Test of the Angle of Attack (AOA) Warning

TASK 34-10-00-710-007-A
Test of the Angle of Attack (AOA) Warning

ZONE: 210

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 1M(3 FT)
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
210	CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD
822

C. Referenced Information

REFERENCE	DESIGNATION
TASK 10-11-00-555-013-A	Installation of the Aircraft Protection Equipment
TASK 10-11-00-555-014-A	Removal of the Aircraft Protection Equipment
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 27-50-00-866-009-A	Retraction of the Flaps on the Ground
TASK 27-50-00-866-009-A-01	Retraction of the Flaps/Slats on the Ground
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

3. Job Set-up

CAUTION: MAKE SURE THAT THE AOA SENSOR CAN MOVE FREELY DURING THE TEST (IT WILL MOVE FROM THE STANDBY POSITION TO THE TEST POSITION).

Subtask 34-10-00-860-065-A ** ON A/C NOT FOR ALL

A. Aircraft Maintenance Configuration
(1) Remove the AOA sensor protections, if installed (Ref. AMM TASK 10-11-00-555-014).
(2) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(3) On the overhead panel:

On flight control panels 23VU and 24VU, make sure that the FAC, ELAC and SEC pushbutton switches are not pushed. The OFF legends are on.
On panel 20VU, on the ADIRS CDU, make sure that the three OFF/NAV/ATT selector switches are set to OFF.

(4) Fully retract the flaps (Ref. AMM TASK 27-50-00-866-009).

NOTE: This test is for the system 1. For the other system(s), use the indications between the parentheses.

(5) Do the EIS start procedure (PFD only) (Ref. AMM TASK 31-60-00-860-001).
(6) On the Multipurpose Control and Display Unit (MCDU), get the SYSTEM REPORT/TEST/NAV page
(Ref. AMM TASK 31-32-00-860-010).

Subtask 34-10-00-860-065-C ** ON A/C NOT FOR ALL

On flight control panels 23VU and 24VU, make sure that the FAC, ELAC and SEC pushbutton switches are not pushed. The OFF legends are on.
On ADIRS MSU panel 41VU, make sure that the three OFF/NAV/ATT selector switches are set to OFF.

(4) Fully retract the flaps (Ref. AMM TASK 27-50-00-866-009).

NOTE: This test is for the system 1. For the other system(s), use the indications between the parentheses.

(5) Do the EIS start procedure (PFD only) (Ref. AMM TASK 31-60-00-860-001).
(6) On the MCDU, get the SYSTEM REPORT/TEST/NAV page
(Ref. AMM TASK 31-32-00-860-010).

Subtask 34-10-00-010-064-A

B. Get Access
(1) Put the ACCESS PLATFORM 1M(3 FT) in position below access door 822.
(2) Open access door 822.
(3) On battery power-center 105VU:

Loosen the two screws and remove the protective cover.

Subtask 34-10-00-865-064-A

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

PANEL	DESIGNATION	FIN	LOCATION
** 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
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	EIS/HORN/SPLY	2WC	P09
121VU	HYDRAULIC/LGCIU/SYS2	2GA	Q35
121VU	HYDRAULIC/LGCIU/SYS1/GRND SPLY	52GA	Q34
** ON A/C NOT FOR ALL
121VU	ADIRS/2PWR/SHED &/AOA2 MON	10FP	N10

