Test Program after Removal/Installation of a VU Panel

TASK 31-10-00-700-001-A
Test Program after Removal/Installation of a VU Panel

CAUTION: DO NOT USE THIS PROCEDURE TO SWAP VU PANELS BETWEEN AIRCRAFT. THIS PROCEDURE IS USED TO REMOVE AND INSTALL A VU PANEL ON AN AIRCRAFT. VU PANELS ARE NOT LINE REPLACEABLE UNITS (LRU).

ZONE: 210

1. Reason for the Job
Do the tests necessary to make sure that all the primary functions are operational after removal/installation of VU panel.
It is possible that your version of the panel does not have all of these functions. Do only the tests that are applicable to your version of the panel.
2. Job Set-up Information
A. Work Zones and Access Panels

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

B. Referenced Information

REFERENCE	DESIGNATION
TASK 21-21-00-710-001-A	Operational Test of the Cabin Recirculation Fans
TASK 21-26-00-710-002-A	Operational Check of Override Function (BLOWER and EXTRACT)
TASK 21-31-00-710-003-A	Operational Test of Manual Mode Selection and Manual Mode Pressure Control and Functional Test of Manual Mode Cabin Altitude/Outflow Valve Position Indication
TASK 21-31-00-710-004-A	Operational Test of the Outflow Valve Closing in Ditching Configuration
TASK 21-43-00-710-002-A	Operational Test of the FWD Cargo Compartment Heating System
TASK 21-51-00-710-002-A	Operational Test of the Flow Control and Indicating System
TASK 21-51-00-710-003-A	Operational Test of the Flow Control Valves Closing
TASK 21-55-00-710-001-A	Operational Check of the Emergency Ram-Air Inlet System
TASK 21-63-00-720-001-A	Functional Test of the Cockpit and Cabin Temperature Control without CFDS/MCDU.
TASK 22-60-00-710-002-A	Operational Test of the Automatic Change-Over Function
TASK 22-70-00-610-008-A	Uploading of the Flight Management (FM) Data to the Flight Management and Guidance Computer (FMGC)
TASK 22-70-00-610-008-C	Uploading of the Flight Management (FM) Data to the Flight Management and Guidance Computer (FMGC)
TASK 22-70-00-610-008-C-01	Uploading of the Flight Management (FM) Data to the Flight Management and Guidance Computer (FMGC)
TASK 22-70-00-610-008-D	Uploading of the Flight Management (FM) Data to the Flight Management and Guidance Computer (FMGC)
TASK 22-70-00-610-008-H	Uploading of the Flight Management (FM) Data to the Flight Management and Guidance Computer (FMGC)
TASK 22-96-00-710-001-A	Operational Test of the AFS
TASK 22-97-00-710-001-A	Operational Test of the LAND CAT III Capability
TASK 23-36-00-710-001-A	Operational Test of the Passenger Entertainment (Video)
TASK 23-42-00-710-001-A	Operational Test of the Mechanic Call
TASK 23-44-00-700-001-A	Operational Test of the Service Interphone
TASK 23-51-00-710-001-A	Operational Test of the Audio Management Unit (AMU)
TASK 23-71-00-710-001-A	Operational Check of CVR and CVR-Channel Recording
TASK 23-71-00-720-002-A	Functional Test of the bulk-erase function and bulk-erase inhibition-logic of the CVR
TASK 23-73-00-710-003-A	Operational Test of the Cabin and Flight Crew Interphone System
TASK 23-73-00-710-004-A	Operational Test of the Emergency Evacuation (EVAC) Signaling System
TASK 23-73-00-710-017-A	Operational Test of the Cabin Signs
TASK 23-73-00-710-021-A	Operational Test of the Cabin and Flight Crew Interphone System
TASK 23-73-00-710-026-A	Operational Test of the Emergency Evacuation (EVAC) Signaling System
TASK 23-73-00-710-040-A	Operational Test of the Cabin/Cockpit Incident Alert System
TASK 23-73-00-710-042-A	Operational Test of the Battery-Bus powered PA
TASK 24-21-00-710-040-A	Operational Test of the IDG Disconnect and Reconnect Function - Engine Static
TASK 24-21-00-710-042-A	Operational Test of the IDG Disconnect and Reconnect Function - Engine Static
TASK 24-21-00-710-803-A	Operational Test of the IDG Disconnect and Reconnect Function - Engine Static
TASK 24-21-00-710-803-A-01	Operational Test of the IDG Disconnect and Reconnect Function - Engine in Operation
TASK 24-22-00-710-001-A	Operational Test of the Generator Line Contactor (GLC-1) Opening in the Smoke Procedure
TASK 24-22-00-710-002-A	Operational Test of the Transfer Inhibition
TASK 24-24-00-710-001-A	Operational Check of Emergency Generating System
TASK 24-25-00-710-001-A	Operational Check of AC ESS Generation Switching
TASK 24-26-00-710-002-A	Operational Check of the Manual and Automatic Galley and Bus Shedding
TASK 24-28-00-710-001-A	Operational Test of the Static Inverter when the Aircraft Electrical Circuits are Energized from the External Power
TASK 24-28-00-710-001-A-01	Operational Test of the Static Inverter when the Aircraft Electrical Circuits are Energized from the APU
TASK 24-41-00-740-002-B	Operational Check of the GAPCU via the CFDS
TASK 24-41-00-740-004-A	Operational Check of the GPCU via the CFDS
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 24-56-00-710-001-A	Operational Test of the Galley Supply
TASK 25-65-00-740-001-A	Emergency Locator Transmitter (ELT) System - BITE Test
TASK 26-12-00-710-001-A	Operational Check of Loop/Squib
TASK 26-16-00-710-001-A	Operational Check of Cargo Compartment Smoke Detection by PTT
TASK 26-16-00-710-003-A	Operational Check of Cargo Compartment Smoke Detection by CFDS to Confirm Isolation Valves Latching Circuit Integrity.
TASK 26-22-00-710-001-A	Operational Test of the APU Fire-Extinguishing Loop/Squib
TASK 26-23-00-710-001-A	Operational Test of the Cargo-Compartment Fire-Extinguishing System
TASK 26-23-00-710-003-A	Check Firing Circuit Continuity and Perform Operational Check of Priority Switching
TASK 26-23-00-710-003-A-01	Check Firing Circuit Continuity and Perform Operational Check of Priority Switching
TASK 26-23-00-710-004-A	Perform Functional Check of Time Delay for Illumination of "Disch Agent 2" Reminder Light
TASK 26-23-00-720-001-A	Check Firing Circuit Continuity
TASK 26-23-00-720-001-A-01	Check Firing Circuit Continuity
TASK 27-22-00-710-001-A	Operational Test of the Reset Function
TASK 27-51-00-710-001-A	Operational Test of the Wing Tip Brake and the Pressure Off Brake
TASK 27-54-00-710-001-A	Operational Test of the Flap System
