(2)
 Clean draining hole of the pitot probe 3 with CLEANER - PITOT PROBE

 (3)
 Make sure that there is no contamination in the pressurized gas at these outlets:

 -L static probe 3 and R static probe 3
 -Pitot probe 3
 -Water drain
 -Pipe of the cabin-pressure detection pressure-switch.

 (4)
 Put an ADAPTER COVER-STATIC PORT on the L static probe 3 then on the R static probe 3.

 (5)
 Make sure that the flow of gas is correct at :

 -
the pipe of the pressure switch

 -
the water drain.

 (6)
 Stop the flow of gas.

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 **ON A/C 001-049, 051-099, 101-105,

 Subtask 34-10-00-860-054
 B. Put the aircraft back to its initial configuration.
 (1)
 Disconnect the dry nitrogen source.

 (2)
 Remove the adapters.

 (3)
 Install the water drain plug (2) on the water drain (1).

 (4)
 Remove the blanking cap from the pressure switch 14WN (3).

 (5)
 Connect the static pipe to the pressure switch 14WN (3).

 (6)
 Connect the quick-disconnect coupling (8) to the ADM 19FP3 and the quick-disconnect coupling (4) to the ADM 19FP8.

 NOTE : After the connection:
____
 -make sure that a colored ring is shown on the quick-disconnect couplings (4) and (8)
 -pull the connectors to be sure that they are correctly attached.
 (7) Install the standby airspeed indicator (Ref. TASK 34-21-26-400-001) the standby altimeter (Ref. TASK 34-21-22-400-001) and the metric altimeter (15FN) (Ref. TASK 34-21-25-400-001) on the center instrument panel.
 (8) Release the hoses. R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 34-10-00-860-054-A
 B. Put the aircraft back to its initial configuration.
 (1)
 Disconnect the dry nitrogen source.

 (2)
 Remove the adapters.

 (3)
 Install the water drain plug (2) on the water drain (1).

 (4)
 Remove the blanking cap from the pressure switch 14WN (3).

 1EFF : ALL 1 34-10-00Page 318 1 1 Aug 01/05 1 1 1CES 1

 (5)
 Connect the static pipe to the pressure switch 14WN (3).

 (6)
 Connect the quick-disconnect coupling (8) to the ADM 19FP3 and the quick-disconnect coupling (4) to the ADM 19FP8.

 NOTE : After the connection:
____
 -make sure that a colored ring is shown on the quick-disconnect couplings (4) and (8)
 -pull the connectors to be sure that they are correctly attached.
 (7) Install the standby airspeed indicator (Ref. TASK 34-21-26-400-001) and the standby altimeter (Ref. TASK 34-21-22-400-001) on the center instrument panel.
 (8) Release the hoses. **ON A/C ALL
 Subtask 34-10-00-790-052
 C. Leak test
 (1)
 Make sure that all the hoses are connected correctly.

 (2)
 Do a leak test of the standby air data system
 (Ref. TASK 34-21-00-790-001).

 5. Close-up
________ Subtask 34-10-00-410-061
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 (3)
 Close the access door 811.

 (4)
 Remove the access platform(s).

 1EFF : ALL 1 34-10-00Page 319 1 1 May 01/05R 1 1 1CES 1

 AIR DATA/INERTIAL REFERENCE SYSTEM (ADIRS) - DEACTIVATION/REACTIVATION
______________________________________________________________________
R
 TASK 34-10-00-040-002
 ADIRS - Check of all Flight Control Accelerometers for Correct Operation
 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 34-10-01
 Air data inertial reference
 ADIRS
 ADIRS (FAA Only)

 2. Job Set-up Information
______________________
 A. 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
 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
　
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