B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02 105VU ELEC/CSM/G /EV AUTO/SPLY 7XE C01 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14 122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11 122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16 122VU ANTI ICE/PROBES/3/STATIC 5DA3 Z14 122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13
Subtask 34-13-00-860-055
C. Put the aircraft back to its initial configuration.
(1)
Do a reset of each ELAC:
- on the panel 49VU, open then close the ELAC1 C/B,
- on the panel 121VU, open then close the ELAC2 C/B.
(2)
Install the slip on covers on the static probes and on the pitot probes.
(3)
Make sure that the drain holes on the pitot probes are not blocked by unwanted materials. (Ref. TASK 34-11-15-200-001)
(4)
Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).
(5)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 34-13-00Page 552 1201-209, 1May 01/05 1 1 1CES 1R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
Post SB 34-1222 For A/C 001-049,101-105,151-158,201-209,
TASK 34-13-00-720-009-A
Functional Test of the Altitude and Airspeed Data (A/C with RVSM capability on three ADIRUs)
CAUTION : OBEY THESE PRECAUTIONS WHEN YOU DO THE TEST TO PREVENT DAMAGE TO
_______
INSTRUMENTS:
-PRESSURE SET MUST NOT BE MORE THAN 1050 hPa (31 in Hg) OR LESS THAN 115 hPa (3.39 in Hg)
-CHANGES IN PRESSURE MUST NOT BE MORE THAN 6000 FEET/MINUTE
-DO NOT SUDDENLY OPEN LINES TO AMBIENT AIR WHILE THE PRESSURE GENERATOR IS CONNECTED.
CAUTION : THE TOTAL PRESSURE IN THE PITOT SYSTEM MUST NEVER BE LESS THAN THE
_______ STATIC PRESSURE. THE DIFFERENCE BETWEEN THE PITOT AND THE STATIC PRESSURE CIRCUITS MUST NEVER BE MORE THAN 368 hPa (10.86 in Hg).
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 colored adhesive tape R No specific 1 GENERATOR - GROUND PRESSURE MINI. 100 MB (1.45 PSI) R TO 1400 MB (20.3 PSI)
36122 1 ADAPTOR-CHARGING,PITOT PROBE
98D34003500000 1 ADAPTER COVER-STATIC PORT
R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-13-00Page 553 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 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 27-50-00-866-009 Retraction of the Flaps on the Ground 31-60-00-860-001 EIS Start Procedure 34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-005 ADIRS Stop Procedure 34-11-15-200-001 Inspection/Check of the Pitot Probe (9DA1,9DA2,9DA3)
3. Job Set-up
__________
R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
Post SB 34-1252 For A/C 154-158,207-209,
Subtask 34-13-00-860-092
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (PFD DUs only) (Ref. TASK 31-60-00-860-001).
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