TASK 27-96-00-710-002-A	Operational Test of the Computers Engagement/Disengagement
TASK 27-96-00-710-003-A	Operational Test of the Side Stick Priority
TASK 28-21-00-710-001-A	Operational Test of the Wing-Tank Fuel Control
TASK 28-21-00-710-010-A	Operational Test of the Center-Tank Pump Control
TASK 28-23-00-720-001-A	Operational Check of Crossfeed Valve Using Individual Motors and Check Fuel Flow in "Open" and Fuel Shut Off in "Closed" Positions
TASK 28-25-00-710-003-A	Operational Test of the Refuel System
TASK 28-26-00-710-001-A	Operational Test of the Main Transfer System
TASK 28-28-00-710-001-A	Operational Check of the ACT Manual Transfer System
TASK 29-10-00-720-001-A	Functional Check of Hydraulic Fire Shut-Off Valves
TASK 29-10-00-720-802-A	Functional Check of Hydraulic Fire Shut-Off Valves
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 29-10-00-863-003-A-01	Pressurize the Blue Hydraulic System with the Blue Electric Pump
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 29-12-00-710-001-A	Functional Check of Blue Electrical Pump Pressure by Reading ECAM Indication
TASK 29-14-00-614-002-A	Pressurization of the Hydraulic Reservoirs through the Ground Connector
TASK 29-14-00-614-002-A-01	Pressurization of the Hydraulic Reservoirs with the Auxiliary Power Unit (APU)
TASK 29-22-00-710-007-A	Operational Test of the Manual Deployment and the Retraction of the Ram Air Turbine
TASK 29-22-00-869-005-A	Extension of the Ram Air Turbine (RAT) on the Ground
TASK 29-22-00-869-006-A	Retraction of the Ram Air Turbine (RAT) on the Ground
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 30-11-00-710-001-A	Operational Test of the Wing Ice-Protection System
TASK 30-21-00-710-002-A	Operational Check of the Engine-Air-Intake Ice-Protection System (with the Engines in operation)
TASK 30-42-00-710-001-A	Operational Test of the Windshield Anti-Icing and Defogging
TASK 30-45-00-200-001-A	Inspection/Check of the Operation of the Windshield Wipers.
TASK 30-45-00-720-001-A	Functional Test of the Windshield Rain Protection
TASK 31-32-00-600-001-A	Uploading of the Maintenance Filter Data Base to the CFDIU with the Portable Data Loader (SFIM)
TASK 31-32-00-600-001-C	Uploading of the Maintenance Filter Data Base to the CFDIU
TASK 31-32-00-600-001-D	Uploading of the Maintenance Filter Data Base to the CFDIU
TASK 31-50-00-710-002-A	Operational Test of the Flight Warning Computer (FWC)
TASK 31-50-00-710-003-A	Operational Test of the System Data Acquisition Concentrator (SDAC)
TASK 31-60-00-710-002-A	Operational Test of EFIS/ECAM Switching Functions
TASK 31-60-00-710-003-A	PFD/ND/Upper and Lower ECAM Display Units (DU) - Brightness
TASK 31-60-00-710-005-A	Operational Check of Correct Operation of EFIS and ECAM DMC Automatic and Manual Transfer
TASK 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure
TASK 32-42-00-710-003-A	Operational Check of Antiskid Inhibition
TASK 32-42-00-710-005-A	Operational test of the autobrake deceleration rate arming
TASK 32-45-00-710-001-A	Operational Check of the Parking Brake System
TASK 33-12-00-710-001-A	Operational Test of the General Illumination
TASK 33-13-00-710-001-A	Operational Test of the Instrument and Panel Integral-Lighting
TASK 33-14-00-710-001-A	Operational Check of the Light Test System
TASK 33-35-00-720-001-A	Functional Test of the Avionics-Compartment Lighting
TASK 33-41-00-710-001-A	Operational Test of the Navigation Lights
TASK 33-42-00-710-001-A	Operational Test of the Landing Lights
TASK 33-43-00-710-001-A	Operational Test of the Runway Turnoff Lights
TASK 33-46-00-710-001-A	Operational Test of the Taxi and Take Off Lights
TASK 33-47-00-710-002-A	Operational Test of the Logo Lights
TASK 33-48-00-710-001-A	Operational Test of the Anti-Collision Lighting
TASK 33-48-00-710-002-A	Operational Test of the Anti-Collision/Strobe Lighting
TASK 33-49-00-710-001-A	Operational Test of the Wing and Engine Scan Lights
TASK 33-51-00-710-004-A	Check of the Manual Operation from the two Control Panels and of all the Cabin Lights and Signs illuminated by Batteries
TASK 34-10-00-710-007-A	Test of the Angle of Attack (AOA) Warning
TASK 34-10-00-860-005-A	ADIRS Stop Procedure
TASK 34-11-15-710-001-A	Test of the Pitot Probe without the CFDS
TASK 34-13-00-710-001-A	Operational Test of the AIR DATA Switching Function
TASK 34-13-00-710-009-A	Operational Check of the Back Up Speed Scale Display
TASK 34-14-00-710-003-A	Operational Test of the Attitude/Heading (ATT/HDG) Switching Function
TASK 34-14-00-740-001-A	Interface Test of the IR
TASK 34-22-25-710-001-A	Operational Check of ISIS DC HOT Bus SUPPLY
TASK 34-43-00-740-001-A	BITE Test of the TCAS
TASK 34-43-00-740-001-C	BITE Test of the TCAS
TASK 34-48-00-710-001-B	Operational Check of Ground Self Test System
TASK 34-48-00-710-001-G	Operational Check of Ground Self Test System
TASK 34-72-00-740-001-A	BITE Test of the T/TISS
TASK 35-12-00-710-001-A	Functional Check of Low Pressure Switch
TASK 35-23-00-710-001-A	Operational Check of Manual Mask Release
TASK 36-11-00-710-003-A	Operational Test of the Bleed Air System
TASK 49-00-00-710-008-A	Operational Test of the APU
TASK 49-00-00-710-010-A	Operational Test of the APU
TASK 49-62-00-710-004-A	Operational Test of the Emergency Shutdown Circuit (using the APU Shut Off Switch 1KL) (APS 3200)
TASK 49-62-00-710-007-A	Operational Test of Emergency Shutdown System (with APU SHUT OFF Switch 1KL) (131-9(A))
TASK 52-51-00-710-002-A	Operational Test of the Cockpit-Door Locking System (CDLS)
TASK 52-51-12-400-001-A	Installation of the Electrical Release Strike
TASK 73-21-00-710-806-A	Test No.7 - EEC Operation Test (Self Test)
TASK 73-21-60-720-040-A	Functional Test of the Electronic Control Unit (ECU)
TASK 73-21-60-720-040-B	Functional Test of the Electronic Control Unit (ECU)
TASK 73-22-34-710-040-A	Operational Test of the EEC
ESPM 2052100

3. Job Set-up
Subtask 31-10-00-860-050-A

A. Not applicable.

4. Procedure

NOTE: Some aircraft do not have all the systems/functions referred to in this procedure. Ignore the tests related to systems/functions that are not installed on your aircraft.

