/05 1 1 1CES 1
Pitot Probe Tip Configuration Figure 601A/TASK 34-11-15-991-002-B
R 1EFF : 106-149, 201-299, 301-399, 401-499, 1 34-11-15Page 604 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 001-049, 051-099, 101-105, 151-199,
中國航空網(wǎng) m.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1(76)
