R (3) Do the ADIRS start procedure (Ref. TASK 34-10-00-860-002).
R (4) Pressurize the aircraft hydraulic systems
 (Ref. TASK 29-10-00-863-001)
 (Ref. TASK 29-10-00-863-002)
 (Ref. TASK 29-10-00-863-003) (NOTE : You can use the electric pumps).
 Subtask 34-13-00-860-052
 B. Aircraft Maintenance Configuration
 (1)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (2)
 On the center pedestal, on one MCDU, get the SYSTEM REPORT/TEST/NAV page (Ref. TASK 31-32-00-860-010).

 (3)
 On the overhead panel, on the FLT CTL panels 23VU and 24VU:

 -make sure that the FAC, ELAC and SEC pushbutton switches are not pushed (in). The OFF legends are on.

 (4)
 On the center pedestal (panel 114VU), set the flap and slat control lever to the FULL position.

 (5)
 On the panel 50VU, release the ENG/FADEC GND PWR/1 and ENG/FADEC GND PWR/2 pushbutton switches. The ON legends come on.

 1EFF : ALL 1 34-13-00Page 532 1 1 May 01/05 1 1 1CES 1 Subtask 34-13-00-010-060

 C. Get Access
 (1)
 Put the access platform in position at the access door 822.

 (2)
 Open the access door 822

 (3)
 On the battery power center 105VU:

 -loosen the two screws and remove the protective cover
 Subtask 34-13-00-865-082
 D. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 49VU NAV PROBES/ADIRU3/PWR/SWTG 8FP F09 49VU NAV PROBES/ADIRU 1/AND AOA 1/26VAC 5FP1 F07 49VU NAV PROBES/ADIRU1/115VAC 4FP1 F06
 105VU ADIRS/ADIRU1/28VDC 6FP1 C02
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 121VU ADIRS/ADIRU/2PWR/SHED 10FP N11 121VU ADIRS/ADIRU/3PWR/SWTG 9FP N10 121VU ADIRS/ADIRU/2/26VAC AND AOA 5FP2 N09 121VU ADIRS/ADIRU/3/26VAC AND AOA 5FP3 N08 121VU ADIRS/ADIRU/2/115VAC 4FP2 N07 121VU ADIRS/ADIRU/3/115VAC 4FP3 N06 121VU ADIRS/ADIRU/2/28VDC 6FP2 N05 121VU ADIRS/ADIRU/3/28VDC 6FP3 N04
 **ON A/C ALL
 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35

R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 121VU ADIRS/ADIRU/2PWR/SHED 10FP N10 121VU ADIRS/ADIRU/3PWR/SWTG 9FP N09 121VU ADIRS/ADIRU/2/26VAC AND AOA 5FP2 N08
 1EFF : ALL 1 34-13-00Page 533 1 1 Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------121VU ADIRS/ADIRU/3/26VAC AND AOA 5FP3 N07 121VU ADIRS/ADIRU/2/115VAC 4FP2 N06 121VU ADIRS/ADIRU/3/115VAC 4FP3 N05 121VU ADIRS/ADIRU/2/28VDC 6FP2 N04 121VU ADIRS/ADIRU/3/28VDC 6FP3 N03

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 34-13-00-865-085
 E. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 105VU ELEC/CSM/G /EV AUTO/SPLY 7XE C01 121VU AUTO FLT/FAC2/28VDC 5CC2 M19
 **ON A/C ALL
 Subtask 34-13-00-860-090
 F. Aircraft Maintenance Configuration
 (1) On the center pedestal, on the ECAM control panel:
 -
push the CLR key until the MASTER CAUT and MASTER WARN lights go off on the panels 131VU and 130VU.

 -
push the CLR key until the memo section comes into view in the lower part of the upper ECAM display unit.

 1EFF : ALL 1 34-13-00Page 534 1 1 Aug 01/05 1 1 1CES 1

 4. Procedure
_________ Subtask 34-13-00-710-057
 A. Test of the VFE Overspeed Warning
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the overhead panel 20VU, on the ADIRS CDU:
 -push the ADR2 and ADR3
pushbutton switches.

2. On the MCDU:
-
push the line key adjacent to the NAV indication

-
push the line key adjacent to the ADR1 (ADR2) (ADR3) indication

 -
push the line key adjacent to the OUTPUT TESTS indication

-
push the line key adjacent to the SLEW TESTS indication

-
push the line key adjacent to the CAS DYNAMIC SLEW indication

- on the keyboard, enter these limits: 175/260

 -
push the line key adjacent to the CAS LIMITS (KT) indication
　
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