BITE Check Using MCDU to Ensure "Gear NOT DOWN for Landing" Warnings Operative
TASK 32-61-00-710-001-A
BITE Check Using MCDU to Ensure "Gear NOT DOWN for Landing" Warnings Operative
Refer to the MPD TASK: 323100-06
BITE CHECK USING MCDU TO ENSURE "GEAR NOT DOWN FOR LANDING" WARNINGS OPERATIVE
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 32-61-00-941-051-A
Subtask 32-61-00-710-050-A
Subtask 32-61-00-865-050-A
[Rev.10 from 2021]
2026.04.01 00:52:06 UTC
BITE Check Using MCDU to Ensure "Gear NOT DOWN for Landing" Warnings Operative
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.
ZONE: 210
1. Reason for the JobRefer to the MPD TASK: 323100-06
BITE CHECK USING MCDU TO ENSURE "GEAR NOT DOWN FOR LANDING" WARNINGS OPERATIVE
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) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 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 27-50-00-866-008-A | Extension of the Flaps on the Ground |
| TASK 27-50-00-866-008-A-01 | Extension of the Flaps/Slats on the Ground |
| 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 31-32-00-860-009-A | Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| TASK 32-00-00-481-001-A | Installation of the Safety Devices on the Landing Gears |
| TASK 32-00-00-860-001-A | Flight Configuration Precautions with Electrical Power |
| TASK 32-00-00-860-001-A-01 | Flight Configuration Precautions without Electrical Power |
| TASK 32-00-00-860-002-A | Ground Configuration after Flight Configuration with Electrical Power |
| TASK 32-00-00-860-002-A-01 | Ground Configuration after Flight Configuration without Electrical Power |
Subtask 32-61-00-941-051-A
A. Safety Precautions
(1) Put the SAFETY BARRIER(S) in position.
(2) Make sure that the ground safety locks are on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
(a) Make sure that the landing-gear control-lever is in the DOWN position
(b) Put a WARNING NOTICE(S) in position to tell persons not to operate the landing gear.
Subtask 32-61-00-860-050-A (1) Put the SAFETY BARRIER(S) in position.
(2) Make sure that the ground safety locks are on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On panel 400VU:
(a) Make sure that the landing-gear control-lever is in the DOWN position
(b) Put a WARNING NOTICE(S) in position to tell persons not to operate the landing gear.
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Fully extend the flaps (Ref. AMM TASK 27-50-00-866-008).
(3) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(4) On the ECAM control panel (CP), push (in) the WHEEL pushbutton switch (P/BSW). Make sure that the WHEEL page shows on the ECAM lower display unit (DU).
Subtask 32-61-00-869-052-A (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Fully extend the flaps (Ref. AMM TASK 27-50-00-866-008).
(3) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(4) On the ECAM control panel (CP), push (in) the WHEEL pushbutton switch (P/BSW). Make sure that the WHEEL page shows on the ECAM lower display unit (DU).
C. Flight Configuration Precautions
(1) Do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) before you open the LGCIU circuit breaker.
Subtask 32-61-00-865-052-A (1) Do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) before you open the LGCIU circuit breaker.
D. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 32-61-00-865-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | ENGINE/2/FADEC A/AND EIU 2 | 2KS2 | A05 |
| 49VU | ENGINE/1/FADEC A/AND EIU 1 | 2KS1 | A04 |
| 49VU | CAPT/LOUD/SPKR | 5WW | F10 |
| 49VU | FWS/FWC1/SPLY | 3WW | F01 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | ENGINE/ENG2/FADEC B | 4KS2 | Q40 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | ENGINE/ENG1/FADEC B/AND EIU 1 | 4KS1 | R41 |
| ** ON A/C ALL | |||
| 121VU | COM NAV/RAD ALTM/2 | 1SA2 | K12 |
| 121VU | COM NAV/RAD ALTM/1 | 1SA1 | K11 |
| 121VU | EIS/F/O/LOUD/SPKR | 4WW | P08 |
| 121VU | EIS/FWC2/SPLY | 2WW | Q07 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | ENGINE/ENG2/FADEC B/AND EIU2 | 4KS2 | Q40 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | ENGINE/ENG2/FADEC B/AND EIU2 | 4KS2 | R41 |
| 121VU | ENGINE/ENG1/FADEC B/AND EIU 1 | 4KS1 | R40 |
E. Open, safety and tag this(these) circuit breaker(s):
Subtask 32-61-00-869-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
F. Cockpit Configuration
(1) On panel 115VU, make sure that the ENG MASTER 1 and MASTER 2 levers are set to the OFF position.
