1EFF : ALL 1 34-52-00Page 507 1 1 May 01/04R 1 1 1CES 1

 (3)
 Install the ATC ground test unit in the cockpit. Put the antenna of the ATC ground test unit at 50 cm (approx. 2 ft) from the ATC antennas. Connect the antenna to the ATC ground test unit.

 (4)
 On the SWITCHING panel 8VU, make sure that the AIR DATA selector switch is at NORM.

 (5)
 On the center pedestal, on the ATC/TCAS control unit:

 -
set the ATC system 1(2) on.

 -
set the ALT RPTG/OFF/ON switch to OFF.

 -
set the AUTO/ON/STBY switch to ON.

 -make sure that the display does not show an emergency code: 7500, 7600 or 7700.

 (6)
 On the panel 13VU, on the CAPT and F/O EFIS control sections of the FCU, make sure that the baro displays show STD.

 (7)
 Do the operational test of ALT DYNAMIC SLEW TEST (Ref. TASK 34-13-00-710-004) to simulate an altitude of 23,458 ft. On the MCDU, enter 0/23 458 as SLEW LIMITS and push the line key adjacent to the UP (START SLEW) indication to start the test.

 Subtask 34-52-00-865-056
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU COM NAV/ATC/1 5SH1 G11 121VU COM NAV/ATC/2 5SH2 K07
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 4. Procedure
_________ Subtask 34-52-00-720-061
 A. Functional Test of the Altitude Reporting Function
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ATC/TCAS control unit:  On the ATC/TCAS control unit: - the ATC FAULT or FAIL indicator light is off. 
R R  - set the ALT RPTG ON/OFF switch to ON.  On the ATC ground test unit a display shows the standard altitude of approx. 23,458 ft or equivalent and the last code set.
 The difference between the altitude
 shown on CAPT and F/O PFDs and that shown on the ATC ground test unit must not be more than 125 ft.
 - set the AUTO/ON/STBY switch to STBY.  On the ATC/TCAS control unit:- the display stays on.
 5. Close-up________
 Subtask 34-52-00-860-059

 A. Put the aircraft back to its initial configuration.
 (1)
 Disconnect the ATC ground test unit.

 (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).

 (4)
 Make sure that the work area is clean and clear of tool(s) and other items.

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 Functional Test of the ATC/Mode S Transponder
 NOTE : You must do this test very quickly to prevent interference with air
____ traffic, specially if the aircraft is in the open air. If the test is long, you must tell the nearest airport of this test.
 NOTE : For best test results, buildings, vehicles and other aircraft must not
____
 be in the area of the main antenna lobe (approx 30 ft.).

 1. Reason for the Job
__________________
 Refer to the MPD TASK: 345200-03
 NOTE : There are alternative methods for this procedure. This task gives one
____ of the methods. For the other method with a different Ground Test Unit, refer to the other task in this page block.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform
 No specific circuit breaker(s) safety clip(s)
 No specific telescopic pole
 No specific T49 - ATC GROUND TEST UNIT (or equivalent)

 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 R 32-00-00-860-001 Flight Configuration Precautions with Electrical R Power R 32-00-00-860-002 Ground Configuration after Flight Configuration with R Electrical Power
　
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