Subtask 31-10-00-710-050-A

A. Preliminary Tests
(1) Do a visual check of the locking connectors ESPM 2052100.
(2) Do the operational test of the instrument and panel integral-lighting (Ref. AMM TASK 33-13-00-710-001).
(3) Do the operational test of the lights (Ref. AMM TASK 33-14-00-710-001).

Subtask 31-10-00-710-051-A ** ON A/C NOT FOR ALL

B. Test Program after Removal/Installation of Panel 8VU
(1) Do the operational test of the EFIS/ECAM switching functions (Ref. AMM TASK 31-60-00-710-002).
(2) Do the operational test of the AIR DATA switching function (Ref. AMM TASK 34-13-00-710-001).
(3) Do the operational test of the ATT/HDG switching function (Ref. AMM TASK 34-14-00-710-003).

Subtask 31-10-00-710-051-B ** ON A/C NOT FOR ALL

B. Test Program after Removal/Installation of Panel 8VU
(1) Do the operational test of the EFIS/ECAM DMC automatic and manual transfer (Ref. AMM TASK 31-60-00-710-005).
(2) Do the operational test of the AIR DATA switching function (Ref. AMM TASK 34-13-00-710-001).
(3) Do the operational test of the ATT/HDG switching function (Ref. AMM TASK 34-14-00-710-003).

Subtask 31-10-00-710-052-A

C. Test Program after Removal/Installation of Panel 15VU
(1) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).

Subtask 31-10-00-710-053-A

D. Test Program after Removal/Installation of Panel 16VU
(1) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).

Subtask 31-10-00-710-054-A

E. Test Program after Removal/Installation of Panel 17VU
(1) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).

Subtask 31-10-00-710-055-A ** ON A/C NOT FOR ALL

F. Test Sequence after the Removal/Installation of Panel 21VU
(1) Do the operational test of the passenger entertainment (video) (if installed) (Ref. AMM D/O 23-36-00-71).
(2) Do the operational test of the mechanic call (Ref. AMM TASK 23-42-00-710-001).
(3) Do the operational test of the Cockpit Voice Recorder (CVR) and the CVR channel recording (Ref. AMM TASK 23-71-00-710-001).
(4) Do the operational test of the cabin and flight crew interphone-system (if installed) (Ref. AMM TASK 23-73-00-710-003).
(5) Do the operational test of the emergency Evacuation (EVAC) signaling system (if installed) (Ref. AMM D/O 23-73-00-71).
(6) Do the operational test of the battery-bus powered Passenger Address (PA) system (if available) (Ref. AMM TASK 23-73-00-710-042).
(7) Do the operational test of the cabin and flight crew interphone-system (if installed) (Ref. AMM D/O 23-73-00-71).
(8) Do the operational test of the emergency EVAC signaling system (if installed) (Ref. AMM D/O 23-73-00-71).
(9) Do the operational test of the opening of the Generator Line Contactor-1 (GLC1) in the smoke procedure (Ref. AMM TASK 24-22-00-710-001).
(10) Do the operational test of the emergency generation system (Ref. AMM TASK 24-24-00-710-001).
(11) Do the inspection/check of the operation of the windshield wipers (Ref. AMM TASK 30-45-00-200-001).
(12) Do the functional test of the windshield rain protection (Ref. AMM TASK 30-45-00-720-001).
(13) Do the step that follows:

Do the operational test of the (enhanced, if applicable) Ground Proximity Warning System (GPWS) ground self-test function (if available) (Ref. AMM TASK 34-48-00-710-001), or
Do the BITE test of the Traffic and Terrain Integrated Surveillance System (T/TISS) (Terrain Awareness and Warning System (TAWS) part) (if available) (Ref. AMM D/O 34-72-00-74).

(14) Do the BITE test of the Traffic Alert and Collision Avoidance System (TCAS) (if available) (Ref. AMM TASK 34-43-00-740-001) or (Ref. AMM TASK 34-43-00-740-002) or (Ref. AMM D/O 34-43-00-74).
(15) Do the BITE test of the Traffic and Terrain Collision Avoidance System (T2CAS) (if available) (Ref. AMM D/O 34-43-00-74).
(16) Do the BITE test of the T/TISS (TCAS part) (if available) (Ref. AMM D/O 34-72-00-74).
(17) Do the functional check of the low pressure switch (Ref. AMM TASK 35-12-00-710-001).
(18) Do the operational check of the manual mask release (if available) (Ref. AMM TASK 35-23-00-710-001).
(19) Do the operational check of the DC HOT bus supply of the standby horizon indicator (7FN):

ACTION	RESULT
1.On overhead circuit breaker panel 49VU, open circuit breaker 5FN.	On left center instrument panel 401VU, on the standby horizon indicator: The flag comes into view.
2.On the overhead panel: On overhead control and indicator panel 21VU, push and hold the EMER GEN TEST pushbutton switch. At the same time, on electrical panel 35VU, release the EXT PWR pushbutton switch.	The flag goes out of view in less than two minutes.
3.On the overhead panel: On overhead control and indicator panel 21VU, release the EMER GEN TEST pushbutton switch. On electrical panel 35VU, push the EXT PWR pushbutton switch.	The flag comes into view.
4.On overhead circuit breaker panel 49VU, close circuit breaker 5FN.	The flag goes out of view in less than two minutes.

(20) Do the steps that follow:

Do the extension of the Ram Air Turbine (RAT) on the ground (if available) (Ref. AMM D/O 29-22-00-86) and the retraction of the RAT on the ground (if available) (Ref. AMM D/O 29-22-00-86), or
Do the extension of the RAT on the ground (if available) (Ref. AMM TASK 29-22-00-869-005) and the retraction of the RAT on the ground (if available) (Ref. AMM TASK 29-22-00-869-006).

