Operational Check of Overspeed Warnings VFE/VLE Using CFDS

TASK 34-13-00-710-007-A
Operational Check of Overspeed Warnings VFE/VLE Using CFDS

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:

THE FLIGHT CONTROLS
THE FLIGHT CONTROL SURFACES
THE LANDING GEAR AND THE RELATED DOORS
COMPONENTS THAT MOVE.

MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.

NOTE: This test is for system 1. For systems 2 and 3, use the indications between parentheses.

ZONE: 210

1. Reason for the Job
Refer to the MPD TASK: 341300-03
OPERATIONAL CHECK OF OVERSPEED WARNINGS VFE/VLE USING CFDS.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	SAFETY BARRIER(S)
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	AR	WARNING NOTICE(S)

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
210	CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD

C. Referenced Information

REFERENCE	DESIGNATION
TASK 24-41-00-861-002-A	Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01	Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02	Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A	De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01	De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02	De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 29-10-00-863-001-A	Pressurize the Green Hydraulic System with a Hydraulic Ground Power-Cart
TASK 29-10-00-863-002-A	Pressurize the Yellow Hydraulic System with a Hydraulic Ground Power-Cart
TASK 29-10-00-863-003-A	Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart
TASK 29-10-00-864-001-A	Depressurize the Green Hydraulic System
TASK 29-10-00-864-002-A	Depressurize the Yellow Hydraulic System
TASK 29-10-00-864-003-A	Depressurize the Blue Hydraulic System
TASK 29-23-00-863-001-A	Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
TASK 29-23-00-864-001-A	Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU
TASK 31-32-00-860-010-A	Procedure to Get Access to the SYSTEM REPORT/TEST NAV Page
TASK 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure
TASK 32-22-00-010-001-A	Nose Gear Doors - Ground Doors Opening
TASK 32-22-00-410-001-A	Nose Gear Doors - Ground Doors Closing
TASK 34-10-00-860-002-A	ADIRS Start Procedure
TASK 34-10-00-860-005-A	ADIRS Stop Procedure

3. Job Set-up
Subtask 34-13-00-941-050-A

A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Put the WARNING NOTICE(S) in position to tell persons that the slat system is in operation.

Subtask 34-13-00-860-050-A

B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the nose landing-gear doors are closed
(Ref. AMM TASK 32-22-00-410-001).
(3) Do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002).
(4) Pressurize the aircraft hydraulic systems
(Ref. AMM TASK 29-10-00-863-001)
(Ref. AMM TASK 29-10-00-863-002)
(Ref. AMM TASK 29-10-00-863-003)
(Ref. AMM TASK 29-23-00-863-001).

Subtask 34-13-00-860-052-A

C. Aircraft Maintenance Configuration
(1) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
(2) On the center pedestal, on one MCDU, get the SYSTEM REPORT/TEST/NAV page
(Ref. AMM 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.

Subtask 34-13-00-865-082-A

D. Make sure that this(these) circuit breaker(s) is(are) closed:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	NAV PROBES/ADIRU3/PWR/SWTG	8FP	F09
** ON A/C ALL
49VU	L/G/LGCIU/SYS1/NORM	1GA	C09
49VU	NAV PROBES/ADIRU 1/AND AOA 1/26VAC	5FP1	F07
49VU	NAV PROBES/ADIRU1/115VAC	4FP1	F06
** ON A/C NOT FOR ALL
49VU	NAV PROBES/ADIRU3/PWR/SWTG	8FP	F08
** ON A/C ALL
105VU	ADIRS/ADIRU1/28VDC	6FP1	C02
** ON A/C NOT FOR ALL
121VU	ADIRS/ADIRU/2PWR/SHED	10FP	N10
** ON A/C ALL
121VU	ADIRS/ADIRU/3PWR/SWTG	9FP	N09
121VU	ADIRS/ADIRU/2/26VAC AND AOA	5FP2	N08
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
121VU	HYDRAULIC/LGCIU/SYS2	2GA	Q35
** ON A/C NOT FOR ALL
121VU	ADIRS/2PWR/SHED &/AOA2 MON	10FP	N10

Subtask 34-13-00-875-062-A

WARNING: OPEN CIRCUIT BREAKER 7XE. THIS WILL PREVENT A POSSIBLE DEPLOYMENT OF THE RAT IF THE MAIN AC BUSBARS 1XP AND 2XP BECOME ISOLATED.

E. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	AUTO FLT/FAC1/28VDC	5CC1	B04
** ON A/C NOT FOR ALL
49VU	AUTO FLT/FAC1/28VDC	5CC1	H10
** ON A/C ALL
105VU	ELEC/CSM/G /EV AUTO/SPLY	7XE	C01
121VU	AUTO FLT/FAC2/28VDC	5CC2	M19

Subtask 34-13-00-860-090-A

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.

4. Procedure
Subtask 34-13-00-710-057-C ** ON A/C NOT FOR ALL

A. Test of the VFE Overspeed Warning

ACTION	RESULT
1.On overhead panel 20VU, on the ADIRS CDU:	On the ADIRS CDU, on the ADR2 and ADR3 pushbutton switches:
Push the ADR2 and ADR3 pushbutton switches.	The OFF legends come on.
2.On the MCDU:	On the MCDU:
Push the line key adjacent to the NAV indication.	The SYSTEM REPORT/TEST page which contains the three ADR comes into view.
Push the line key adjacent to the ADR1 (ADR2) (ADR3) indication.	The ADR1 (ADR2) (ADR3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	The ADR1 (ADR2) (ADR3) OUTPUT TESTS page comes into view.
Push the line key adjacent to the SLEW TESTS indication.	The ADR1 (ADR2) (ADR3) SLEW TESTS page comes into view.
Push the line key adjacent to the CAS DYNAMIC SLEW indication.	The ADR1 (ADR2) (ADR3) CAS DYNAMIC SLEW page comes into view.
On the keyboard, enter these limits: 175/260
Push the line key adjacent to the CAS LIMITS (KT) indication.	The slew limits set come into view below the related indication.
On the keyboard, enter this slew rate: 020
Push the line key adjacent to the CAS SLEW RATE (KT/MIN) indication.	The slew rate set comes into view below the related indication.
Push the line key adjacent to the UP-START SLEW indication.	On the CAPT (F/O) PFD, the speed scale moves from 175 kts to 260 kts as specified in the table that follows. On the upper ECAM display unit, make sure that all the indications given in the table that follows come into view. On F/O glareshield-panel 130VU and CAPT glareshield-panel 131VU, the MASTER WARN lights flash when the speeds set come into view. The continuous chime operates again and again.
Set the flap and slat control lever to a lower position.	On F/O glareshield-panel 130VU and CAPT glareshield-panel 131VU, the MASTER WARN lights go off.

Subtask 34-13-00-710-057-E ** ON A/C NOT FOR ALL

A. Test of the VFE Overspeed Warning

ACTION	RESULT
1.On ADIRS MSU panel 41VU:
For ADR1 and ADR2, make sure that the AIR DATA selector switch is set to NORM. For ADR3, make sure that the AIR DATA selector switch is set to CAPT/3 or F/O/3 to get the reading on the CAPT or F/O PFD.
Push ADR2 and ADR3 (ADR1 and ADR3) (ADR1 and ADR2) pushbutton switches.	On ADIRS MSU panel 41VU, the OFF legends of ADR2 and ADR3 (ADR1 and ADR3) (ADR1 and ADR2) pushbutton switches come on.
2.On the MCDU:	On the MCDU:
Push the line key adjacent to the NAV indication.	The SYSTEM REPORT/TEST page that contains the three ADRs comes into view.
Push the line key adjacent to ADR1 (ADR2) (ADR3) indication.	ADR1 (ADR2) (ADR3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	ADR1 (ADR2) (ADR3) OUTPUT TESTS page comes into view.
Push the line key adjacent to the SLEW TESTS indication.	ADR1 (ADR2) (ADR3) SLEW TESTS page comes into view.
Push the line key adjacent to the CAS DYNAMIC SLEW indication.	ADR1 (ADR2) (ADR3) CAS DYNAMIC SLEW page comes into view.
On the keyboard, enter these limits: 175/260
Push the line key adjacent to the CAS LIMITS (KT) indication.	The set slew limits come into view below the related indication.
On the keyboard, enter this slew rate: 020
Push the line key adjacent to the CAS SLEW RATE (KT/MIN) indication.	The set slew rate comes into view below the related indication.
Push the line key adjacent to the UP-START SLEW indication.	The SLEWING IN PROGRESS 255S indication comes into view. During the test: On the CAPT (F/O) PFD, the speed scale moves from 175 kts to 260 kts as shown in the table that follows. On the upper ECAM display unit, make sure that all the indications given in the table that follows come into view. On F/O glareshield-panel 130VU and CAPT glareshield-panel 131VU, the MASTER WARN lights flash when the set speeds come into view. The continuous alarm operates again and again.
Set the flap and slat control lever to a lower position.	On F/O glareshield-panel 130VU and CAPT glareshield-panel 131VU, the MASTER WARN lights go off.