(2) On panel 50VU, push (in) and release (out) the FADEC GND PWR 1 or 2 P/BSW. Make sure that the applicable P/BSW ON light comes on.
(3) Make sure that the throttle control levers are in the 0 (idle stop) position.
(4) Get access to the L/G page on the MCDU (Ref. AMM TASK 31-32-00-860-009).
4. Procedure(1) On panel 115VU, make sure that the ENG MASTER 1 and MASTER 2 levers are set to the OFF position.
(2) On panel 50VU, push (in) and release (out) the FADEC GND PWR 1 or 2 P/BSW. Make sure that the applicable P/BSW ON light comes on.
(3) Make sure that the throttle control levers are in the 0 (idle stop) position.
(4) Get access to the L/G page on the MCDU (Ref. AMM TASK 31-32-00-860-009).
Subtask 32-61-00-710-050-A
A. BITE Check With Use of MCDU to Ensure "Gear NOT DOWN for Landing" Warnings Operative
(1) Do this test:
5. Close-up(1) Do this test:
| ACTION | RESULT |
|---|---|
| 1.On the MCDU: | On the MCDU: |
|
|
|
|
|
|
|
|
|
|
| | On the ECAM lower DU:
|
| | On 402VU: |
| | - The UNLK (red) indicator lights show. |
| | On the ECAM upper DU:
|
| | On panels 130VU and 131VU:
|
| | On the Landing-Gear Normal Control-Lever (6GA):
|
| 2.On the ECAM CP: | |
| The warning chime stops. |
| | On the panels 130VU and 131VU:
|
| | On 402VU: |
| | - The UNLK (red) indicator lights stay on. |
| 3.On the MCDU: | On the ECAM upper DU: |
|
|
| | - The UNLK (red) indicator lights go out and the LKD (green) indicator lights come on. |
| | On the Landing-Gear Normal Control-Lever (6GA):
|
| | On the ECAM lower DU:
|
| 4.Push (in) the RETURN P/BSW until the CFDS menu page shows. |
|
| 5.Push in the MCDU MENU P/BSW. | |
Subtask 32-61-00-865-050-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 32-61-00-860-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R33 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/LGCIU/SYS2 | 2GA | Q35 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | LGCIU/BAT SPLY/SYS2 | 59GA | R32 |
B. Aircraft Maintenance Configuration
(1) Put the aircraft back to the ground configuration (Ref. AMM TASK 32-00-00-860-002).
(2) Fully retract the flaps (Ref. AMM TASK 27-50-00-866-009).
(3) Cockpit Configuration:
(a) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(b) On panel 50VU:
1 Push (in) the FADEC GND PWR 1 or 2 P/BSW. Make sure that the applicable P/BSW ON light goes off.
(4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 32-61-00-942-051-A (1) Put the aircraft back to the ground configuration (Ref. AMM TASK 32-00-00-860-002).
(2) Fully retract the flaps (Ref. AMM TASK 27-50-00-866-009).
(3) Cockpit Configuration:
(a) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(b) On panel 50VU:
1 Push (in) the FADEC GND PWR 1 or 2 P/BSW. Make sure that the applicable P/BSW ON light goes off.
(4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
C. Removal of Equipment
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the SAFETY BARRIER(S).
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the SAFETY BARRIER(S).
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.