Subtask 31-10-00-710-055-B ** ON A/C NOT FOR ALL

F. Test Sequence after the Removal/Installation of Panel 21VU
(1) Do the operational test of the passenger entertainment (video) (if installed) (Ref. AMM TASK 23-36-00-710-001).
(2) Do the operational test of the mechanic call (Ref. AMM TASK 23-42-00-710-001).
(3) Do the operational test of the Cockpit Voice Recorder (CVR) and the CVR channel recording (Ref. AMM TASK 23-71-00-710-001).
(4) Do the operational test of the cabin and flight crew interphone-system (if installed) (Ref. AMM TASK 23-73-00-710-003).
(5) Do the operational test of the emergency Evacuation (EVAC) signaling system (if available) (Ref. AMM TASK 23-73-00-710-004).
(6) Do the operational test of the battery-bus powered Passenger Address (PA) system (if available) (Ref. AMM TASK 23-73-00-710-042).
(7) Do the operational test of the cabin and flight crew interphone-system (if installed) (Ref. AMM TASK 23-73-00-710-021).
(8) Do the operational test of the emergency EVAC signaling system (if installed) (Ref. AMM TASK 23-73-00-710-026).
(9) Do the operational test of the opening of the Generator Line Contactor-1 (GLC1) in the smoke procedure (Ref. AMM TASK 24-22-00-710-001).
(10) Do the operational test of the emergency generation system (Ref. AMM TASK 24-24-00-710-001).
(11) Do the inspection/check of the operation of the windshield wipers (Ref. AMM TASK 30-45-00-200-001)
(12) Do the functional test of the windshield rain protection (Ref. AMM TASK 30-45-00-720-001).
(13) Do the step that follows:

Do the operational test of the enhanced Ground Proximity Warning System (GPWS) ground self-test function (if available) (Ref. AMM TASK 34-48-00-710-001), or
Do the BITE test of the Traffic and Terrain Integrated Surveillance System (T/TISS) (Terrain Awareness and Warning System (TAWS) part) (if available) (Ref. AMM TASK 34-72-00-740-001).

(14) Do the BITE test of the Traffic Alert and Collision Avoidance System (TCAS) (if available) (Ref. AMM TASK 34-43-00-740-001) or (Ref. AMM D/O 34-43-00-74).
(15) Do the BITE test of the Traffic and Terrain Collision Avoidance System (T2CAS) (if available) (Ref. AMM D/O 34-43-00-74).
(16) Do the BITE test of the T/TISS (TCAS part) (if available) (Ref. AMM TASK 34-72-00-740-001).
(17) Do the functional check of the low pressure switch (Ref. AMM TASK 35-12-00-710-001).
(18) Do the operational check of the manual mask release (if available) (Ref. AMM TASK 35-23-00-710-001).
(19) Do the operational check of the DC HOT busbar supply of the Integrated Standby Instrument System (ISIS) (Ref. AMM TASK 34-22-25-710-001).
(20) Do the steps that follow:

Do the extension of the Ram Air Turbine (RAT) on the ground (if available) (Ref. AMM D/O 29-22-00-86) and the retraction of the RAT on the ground (if available) (Ref. AMM D/O 29-22-00-86), or
Do the extension of the RAT on the ground (if available) (Ref. AMM TASK 29-22-00-869-005) and the retraction of the RAT on the ground (if available) (Ref. AMM TASK 29-22-00-869-006).

Subtask 31-10-00-710-056-A ** ON A/C NOT FOR ALL

G. Test Program after Removal/Installation of Panel 22VU
(1) Do the operational test of cabin recirculation fans 14HG and 15HG (Ref. AMM TASK 21-21-00-710-001).
(2) Do the operational check of the override function (BLOWER and EXTRACT) (Ref. AMM TASK 21-26-00-710-002).
(3) Do the operational check of the fault warning (if installed) (Ref. AMM D/O 21-27-00-71).
(4) Do the operational test of the FWD cargo-compartment heating-system (if installed) (Ref. AMM D/O 21-43-00-71).
(5) Do the operational test of the landscape camera (if installed) (Ref. AMM D/O 23-36-00-71).
(6) Do the operational check of the cargo-compartment smoke detection by PTT (Ref. AMM TASK 26-16-00-710-001).
(7) Do the operational check of the cargo-compartment smoke detection by the CFDS to confirm the isolation-valve latching-circuit integrity (if the aft and/or the FWD cargo-compartment isolation-valve(s) is (are) installed) (Ref. AMM TASK 26-16-00-710-003).
(8) Do the operational test of the ground cooling isolation-valve to verify closing in case of smoke warning (if installed) (Ref. AMM D/O 26-16-00-71).
(9) Do the operational test of the cargo-compartment fire-extinguishing system (if installed) (Ref. AMM TASK 26-23-00-710-001).
(10) Do a check of the firing circuit continuity and do the operational test of the priority switching (if two fire extinguisher bottles are installed) (Ref. AMM TASK 26-23-00-710-003).
(11) Do the functional test of time delay for illumination of the "DISCH AGENT 2" reminder light (if two fire extinguisher bottles are installed) (Ref. AMM TASK 26-23-00-710-004).
(12) Do a check of firing circuit continuity (if installed) (Ref. AMM TASK 26-23-00-720-001).
(13) Do the inspection/check of the operation of the windshield wipers (Ref. AMM TASK 30-45-00-200-001).
(14) Do the functional test of the windshield rain protection (Ref. AMM TASK 30-45-00-720-001).
(15) Do the functional test of the ECU (Ref. AMM TASK 73-21-60-720-040).