Subtask 34-13-00-710-057-F ** ON A/C NOT FOR ALL

A. Test of the VFE Overspeed Warning

ACTION	RESULT
1.On ADIRS MSU panel 41VU:
For ADR 1 and ADR 2, make sure that the AIR DATA selector switch is set to NORM. For ADR 3, make sure that the AIR DATA selector switch is set to CAPT/3 or F/O/3 to get the indication on the CAPT or F/O PFD.
Push the ADR 2 and ADR 3 (ADR 1 and ADR 3) (ADR 1 and ADR 2) pushbutton switches.	On ADIRS MSU panel 41VU, the OFF legends of the ADR 2 and ADR 3 (ADR 1 and ADR 3) (ADR 1 and ADR 2) pushbutton switches come on.
2.On the MCDU:	On the MCDU:
Push the line key adjacent to the NAV indication.	The SYSTEM REPORT/TEST page that contains the three ADRs comes into view.
Push the line key adjacent to the ADR 1 (ADR 2) (ADR 3) indication.	The ADR 1 (ADR 2) (ADR 3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	The ADR 1 (ADR 2) (ADR 3) OUTPUT TESTS page comes into view.
Push the line key adjacent to the SLEW TESTS indication.	The ADR 1 (ADR 2) (ADR 3) SLEW TESTS page comes into view.
Push the line key adjacent to the CAS DYNAMIC SLEW indication.	The ADR 1 (ADR 2) (ADR 3) CAS DYNAMIC SLEW page comes into view.
On the keyboard, enter these limits: 175/260.
Push the line key adjacent to the CAS LIMITS (KT) indication.	The set slew limits come into view below the related indication.
On the keyboard, enter this slew rate: 020.
Push the line key adjacent to the CAS SLEW RATE (KT/MIN) indication.	The set slew rate comes into view below the related indication.
Push the line key adjacent to the UP-START SLEW indication.	On the CAPT (F/O) PFD, the speed scale goes across 80 kts.
Push the RCL button on the ECAM control panel.	Alerts can come into view. If this occurs, ignore these alerts. On the CAPT (F/O) PFD, the speed scale moves from 175 kts to 260 kts as shown in the table that follows. On the upper ECAM DU, make sure that all the indications given in the table that follows come into view. On F/O glareshield-panel 130VU and CAPT glareshield-panel 131VU, the MASTER WARN lights flash when the set speeds come into view. The continuous alarm operates again and again.
Set the flap and slat control lever to a lower position.	On F/O glareshield-panel 130VU and CAPT glareshield-panel 131VU, the MASTER WARN lights go off.

Subtask 34-13-00-710-061-A ** ON A/C NOT FOR ALL

B. Speed values
Get the correct speed values before you move the flaps/slats control lever.

SPEED IS MORE THAN	SLATS AND FLAPS Position of CTL LEVER	SLATS AND FLAPS Indication on the upper ECAM DU	INDICATION ON THE UPPER ECAM DISPLAY UNIT
181 Kts	FULL	FULL	OVERSPEED - VFE 177
181 Kts	3	3	The indication goes out of view.
189 Kts	3	3	OVERSPEED - VFE 185
189 Kts	2	2	The indication goes out of view.
204 Kts	2	2	OVERSPEED - VFE 200
204 Kts	1	1+F	The indication goes out of view.
219 Kts	1	1+F	OVERSPEED - VFE 215
234 Kts (or equal)	1	1+F	OVERSPEED - VFE 215
234 Kts (or equal)	0	0	When OVERSPEED - VFE 215: indication goes out of view: OVERSPEED - VFE 230 This indication comes into view when you are in the intermediate position.

Subtask 34-13-00-710-061-C ** ON A/C NOT FOR ALL

B. Speed values

NOTE: Make sure that the speed values are reached before you move the flaps/slats control lever.

-------------------------------------------------------------------------------

! ! SLATS AND FLAPS ! !

! !---------------------------------! !

! ! ! ! !

! SPEED ! Position ! Indication ! INDICATION !

! IS MORE ! of CTL LEVER ! on the upper ! ON THE UPPER ECAM !