Subtask 34-10-00-865-076-A

D. 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
121VU	AUTO FLT/FAC2/28VDC	5CC2	M19

4. Procedure
Subtask 34-10-00-710-062-J ** ON A/C NOT FOR ALL

A. Test of the Angle of Attack Warning

ACTION	RESULT
1.On the ADIRS CDU: Set the three OFF/NAV/ATT selector switches to NAV.	On the CAPT and F/O PFDs: Make sure that the CAS, ALT, V/S data are shown. Make sure that the attitude data is shown for 40 seconds after the start up.
2.On MCDU1 or MCDU2, on the NAV page:	On MCDU1 or MCDU2:
Push the line key adjacent to the ADR1 (ADR2) (ADR3) indication.	The ADIRS ADR1 (ADR2) (ADR3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	The OUTPUT TESTS page comes into view.
Push the line key adjacent to the AOA SENSOR TEST indication.	The AOA SENSOR TEST page comes into view with these indications: * AOA SENSOR COMMANDED TO FIXED POSITION * MAKE SURE THAT THE AURAL STALL WARNING IS GENERATED. On the left (right) side of the fuselage, in zone 231 (232) (127), the angle of attack sensor 3FP1 (3FP2) (3FP3) moves to the test position. On panels 130VU and 131VU, the MASTER WARN lights flash. You can hear the cricket aural warning and the STALL voice.
Push the line key adjacent to the YES indication.	On the MCDU: The TEST OK indication comes into view.
Push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.	The test procedure stops. The MASTER WARN lights go off. The cricket aural warning and the STALL voice stop. On the MCDU: The CFDS menu page comes into view.

Subtask 34-10-00-710-062-O ** ON A/C NOT FOR ALL

A. Test of the Angle of Attack Warning

ACTION	RESULT
1.On ADIRS MSU panel 41VU: Set the three OFF/NAV/ATT selector switches to NAV.	On the CAPT and F/O PFDs: Make sure that the CAS, ALT, V/S data are shown. Make sure that the attitude data is shown for 40 seconds after the start up.
2.On MCDU1 or MCDU2, on the NAV page:	On MCDU1 or MCDU2:
Push the line key adjacent to the ADR1 (ADR2) (ADR3) indication.	The ADIRS ADR1 (ADR2) (ADR3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	The OUTPUT TESTS page comes into view.
Push the line key adjacent to the AOA SENSOR TEST indication.	The AOA SENSOR TEST page comes into view with these indications: * AOA SENSOR COMMANDED TO FIXED POSITION * MAKE SURE THAT THE AURAL STALL WARNING IS GENERATED. On the left (right) side of the fuselage, in zone 231 (232) (127), the angle of attack sensor 3FP1 (3FP2) (3FP3) moves to the test position. On panels 130VU and 131VU, the MASTER WARN lights flash. You can hear the cricket aural warning and the STALL voice.
Push the line key adjacent to the YES indication.	On the MCDU: The TEST OK indication comes into view.
Push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.	The test procedure stops. The MASTER WARN lights go off. The cricket aural warning and the STALL voice stop. On the MCDU: The CFDS menu page comes into view.

Subtask 34-10-00-710-062-P ** ON A/C NOT FOR ALL

A. Test of the Angle of Attack Warning

ACTION	RESULT
1.On ADIRS MSU panel 41VU: Set the three OFF/NAV/ATT selector switches to NAV.	On the CAPT and F/O PFDs: Make sure that the CAS, ALT, V/S data are shown. Make sure that the attitude data is shown for 40 seconds after the start up.
2.On MCDU1 or MCDU2, on the NAV page:	On MCDU1 or MCDU2:
Push the line key adjacent to the ADR1 (ADR2) (ADR3) indication.	The ADIRS ADR1 (ADR2) (ADR3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	The OUTPUT TESTS page comes into view.
Push the line key adjacent to the AOA SENSOR TEST indication.	The AOA SENSOR TEST page comes into view with these indications: * AOA SENSOR COMMANDED TO FIXED POSITION * MAKE SURE THAT THE AURAL STALL WARNING IS GENERATED. On the left (right) side of the fuselage, in zone 231 (232) (127), the angle of attack sensor 3FP1 (3FP2) (3FP3) moves to the test position. On panels 130VU and 131VU, the MASTER WARN lights flash. You can hear the cricket aural warning and the STALL voice.
Push the line key adjacent to the YES indication.	On the MCDU: The TEST OK indication comes into view.
Push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.	The test procedure stops. The MASTER WARN lights go off. The cricket aural warning and the STALL voice stop. On the MCDU: The CFDS menu page comes into view.
If there is no STALL voice at the end of the test for ADR1, do the test for ADR2 or ADR3. Then, do the test for ADR1 again to make sure that the STALL voice operates correctly. NOTE: It is possible that there is no STALL voice at the end of the test for ADR1 because the FWS reset was done with the ADIRU set to NAV.