Subtask 31-10-00-710-056-B ** ON A/C NOT FOR ALL

G. Test Program after Removal/Installation of Panel 22VU
(1) Do the operational test of the cabin recirculation fans 14HG and 15HG (Ref. AMM TASK 21-21-00-710-001).
(2) Do the operational test of the override function (BLOWER and EXTRACT) (Ref. AMM TASK 21-26-00-710-002).
(3) Do the operational check of fault warning (if installed) (Ref. AMM D/O 21-27-00-71).
(4) Do the operational test of the FWD cargo-compartment heating system (if installed) (Ref. AMM D/O 21-43-00-71).
(5) Do the operational test of the landscape camera (if installed) (Ref. AMM D/O 23-36-00-71).
(6) Do the operational check of the cargo-compartment smoke detection by Push-to-Test (PTT) (Ref. AMM TASK 26-16-00-710-001).
(7) Do the operational check of cargo-compartment smoke detection by Centralized Fault Display System (CFDS) to confirm isolation valve latching circuit integrity (if AFT and/or FWD cargo-compartment isolation-valve(s) installed) (Ref. AMM D/O 26-16-00-71).
(8) Do the operational test of the cargo-compartment fire-extinguishing system (if installed) (Ref. AMM TASK 26-23-00-710-001).
(9) Do a check of the firing circuit continuity and do the operational test of priority switching (if two fire extinguisher bottles installed) (Ref. AMM TASK 26-23-00-710-003).
(10) Do the functional test of time delay for illumination of "DISCH AGENT 2" reminder light (if two fire extinguisher bottles installed) (Ref. AMM TASK 26-23-00-710-004).
(11) Do a continuity check of the cargo-compartment firing-circuit (if installed) (Ref. AMM D/O 26-23-00-72).
(12) Do the inspection/check of the operation of the windshield wipers (Ref. AMM TASK 30-45-00-200-001).
(13) Do the functional test of the windshield rain protection (Ref. AMM TASK 30-45-00-720-001).
(14) Do the operational test of the Electronic Engine Control (EEC) (Ref. AMM TASK 73-22-34-710-040).

Subtask 31-10-00-710-056-E ** ON A/C NOT FOR ALL

G. Test Program after Removal/Installation of Panel 22VU
(1) Do the operational test of the cabin recirculation fans 14HG and 15HG (Ref. AMM TASK 21-21-00-710-001).
(2) Do the operational test of the override function (BLOWER and EXTRACT) (Ref. AMM TASK 21-26-00-710-002).
(3) Do the operational test of the FWD cargo-compartment heating system (if installed) (Ref. AMM TASK 21-43-00-710-002).
(4) Do the operational check of cargo-compartment smoke detection by PTT (Ref. AMM TASK 26-16-00-710-001).
(5) Do the operational check of cargo-compartment smoke detection by CFDS to confirm isolation valve latching circuit integrity (if AFT and/or FWD cargo compartment isolation valve(s) installed) (Ref. AMM TASK 26-16-00-710-003).
(6) Do the operational test of the cargo-compartment fire-extinguishing system (if installed) (Ref. AMM TASK 26-23-00-710-001).
(7) Do a check of the firing circuit continuity and do the operational test of priority switching (if two fire extinguisher bottles installed) (Ref. AMM TASK 26-23-00-710-003).
(8) Do the functional test of time delay for illumination of "DISCH AGENT 2" reminder light (if two fire extinguisher bottles installed) (Ref. AMM TASK 26-23-00-710-004).
(9) Do a continuity check of the cargo-compartment firing-circuit (if installed) (Ref. AMM TASK 26-23-00-720-001).
(10) Do the inspection/check of the operation of the windshield wipers (Ref. AMM TASK 30-45-00-200-001).
(11) Do the functional test of the windshield rain protection (Ref. AMM TASK 30-45-00-720-001).
(12) Do the EEC operation test (self-test) (Ref. AMM TASK 73-21-00-710-806).

Subtask 31-10-00-710-057-A

H. Test Program after Removal/Installation of Panel 23VU
(1) Do the operational test of the computer engagement/disengagement (Ref. AMM TASK 27-96-00-710-002).
(2) Do the operational test of the automatic change-over function (Ref. AMM TASK 22-60-00-710-002).

Subtask 31-10-00-710-058-A

I. Test Program after Removal/Installation of Panel 24VU
(1) Do the operational test of the computer engagement/disengagement (Ref. AMM TASK 27-96-00-710-002).
(2) Do the operational test of the automatic change-over function (Ref. AMM TASK 22-60-00-710-002).

Subtask 31-10-00-710-059-A

J. Test Program after Removal/Installation of Panel 25VU
(1) Do the operational test of the general illumination (Ref. AMM TASK 33-12-00-710-001).
(2) Do the operational test of the manual mode selection and manual mode pressure control and functional test of manual mode cabin altitude/outflow valve position indication (Ref. AMM TASK 21-31-00-710-003).
(3) Do the operational test of the outflow valve closing in ditching configuration (Ref. AMM TASK 21-31-00-710-004).
(4) Do the operational test of the cabin signs (only the test of the passengers lighted signs in Para. 4.A.) (if installed) (Ref. AMM TASK 23-73-00-710-017).
(5) Do the operational test of the wing ice-protection system (Ref. AMM TASK 30-11-00-710-001).
(6) Do the operational test of the windshield anti-icing and defogging (Ref. AMM TASK 30-42-00-710-001).
(7) Do the operational test of the engine air-intake ice-protection (with the engines in operation) (Ref. AMM TASK 30-21-00-710-002).
(8) Do the operational test of the lights (Ref. AMM TASK 33-14-00-710-001).
(9) Do the operational test of the navigation lights (Ref. AMM TASK 33-41-00-710-001).
(10) Do the operational test of the landing lights (Ref. AMM TASK 33-42-00-710-001).
(11) Do the operational test of the runway turnoff lights (Ref. AMM TASK 33-43-00-710-001).
(12) Do the operational test of the taxi and take off lights (Ref. AMM TASK 33-46-00-710-001).
(13) Do the operational test of the logo lights (if installed) (Ref. AMM TASK 33-47-00-710-002).
(14) Do the operational test of the anti-collision lighting (Ref. AMM TASK 33-48-00-710-001) or the operational test of the anti-collision/strobe lighting (Ref. AMM TASK 33-48-00-710-002).
(15) Do the operational test of the wing and engine scan lights (Ref. AMM TASK 33-49-00-710-001).
(16) Do the check of the manual operation from the two control panels and of all the cabin lights and signs illuminated by batteries (Ref. AMM TASK 33-51-00-710-004).
(17) Do the test of the pitot probes (9DA1, 9DA2, 9DA3) without the CFDS (Ref. AMM TASK 34-11-15-710-001).
(18) Do the operational test of the APU (GTCP 36-300) (Ref. AMM D/O 49-00-00-71).
(19) Do the operational test of the APU (APS 3200) (Ref. AMM TASK 49-00-00-710-008).
(20) Do the operational test of the APU (131-9(A)) (Ref. AMM TASK 49-00-00-710-010).

Subtask 31-10-00-710-060-A

K. Test Program after Removal/Installation of Panel 27VU
(1) Do the operational test of the PES (music) (if installed) (Ref. AMM D/O 23-33-00-71).
(2) Do the operational test of the passenger entertainment (video) (if installed) (Ref. AMM TASK 23-36-00-710-001).