! THAN ! ! ECAM DU ! DISPLAY UNIT !

! ! ! ! !

!---------!----------------!----------------!---------------------------------!

! 194 Kts ! FULL ! FULL ! OVERSPEED !

! ! ! ! - VFE 190 !

! !----------------!----------------!---------------------------------!

! ! 3 ! 3 ! The indication goes out of view !

!---------!----------------!----------------!---------------------------------!

!199 Kts ! 3 ! 3 ! OVERSPEED !

! ! ! ! - VFE 195 !

! !----------------!----------------!---------------------------------!

! ! 2 ! 2 ! The indication goes out of view !

!---------!----------------!----------------!---------------------------------!

! 219 Kts ! 2 ! 2 ! OVERSPEED !

! ! ! ! - VFE 215 !

! !----------------!----------------!---------------------------------!

! ! 1 ! 1+F ! The indication goes out of view !

! ! ! ! then comes into view !

!---------!----------------!----------------!---------------------------------!

! 234 Kts ! 1 ! 1+F ! OVERSPEED !

! ! ! ! - VFE 215 !

! !----------------!----------------!---------------------------------!

! ! ! ! OVERSPEED !

! ! 0 ! 0 ! -VFE 230 !

! ! ! ! The indication !

! ! ! ! comes into view for !

! ! ! ! approximately (1 second) !

! ! ! ! then goes out of view. !

!-------------------------------------------!---------------------------------!

! When the OVERSPEED VFE 230 goes out of ! !

! view or if the OVERSPEED VFE 215 remained ! !

! displayed, move the control lever to the ! !

! position 1 before you reach CAS 254 Kts ! !

!-------------------------------------------!---------------------------------!

! 254 Kts ! 1 ! 1+F ! OVERSPEED !

! ! ! ! -VFE 215 !

! !----------------!----------------!---------------------------------!

! ! ! ! OVERSPEED !

! ! ! ! -VFE 230 !

! ! 0 ! 0 ! The indication comes into view !

! ! ! ! for some seconds then goes out !

! ! ! ! of view. !

-------------------------------------------------------------------------------

Subtask 34-13-00-710-061-D ** ON A/C NOT FOR ALL

B. Speed values

NOTE: Make sure that speed values are reached before you move the flaps/slats control lever.

-------------------------------------------------------------------------------

! ! SLATS AND FLAPS ! !

! !---------------------------------! !

! ! ! ! !

! SPEED ! Position ! Indication ! INDICATION !

! IS MORE ! of CTL LEVER ! on the upper ! ON THE UPPER ECAM !

! THAN ! ! ECAM DU ! DISPLAY UNIT !

! ! ! ! !

!---------!----------------!----------------!---------------------------------!

! 194 Kts ! FULL ! FULL ! OVERSPEED !

! ! ! ! - VFE 190 !

! !----------------!----------------!---------------------------------!

! ! 3 ! 3 ! The indication goes out of view !

!---------!----------------!----------------!---------------------------------!

! 199 Kts ! 3 ! 3 ! OVERSPEED !

! ! ! ! - VFE 195 !

! !----------------!----------------!---------------------------------!

! ! 2 ! 2 ! The indication goes out of view !

!---------!----------------!----------------!---------------------------------!

! 219 Kts ! 2 ! 2 ! OVERSPEED !

! ! ! ! - VFE 215 !

! !----------------!----------------!---------------------------------!

! ! 1 ! 1+F ! The indication goes out of !

! ! ! ! view (215 be shown while some !

! ! ! ! seconds before the following !

! ! ! ! indication). !

!---------!----------------!----------------!---------------------------------!

! 229 Kts ! 1 ! 1+F ! The indication !

! ! ! ! - VFE 225 !

! ! ! ! comes into view !

! ! ! ! !

!---------!----------------!----------------!---------------------------------!

! 239 Kts ! 1 ! 1+F ! - VFE 225 !

! !----------------!----------------!---------------------------------!

! ! ! ! OVERSPEED !

! ! 0 ! 0 ! -VFE 235 !

! ! ! ! The indication !

! ! ! ! comes into view (for !

! ! ! ! approximately 1 second) !

! ! ! ! then goes out of view. !

!-------------------------------------------!---------------------------------!

! When the OVERSPEED VFE 235 goes out of ! !

! view or if the OVERSPEED VFE 225 remained ! !

! displayed, move the control lever to the ! !