Subtask 34-10-00-710-062-Q

A. Test of the Angle of Attack Warning

ACTION	RESULT
1.On the ADIRS CDU: Set the three OFF/NAV/ATT selector switches to NAV.	On the CAPT and F/O PFDs: Make sure that the CAS, ALT, V/S data are shown. Make sure that the attitude data is shown for 40 seconds after the start up.
2.On MCDU1 or MCDU2, on the NAV page:	On MCDU1 or MCDU2:
Push the line key adjacent to the ADR1 (ADR2) (ADR3) indication.	The ADIRS ADR1 (ADR2) (ADR3) page comes into view.
Push the line key adjacent to the OUTPUT TESTS indication.	The OUTPUT TESTS page comes into view.
Push the line key adjacent to the AOA SENSOR TEST indication.	The AOA SENSOR TEST page comes into view with these indications: * AOA SENSOR COMMANDED TO FIXED POSITION * MAKE SURE THAT THE AURAL STALL WARNING IS GENERATED. On the left (right) side of the fuselage, in zone 231 (232) (127), the angle of attack sensor 3FP1 (3FP2) (3FP3) moves to the test position. On panels 130VU and 131VU, the MASTER WARN lights flash. You can hear the cricket aural warning and the STALL voice.
Push the line key adjacent to the YES indication.	On the MCDU: The TEST OK indication comes into view.
Push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.	The test procedure stops. The MASTER WARN lights go off. The cricket aural warning and the STALL voice stop. On the MCDU: The CFDS menu page comes into view.
If there is no STALL voice at the end of the test for ADR1, do the test for ADR2 or ADR3. Then, do the test for ADR1 again to make sure that the STALL voice operates correctly. NOTE: It is possible that there is no STALL voice at the end of the test for ADR1 because the FWS reset was done with the ADIRU set to NAV.

5. Close-up
Subtask 34-10-00-865-088-A

A. Table of the circuit breakers used in this procedure:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
121VU	T/TISS	2004SG	K07

Subtask 34-10-00-860-082-A ** ON A/C NOT FOR ALL

B. Reset of the T/TISS

Open the circuit breaker (1004SG or 2004SG) and wait approximately 10 seconds.
Close the circuit breaker (1004SG or 2004SG).

Subtask 34-10-00-860-066-A ** ON A/C NOT FOR ALL

C. Put the aircraft back to its initial configuration.
(1) On the ADIRS CDU, set the three OFF/NAV/ATT selector switches to OFF.
(2) On the overhead panel:

On flight control panels 23VU and 24VU, make sure that the FAC, ELAC and SEC pushbutton switches are pushed. The OFF legends are off.

(3) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
(5) Install the AOA sensor protections, if necessary (Ref. AMM TASK 10-11-00-555-013).
(6) Remove the access platform(s).

Subtask 34-10-00-860-066-B ** ON A/C NOT FOR ALL

C. Put the aircraft back to its initial configuration.
(1) On ADIRS MSU panel 41VU, set the three OFF/NAV/ATT selector switches to OFF.
(2) On the overhead panel:

On flight control panels 23VU and 24VU, make sure that the FAC, ELAC and SEC pushbutton switches are pushed. The OFF legends are off.

Subtask 34-10-00-865-077-A

D. 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
121VU	AUTO FLT/FAC2/28VDC	5CC2	M19

Subtask 34-10-00-410-064-A

E. Close Access
(1) Install the protective cover on battery power-center 105VU.
(2) Tighten the two screws.
(3) Close access door 822.
(4) Remove the access platform(s).

[Rev.10 from 2021] 2026.04.01 00:58:07 UTC