Subtask 31-10-00-710-061-A

L. Test Program after Removal/Installation of Panel 30VU
(1) Do the operational test of the flow control and indicating system (Ref. AMM TASK 21-51-00-710-002).
(2) Do the operational test of the flow control valves closing (Ref. AMM TASK 21-51-00-710-003).
(3) Do the operational test of the emergency ram-air inlet (Ref. AMM TASK 21-55-00-710-001).
(4) Do the functional test of the cockpit and cabin temperature control without the CFDS/MCDU (Ref. AMM TASK 21-63-00-720-001).
(5) Do the operational test of the bleed air system (Ref. AMM TASK 36-11-00-710-003).

Subtask 31-10-00-710-062-E ** ON A/C NOT FOR ALL

M. Test Program after the Removal and the Installation of Panel 35VU
(1) Do the operational test of the Integrated Drive Generator (IDG) disconnect and reconnect function (Ref. AMM TASK 24-21-00-710-040).
(2) Do the operational test of the transfer inhibition (Ref. AMM TASK 24-22-00-710-002).
(3) Do the operational check of the AC essential-generation switching (Ref. AMM TASK 24-25-00-710-001).
(4) Do the operational check of the manual and automatic shedding of the galley and the bus (Ref. AMM TASK 24-26-00-710-002).
(5) Do the operational test of the static inverter (3XB) when the aircraft electrical circuits are energized from the external power (Ref. AMM TASK 24-28-00-710-001).
(6) Do the operational check of the Ground Power Control Unit (GPCU) with the Centralized Fault Display System (CFDS) (Ref. AMM TASK 24-41-00-740-004).
(7) Do the operational test of the galley supply (Ref. AMM TASK 24-56-00-710-001).

Subtask 31-10-00-710-062-G ** ON A/C NOT FOR ALL

M. Test Program after the Removal and the Installation of Panel 35VU
(1) Do the operational test of the Integrated Drive Generator (IDG) disconnect and reconnect function (Ref. AMM TASK 24-21-00-710-040).
(2) Do the operational test of the transfer inhibition (Ref. AMM TASK 24-22-00-710-002).
(3) Do the operational check of the AC essential-generation switching (Ref. AMM TASK 24-25-00-710-001).
(4) Do the operational check of the manual and automatic shedding of the galley and the bus (Ref. AMM TASK 24-26-00-710-002).
(5) Do the operational test of the static inverter (3XB) when the aircraft electrical circuits are energized from the external power (Ref. AMM TASK 24-28-00-710-001).
(6) Do the operational check of the Ground and Auxiliary Power Control Unit (GAPCU) with the Centralized Fault Display System (CFDS) (Ref. AMM TASK 24-41-00-740-002).
(7) Do the operational test of the galley supply (Ref. AMM TASK 24-56-00-710-001).

Subtask 31-10-00-710-062-J ** ON A/C NOT FOR ALL

M. Test Program after the Removal and the Installation of Panel 35VU
(1) Do the operational test of the Integrated Drive Generator (IDG) disconnect and reconnect function (Ref. AMM TASK 24-21-00-710-042).
(2) Do the operational test of the transfer inhibition (Ref. AMM TASK 24-22-00-710-002).
(3) Do the operational check of the AC essential-generation switching (Ref. AMM TASK 24-25-00-710-001).
(4) Do the operational check of the manual and automatic shedding of the galley and the bus (Ref. AMM TASK 24-26-00-710-002).
(5) Do the operational test of the static inverter (3XB) when the aircraft electrical circuits are energized from the external power (Ref. AMM TASK 24-28-00-710-001).
(6) Do the operational check of the Ground and Auxiliary Power Control Unit (GAPCU) with the Centralized Fault Display System (CFDS) (Ref. AMM TASK 24-41-00-740-002).
(7) Do the operational test of the galley supply (Ref. AMM TASK 24-56-00-710-001).

Subtask 31-10-00-710-062-N ** ON A/C NOT FOR ALL

M. Test Program after the Removal and the Installation of Panel 35VU
(1) Do the operational test of the Integrated Drive Generator (IDG) disconnect and reconnect function (Ref. AMM TASK 24-21-00-710-803).
(2) Do the operational test of the transfer inhibition (Ref. AMM TASK 24-22-00-710-002).
(3) Do the operational check of the AC essential-generation switching (Ref. AMM TASK 24-25-00-710-001).
(4) Do the operational check of the manual and automatic shedding of the galley and the bus (Ref. AMM TASK 24-26-00-710-002).
(5) Do the operational test of the static inverter (3XB) when the aircraft electrical circuits are energized from the external power (Ref. AMM TASK 24-28-00-710-001).
(6) Do the operational check of the Ground and Auxiliary Power Control Unit (GAPCU) with the Centralized Fault Display System (CFDS) (Ref. AMM TASK 24-41-00-740-002).
(7) Do the operational test of the galley supply (Ref. AMM TASK 24-56-00-710-001).

Subtask 31-10-00-710-063-A ** ON A/C NOT FOR ALL

N. Test Program after Removal/Installation of Panel 40VU
(1) Do the operational test of the center tank pump control (Ref. AMM TASK 28-21-00-710-010).
(2) Do the operational test of the wing-tank fuel control (Ref. AMM TASK 28-21-00-710-001).
(3) Do the operational test of the crossfeed valve using individual motors (Ref. AMM TASK 28-23-00-720-001).
(4) Do the operational test of the ACT manual transfer system (if installed) (Ref. AMM D/O 28-28-00-71).
(5) Do the functional test of hydraulic fire shut-off valves 1046GK and 3046GD (Ref. AMM TASK 29-10-00-720-001).
(6) Do the operational test of the manual deployment and the retraction of the RAT (if installed) (Ref. AMM D/O 29-22-00-71).
(7) Do the operational test of the manual deployment and the retraction of the RAT (if installed) (Ref. AMM TASK 29-22-00-710-007).

Subtask 31-10-00-710-063-B ** ON A/C NOT FOR ALL

N. Test Program after Removal/Installation of Panel 40VU
(1) Do the operational test of the wing-tank fuel control (Ref. AMM TASK 28-21-00-710-001).
(2) Do the operational test of the crossfeed valve using individual motors (Ref. AMM TASK 28-23-00-720-001).
(3) Do the operational test of the ACT manual transfer-system (if installed) (Ref. AMM TASK 28-28-00-710-001).
(4) Do the functional test of hydraulic-fire shut-off valves 1046GK and 3046GD (Ref. AMM TASK 29-10-00-720-802).
(5) Do the operational test of the manual deployment and the retraction of the RAT (if installed) (Ref. AMM TASK 29-22-00-710-007).