! position 1 before you reach CAS 254 Kts. ! !

!-------------------------------------------!---------------------------------!

! 254 Kts ! 1 ! 1+F ! OVERSPEED !

! ! ! ! -VFE 225 !

! !----------------!----------------!---------------------------------!

! ! ! ! OVERSPEED !

! ! ! ! -VFE 235 !

! ! 0 ! 0 ! The indication comes into view !

! ! ! ! for some seconds then goes out !

! ! ! ! of view. !

-------------------------------------------------------------------------------

Subtask 34-13-00-710-061-I ** ON A/C NOT FOR ALL

B. Speed values

NOTE: You must get the correct speed values before you move the flaps/slats control lever.

SPEED IS MORE THAN	SLATS AND FLAPS Position of the CTL LEVER	SLATS AND FLAPS Indication on the upper ECAM DU	INDICATION ON THE UPPER ECAM DU
194 Kts	FULL	FULL	OVERSPEED - VFE 186
194 Kts	3	3	The indication goes out of view.
199 Kts	3	3	OVERSPEED - VFE 195
199 Kts	2	2	The indication goes out of view.
229 Kts	2	2	OVERSPEED - VFE 225
229 Kts	1	1+F	The indication goes out of view then comes into view.
242 Kts	1	1+F	OVERSPEED - VFE 225
242 Kts	0	0	OVERSPEED - VFE 238 The indication comes into view for approximately 1 second then goes out of view. NOTE: When the OVERSPEED VFE 238 indication goes out of view or if the OVERSPEED VFE 225 stayed in view, move the control lever to position 1 before you get CAS 254 Kts.
254 Kts	1	1+F	OVERSPEED - VFE 225
254 Kts	0	0	OVERSPEED - VFE 238 The indication comes into view for some seconds then goes out of view.

Subtask 34-13-00-860-053-A

C. Depressurize the aircraft hydraulic systems (Ref. AMM TASK 29-10-00-864-001) (Ref. AMM TASK 29-10-00-864-002) (Ref. AMM TASK 29-10-00-864-003) (Ref. AMM TASK 29-23-00-864-001).

Subtask 34-13-00-710-059-H ** ON A/C NOT FOR ALL

D. Test of the VLE Overspeed Warning

ACTION	RESULT
1.Open the nose landing gear doors (Ref. AMM TASK 32-22-00-010-001). 2.On overhead panel 20VU, on the ADIRS CDU:
Push the ADR2 and ADR3 pushbutton switches.	On the ADIRS CDU, the OFF legend of the ADR2 and ADR3 pushbutton switches comes on.
3.On the MCDU:	On the MCDU:
Push the line key adjacent to the ADR1 (ADR2) (ADR3) indication.	The ADR1 (ADR2) (ADR3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	The ADR1 (ADR2) (ADR3) OUTPUT TESTS page comes into view.
Push the line key adjacent to the SLEW TESTS indication.	The ADR1 (ADR2) (ADR3) SLEW TESTS page comes into view.
Push the line key adjacent to the CAS DYNAMIC SLEW indication.	The ADR1 (ADR2) (ADR3) CAS DYNAMIC SLEW page comes into view.
On the keyboard, enter these limits: 275/290	The slew limits come into view on the bottom line (scratch pad) of the MCDU.
Push the line key adjacent to the CAS LIMITS (KT) indication.	The slew limits set come into view below the related indication.
On the keyboard, enter this slew rate: 025	The slew rate comes into view on the bottom line (scratch pad) of the MCDU.
Push the line key adjacent to the CAS SLEW RATE (KT/MIN) indication.	The slew rate set comes into view below the related indication.
Push the line key adjacent to the UP-START SLEW indication.	On the CAPT (F/O) PFD, the speed scale moves from 275 kts to 290 kts. On the upper ECAM display unit, when the CAS reaches 284 kts, make sure that this indication comes into view: OVERSPEED VLE...............280/.67 On F/O glareshield-panel 130VU and CAPT glareshield-panel 131VU, the MASTER WARN lights flash. The continuous chime operates again and again.
Push the line key adjacent to the RETURN/STOP indication.	On the CAPT (F/O) PFD, the speed scale moves down. On F/O glareshield-panel 130VU and CAPT glareshield-panel 131VU, the MASTER WARN lights do not flash. The continuous chime that operates again and again stops.
4.On the ADIRS CDU:	On the ADIRS CDU:
Push the ADR1 and ADR2 pushbutton switches.	The OFF legend of the ADR1 pushbutton switch comes on The OFF legend of the ADR2 pushbutton switch goes off.
5.Do the ADR2 test as specified in step 3.	Same results on the F/O side.
6.On the ADIRS CDU:	On the ADIRS CDU:
Push the ADR2 and ADR3 pushbutton switches.	The OFF legend of the ADR2 pushbutton switch comes on The OFF legend of the ADR3 pushbutton switch goes off.
7.On SWITCHING panel 8VU: Set the AIR DATA selector switch to CAPT/3.	On the CAPT PFD, the speed and altitude indications from ADR3 come into view.
8.Do the ADR3 test as specified in step 3.	Same results on the CAPT side.
9.On the ADIRS CDU:
Push the ADR1 and ADR2 pushbutton switches again.	On the ADIRS CDU, the OFF legend of the ADR1 and ADR2 pushbutton switches goes off.

