R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 34-13-00-865-071
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 121VU AUTO FLT/FAC2/28VDC 5CC2 M19
 **ON A/C ALL
 Subtask 34-13-00-860-065
 D. Aircraft Maintenance Configuration
 (1)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (2)
 Do the ADIRS start procedure (Ref. TASK 34-10-00-860-002).

 (3)
 When the circuit breakers 5CC1 and 5CC2 are open: - - the "AUTO FLT FAC 1+2 FAULT" message and the MASTER CAUT light

 come on
 - - you can hear the single chime.

 (4)
 Before the test, on the ECAM Control Panel, push the CLR key to clear the message.

 (5)
 On the glareshield 13VU, on the CAPT and F/O EFIS control sections of the FCU, set the mode selector switch to ROSE/NAV.

 (6)
 On the center pedestal, on one MCDU, get the SYSTEM REPORT/TEST/NAV menu page. (Ref. TASK 31-32-00-860-010).

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 4. Procedure_________
 Subtask 34-13-00-710-053
 A. Operational Test of the ALT Comparison Warning
 NOTE : This test is for the system 1. For the systems 2 and 3, use the____ indications between parentheses. 
R R R  NOTE : For system 3, on the center pedestal, set the SWITCHING/AIR DATA____ selector switch 15FP to CAPT (F/O) position; the CAPT (F/O) PFD shows the ADR3 indications.
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------

1. On the glareshield 13VU, on the CAPT and F/O EFIS control sections of the FCU:
 - pull the baro reference selector knob.  The baro display (above the baroreference selector knob) shows STD. The CAPT and F/O PFDs show the altitude related to the standard barometric
 pressure. Below this indication the PFDs show
 STD.
 2. On the MCDU:  On the MCDU:
 - push the line key adjacent to the ADR1 (ADR2) (ADR3) indication.  - the ADR1 (ADR2) (ADR3) page comesinto view.
R
 - push the line key adjacent to the OUTPUT TESTS indication.  - the ADR1 (ADR2) (ADR3) OUTPUT TESTSpage comes into view.
 - push the line key adjacent to the SLEW TESTS indication.  - the ADR1 (ADR2) (ADR3) SLEW TESTSpage comes into view.
 - push the line key adjacent to the ALT DYNAMIC SLEW indication. - the ADR1 (ADR2) (ADR3) ALT DYNAMICSLEW page comes into view.
 - on the keyboard, enter:  - the display shows:

 -------------------------------------------------------------------------------ACTION RESULT
 -------------------------------------------------------------------------------*the airfield altitude value / *the airfield altitude value / (airfield altitude value plus (airfield altitude value plus 1500) 1500) *(Example: for an airfield altitude value of 1800ft enter: 1800 / 3300). and push the line key adjacent to the ALT LIMITS (FT) indication.
 - on the keyboard, enter 1000 and - the display shows 1000.
 push the line key adjacent to
 the ALT SLEW RATE (FT/MIN)
 indication.

 -push the line key adjacent to The test starts: R the UP (START SLEW) indication.
 -the ADR1 ALT DYNAMIC SLEW TEST page with SLEWING IN PROGRESS 90 S information comes into view.
 -On the CAPT (F/O) PFD the altitude increase.
 When the difference of altitude between the CAPT PFD and the F/O PFD is 650
 ft approximately:

 -
the vertical CHECK ALT indication comes into view on the two PFDs.

 -
the upper ECAM DU shows this warning:

 NAV ALTI DISCREPANCY - on the glareshield panels 130VU and 131VU, the MASTER CAUT light comes on.
 -you can hear the single chime.
 On the MCDU:

 -at the end of the test, the END OF SLEWING indication comes into view.
 -push the line key adjacent to
 the RETURN indication until the
 CFDS menu page comes into view.

 NOTE : After the ADR3 test, set
____
 the AIR DATA selector
 switch 15FP to NORMAL.

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