Subtask 31-10-00-710-063-C ** ON A/C NOT FOR ALL

N. Test Program after Removal/Installation of Panel 40VU
(1) Do the operational test of the wing-tank fuel control (Ref. AMM TASK 28-21-00-710-001).
(2) Do the operational test of the crossfeed valve using individual motors (Ref. AMM TASK 28-23-00-720-001).
(3) Do the operational test of the main transfer system (Ref. AMM TASK 28-26-00-710-001).
(4) Do the operational test of the ACT manual transfer system (if installed) (Ref. AMM TASK 28-28-00-710-001).
(5) Do the functional test of hydraulic fire shut-off valves 1046GK and 3046GD (Ref. AMM TASK 29-10-00-720-001).
(6) Do the operational test of the manual deployment and the retraction of the RAT (if installed) (Ref. AMM TASK 29-22-00-710-007).

Subtask 31-10-00-710-094-A

O. Test Program after Removal/Installation of Panel 41VU
(1) Do the interface test of the IR (Ref. AMM TASK 34-14-00-740-001).
(2) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
(3) Do the operational test of the lights (Ref. AMM TASK 33-14-00-710-001).

Subtask 31-10-00-710-090-A

P. Test Program after Removal/Installation of Panel 45VU
(1) Do the operational test of the CDLS (Ref. AMM TASK 52-51-00-710-002).

Subtask 31-10-00-710-064-A

Q. Test Program after Removal/Installation of Panel 48VU
(1) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).

Subtask 31-10-00-710-065-D ** ON A/C NOT FOR ALL

R. Test Program after the Removal/Installation of Panel 50VU
(1) Do the operational test of the service interphone (Ref. AMM TASK 23-44-00-700-001).
(2) Do the operational test of the CVR and the CVR channel recording (Ref. AMM TASK 23-71-00-710-001).
(3) Do the functional test of the bulk-erase function and bulk-erase inhibition-logic of the CVR (Ref. AMM TASK 23-71-00-720-002).
(4) Do the operational test of the APU fire-extinguishing loop/squib (Ref. AMM TASK 26-22-00-710-001).
(5) To do the functional check of the Blue electrical-pump pressure, read the ECAM indication (Ref. AMM TASK 29-12-00-710-001).
(6) Do the operational test of the HYD/LEAK MEASUREMENT VALVES pushbutton switches:
(a) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(b) Pressurize the hydraulic reservoirs with the ground connector (Ref. AMM TASK 29-14-00-614-002).
(c) Pressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-863-001) or (Ref. AMM TASK 29-23-00-863-001).
(d) Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
(e) Pressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-863-002).
(f) Do the EIS start procedure (upper and lower ECAM DUs only) (Ref. AMM TASK 31-60-00-860-001).
(g) Do this test:

ACTION	RESULT
1.On the ECAM control panel, on the center pedestal: Push the HYD pushbutton switch.	On the lower ECAM DU: The HYD page comes into view.
2.On overhead panel 50VU: Lift the guard and release the HYD/LEAK MEASUREMENT VALVE/G pushbutton switch (the OFF legend comes on).	In less than 15 seconds, on the lower ECAM DU: The color of the system name and of the system arrow becomes amber.
3.On overhead panel 50VU: Lift the guard and push the HYD/LEAK MEASUREMENT VALVE/G pushbutton switch (the OFF legend goes off). When you push the HYD/LEAK MEASUREMENT VALVE/G pushbutton switch, it is possible that the HYD page goes out of view and the ELEC page comes into view. You can also hear the single chime and, on the CAPT and F/O glareshield panels, the MASTER CAUT lights come on. Push, then release the MASTER CAUT lights (the lights go off) and get the HYD page to find the hydraulic indications.	On the lower ECAM DU: The color of the system name becomes white. The color of the system arrow becomes green.
4.On overhead panel 50VU: Lift the guard and release the HYD/LEAK MEASUREMENT VALVE/B pushbutton switch (the OFF legend comes on).	In less than 15 seconds, on the lower ECAM DU: The color of the system name and of the system arrow becomes amber.
5.On overhead panel 50VU: Lift the guard and push the HYD/LEAK MEASUREMENT VALVE/B pushbutton switch (the OFF legend goes off).	On the lower ECAM DU: The color of the system name becomes white. The color of the system arrow becomes green.
6.On overhead panel 50VU: Lift the guard and release the HYD/LEAK MEASUREMENT VALVE/Y pushbutton switch (the OFF legend comes on).	In less than 15 seconds, on the lower ECAM DU: The color of the system name and of the system arrow becomes amber.
7.On overhead panel 50VU: Lift the guard and push the HYD/LEAK MEASUREMENT VALVE/Y pushbutton switch (the OFF legend goes off).	On the lower ECAM DU: The color of the system name becomes white. The color of the system arrow becomes green.

(h) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001) or (Ref. AMM TASK 29-23-00-864-001).
(i) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
(j) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002).
(k) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(l) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(7) Do the functional test of the avionics compartment lighting (Ref. AMM TASK 33-35-00-720-001).
(8) Do the operational check of the manual mask release (Ref. AMM TASK 35-23-00-710-001).
(9) Do the operational test of the EEC (Ref. AMM TASK 73-22-34-710-040).

Subtask 31-10-00-710-065-G ** ON A/C NOT FOR ALL

ACTION	RESULT
1.On the ECAM control panel, on the center pedestal: Push the HYD pushbutton switch.	On the lower ECAM DU: The HYD page comes into view.
2.On overhead panel 50VU: Lift the guard and release the HYD/LEAK MEASUREMENT VALVE/G pushbutton switch (the OFF legend comes on).	In less than 15 seconds, on the lower ECAM DU: The color of the system name and of the system arrow becomes amber.
3.On overhead panel 50VU: Lift the guard and push the HYD/LEAK MEASUREMENT VALVE/G pushbutton switch (the OFF legend goes off). When you push the HYD/LEAK MEASUREMENT VALVE/G pushbutton switch, it is possible that the HYD page goes out of view and the ELEC page comes into view. You can also hear the single chime and, on the CAPT and F/O glareshield panels, the MASTER CAUT lights come on. Push, then release the MASTER CAUT lights (the lights go off) and get the HYD page to find the hydraulic indications.	On the lower ECAM DU: The color of the system name becomes white. The color of the system arrow becomes green.
4.On overhead panel 50VU: Lift the guard and release the HYD/LEAK MEASUREMENT VALVE/B pushbutton switch (the OFF legend comes on).	In less than 15 seconds, on the lower ECAM DU: The color of the system name and of the system arrow becomes amber.
5.On overhead panel 50VU: Lift the guard and push the HYD/LEAK MEASUREMENT VALVE/B pushbutton switch (the OFF legend goes off).	On the lower ECAM DU: The color of the system name becomes white. The color of the system arrow becomes green.
6.On overhead panel 50VU: Lift the guard and release the HYD/LEAK MEASUREMENT VALVE/Y pushbutton switch (the OFF legend comes on).	In less than 15 seconds, on the lower ECAM DU: The color of the system name and of the system arrow becomes amber.
7.On overhead panel 50VU: Lift the guard and push the HYD/LEAK MEASUREMENT VALVE/Y pushbutton switch (the OFF legend goes off).	On the lower ECAM DU: The color of the system name becomes white. The color of the system arrow becomes green.