Subtask 34-13-00-710-059-K ** ON A/C NOT FOR ALL

D. Test of the VLE Overspeed Warning

ACTION	RESULT
1.Open the nose landing-gear doors (Ref. AMM TASK 32-22-00-010-001).
2.On ADIRS MSU panel 41VU: Push ADR2 and ADR3 pushbutton switches.	On ADIRS MSU panel 41VU, the OFF legend of the ADR2 and ADR3 pushbutton switches comes on.
3.On the MCDU:	On the MCDU:
Push the line key adjacent to ADR1 (ADR2) (ADR3) indication.	ADR1 (ADR2) (ADR3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	ADR1 (ADR2) (ADR3) OUTPUT TESTS page comes into view.
Push the line key adjacent to the SLEW TESTS indication.	ADR1 (ADR2) (ADR3) SLEW TESTS page comes into view.
Push the line key adjacent to the CAS DYNAMIC SLEW indication.	ADR1 (ADR2) (ADR3) CAS DYNAMIC SLEW page comes into view.
On the keyboard, enter these limits: 275/290	The slew limits come into view on the bottom line (scratch pad) of the MCDU.
Push the line key adjacent to the CAS LIMITS (KT) indication.	The slew limits set come into view below the related indication.
On the keyboard, enter this slew rate: 025	The slew rate comes into view on the bottom line (scratch pad) of the MCDU.
Push the line key adjacent to the CAS SLEW RATE (KT/MIN) indication.	The slew rate set comes into view below the related indication.
Push the line key adjacent to the UP-START SLEW indication.	On the CAPT (F/O) PFD, the speed scale moves from 275 kts to 290 kts. On the upper ECAM display unit, when the CAS reaches 284 kts, make sure that this indication comes into view: OVERSPEED VLE...............280/.67 On the F/O and CAPT glareshield panels 130VU and 131VU, the MASTER WARN lights flash. The continuous repetitive chime sounds.
Push the line key adjacent to the RETURN/STOP indication.	On the CAPT (F/O) PFD, the speed scale moves down. On F/O and CAPT glareshield panels 130VU and 131VU, the MASTER WARN lights do not flash. The continuous repetitive chime stops.
4.On ADIRS MSU panel 41VU:	On ADIRS MSU panel 41VU:
Push ADR1 and ADR2 pushbutton switches.	The OFF legend of ADR1 pushbutton switch comes on The OFF legend of ADR2 pushbutton switch goes off.
5.Do ADR2 test as specified in step 3.	Same results on the F/O side.
6.On ADIRS MSU panel 41VU:	On ADIRS MSU panel 41VU:
Push ADR2 and ADR3 pushbutton switches.	The OFF legend of ADR2 pushbutton switch comes on The OFF legend of ADR3 pushbutton switch goes off.
7.On SWITCHING panel 8VU: Set the AIR DATA selector switch to CAPT/3.	On the CAPT PFD, the speed and altitude indications from ADR3 come into view.
8.Do ADR3 test as specified in step 3.	Same results on the CAPT side.
9.On ADIRS MSU panel 41VU:
Push ADR1 and ADR2 pushbutton switches again.	On ADIRS MSU panel 41VU, the OFF legend of ADR1 and ADR2 pushbutton switches goes off.

Subtask 34-13-00-710-059-L ** ON A/C NOT FOR ALL

D. Test of the VLE Overspeed Warning

ACTION	RESULT
1.Open the nose landing-gear doors (Ref. AMM TASK 32-22-00-010-001).
2.On ADIRS MSU panel 41VU: Push the ADR 2 and ADR 3 pushbutton switches.	On ADIRS MSU panel 41VU, the OFF legends of the ADR 2 and ADR 3 pushbutton switches come on.
3.On the MCDU:	On the MCDU:
Push the line key adjacent to the ADR 1 (ADR 2) (ADR 3) indication.	The ADR 1 (ADR 2) (ADR 3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	The ADR 1 (ADR 2) (ADR 3) OUTPUT TESTS page comes into view.
Push the line key adjacent to the SLEW TESTS indication.	The ADR 1 (ADR 2) (ADR 3) SLEW TESTS page comes into view.
Push the line key adjacent to the CAS DYNAMIC SLEW indication.	The ADR 1 (ADR 2) (ADR 3) CAS DYNAMIC SLEW page comes into view.
On the keyboard, enter these limits: 275/290.	The slew limits come into view on the bottom line (scratch pad) of the MCDU.
Push the line key adjacent to the CAS LIMITS (KT) indication.	The slew limits set come into view below the related indication.
On the keyboard, enter this slew rate: 025.	The slew rate comes into view on the bottom line (scratch pad) of the MCDU.
Push the line key adjacent to the CAS SLEW RATE (KT/MIN) indication.	The slew rate set comes into view below the related indication.
Push the line key adjacent to the UP-START SLEW indication.	On the CAPT (F/O) PFD, when the speed scale goes across 80 Kts, push the RCL button on the ECAM control panel. When you do this, alerts can come into view. If this occurs, ignore these alerts. On the CAPT (F/O) PFD, the speed scale moves from 275 Kts to 290 Kts. On the upper ECAM DU, when the CAS is at 284 Kts, make sure that this indication comes into view: OVERSPEED VLE...............280/.67 On F/O and CAPT glareshield panels 130VU and 131VU, the MASTER WARN lights flash. The continuous alarm operates again and again.
Push the line key adjacent to the RETURN/STOP indication.	On the CAPT (F/O) PFD, the speed scale moves down. On F/O and CAPT glareshield panels 130VU and 131VU, the MASTER WARN lights do not flash. The continuous alarm stops.
4.On ADIRS MSU panel 41VU:	On ADIRS MSU panel 41VU:
Push ADR 1 and ADR 2 pushbutton switches.	The OFF legend of ADR 1 pushbutton switch comes on. The OFF legend of ADR 2 pushbutton switch goes off.
5.Do the test for ADR 2 as given in step 3.	Same results on the F/O side.
6.On ADIRS MSU panel 41VU:	On ADIRS MSU panel 41VU:
Push the ADR 2 and ADR 3 pushbutton switches.	The OFF legend of the ADR 2 pushbutton switch comes on. The OFF legend of the ADR 3 pushbutton switch goes off.
7.On SWITCHING panel 8VU: Set the AIR DATA selector switch to CAPT/3.	On the CAPT PFD, the speed and altitude indications of ADR 3 come into view.
8.Do the test for ADR 3 as given in step 3.	Same results on the CAPT side.
9.On ADIRS MSU panel 41VU:
Push the ADR 1 and ADR 2 pushbutton switches again.	On ADIRS MSU panel 41VU, the OFF legends of the ADR 1 and ADR 2 pushbutton switches go off.

5. Close-up
Subtask 34-13-00-875-065-A

A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	AUTO FLT/FAC1/28VDC	5CC1	B04
** ON A/C NOT FOR ALL
49VU	AUTO FLT/FAC1/28VDC	5CC1	H10
** ON A/C ALL
105VU	ELEC/CSM/G /EV AUTO/SPLY	7XE	C01
121VU	AUTO FLT/FAC2/28VDC	5CC2	M19

Subtask 34-13-00-860-051-A

B. Put the aircraft back to its initial configuration.
(1) On panel 50VU, push the ENG/FADEC GND PWR/1 and ENG/FADEC GND PWR/2 pushbutton switches. The ON legends go off.
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) Do the ADIRS stop procedure
(Ref. AMM TASK 34-10-00-860-005).
(4) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(5) Close the nose landing-gear doors
(Ref. AMM TASK 32-22-00-410-001).
(6) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

Subtask 34-13-00-942-050-A

C. Removal of Equipment
(1) Remove the SAFETY BARRIERS.
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

[Rev.10 from 2021] 2026.04.01 07:04:47 UTC