(h) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001) or (Ref. AMM TASK 29-23-00-864-001).
(i) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
(j) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002).
(k) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(l) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(7) Do the functional test of the avionics compartment lighting (Ref. AMM TASK 33-35-00-720-001).
(8) Do the operational check of the manual mask release (Ref. AMM TASK 35-23-00-710-001).
(9) Do the functional test of the ECU (Ref. AMM TASK 73-21-60-720-040).

Subtask 31-10-00-710-065-J ** ON A/C NOT FOR ALL

ACTION	RESULT
1.On the ECAM control panel, on the center pedestal: Push the HYD pushbutton switch.	On the lower ECAM DU: The HYD page comes into view.
2.On overhead panel 50VU: Lift the guard and release the HYD/LEAK MEASUREMENT VALVE/G pushbutton switch (the OFF legend comes on).	In less than 15 seconds, on the lower ECAM DU: The color of the system name and of the system arrow becomes amber.
3.On overhead panel 50VU: Lift the guard and push the HYD/LEAK MEASUREMENT VALVE/G pushbutton switch (the OFF legend goes off). When you push the HYD/LEAK MEASUREMENT VALVE/G pushbutton switch, it is possible that the HYD page goes out of view and the ELEC page comes into view. You can also hear the single chime and, on the CAPT and F/O glareshield panels, the MASTER CAUT lights come on. Push, then release the MASTER CAUT lights (the lights go off) and get the HYD page to find the hydraulic indications.	On the lower ECAM DU: The color of the system name becomes white. The color of the system arrow becomes green.
4.On overhead panel 50VU: Lift the guard and release the HYD/LEAK MEASUREMENT VALVE/B pushbutton switch (the OFF legend comes on).	In less than 15 seconds, on the lower ECAM DU: The color of the system name and of the system arrow becomes amber.
5.On overhead panel 50VU: Lift the guard and push the HYD/LEAK MEASUREMENT VALVE/B pushbutton switch (the OFF legend goes off).	On the lower ECAM DU: The color of the system name becomes white. The color of the system arrow becomes green.
6.On overhead panel 50VU: Lift the guard and release the HYD/LEAK MEASUREMENT VALVE/Y pushbutton switch (the OFF legend comes on).	In less than 15 seconds, on the lower ECAM DU: The color of the system name and of the system arrow becomes amber.
7.On overhead panel 50VU: Lift the guard and push the HYD/LEAK MEASUREMENT VALVE/Y pushbutton switch (the OFF legend goes off).	On the lower ECAM DU: The color of the system name becomes white. The color of the system arrow becomes green.

(h) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001) or (Ref. AMM TASK 29-23-00-864-001).
(i) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
(j) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002).
(k) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(l) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(7) Do the functional test of the avionics compartment lighting (Ref. AMM TASK 33-35-00-720-001).
(8) Do the operational check of the manual mask release (Ref. AMM TASK 35-23-00-710-001).
(9) Do the EEC operation test (self-test) (Ref. AMM TASK 73-21-00-710-806).

Subtask 31-10-00-710-066-A

S. Test Program after Removal/Installation of Panel 51VU

(1) Do the operational test of the refuel system (Ref. AMM TASK 28-25-00-710-003).

Subtask 31-10-00-710-067-A

T. Test Program after Removal/Installation of Panel 52VU
(1) Do the uploading of the FM data (Ref. AMM TASK 22-70-00-610-008).
(2) Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001).

Subtask 31-10-00-710-068-A

U. Test Program after Removal/Installation of Panel 54VU

The preliminary tests are sufficient (ref. Para. 4.A.).

Subtask 31-10-00-710-069-A

V. Test Program after Removal/Installation of Panel 55VU

The preliminary tests are sufficient (ref. Para. 4.A.).

Subtask 31-10-00-710-070-A

W. Test Program after Removal/Installation of Panel 56VU
(1) Do the operational test of the landscape camera (if installed) (Ref. AMM D/O 23-36-00-71).

Subtask 31-10-00-710-071-A

X. Test Program after Removal/Installation of Panel 60VU
(1) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).

Subtask 31-10-00-710-072-A

Y. Test Program after Removal/Installation of Panel 61VU
(1) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).

Subtask 31-10-00-710-073-A

Z. Test Program after Removal/Installation of Panel 62VU
(1) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).

Subtask 31-10-00-710-074-A

AA. Test Program after Removal/Installation of Panel 63VU
(1) Do the operational test of the service interphone (Ref. AMM TASK 23-44-00-700-001).
(2) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).

Subtask 31-10-00-710-075-A

AB. Test Program after Removal/Installation of Panel 64VU
(1) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).

Subtask 31-10-00-710-076-A

AC. Test Program after Removal/Installation of Panel 108VU
(1) Do the operational test of the mechanic call (Ref. AMM TASK 23-42-00-710-001).
(2) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).
(3) Do the BITE test of the ELT system (if installed) (Ref. AMM TASK 25-65-00-740-001).
(4) Do the operational test of the lights (Ref. AMM TASK 33-14-00-710-001).
(5) Do the operational test of the emergency shutdown system (using the APU SHUT OFF switch 1KL) (GTCP 36-300) (Ref. AMM D/O 49-62-00-71).
(6) Do the operational test of the emergency shutdown circuit (using the APU Shut Off switch 1KL) (APS 3200) (Ref. AMM TASK 49-62-00-710-004).
(7) Do the operational test of the emergency shutdown system (using the APU SHUT OFF switch 1KL) (131-9(A)) (Ref. AMM TASK 49-62-00-710-007).

Subtask 31-10-00-710-077-A

AD. Test Program after Removal/Installation of Panel 110VU
(1) Do the operational test of the reset function (Ref. AMM TASK 27-22-00-710-001).
(2) Do the operational test of the parking brake system (Ref. AMM TASK 32-45-00-710-001).

Subtask 31-10-00-710-078-A

AE. Test Program after Removal/Installation of Panel 111VU
(1) Do the operational test of the general illumination (Ref. AMM TASK 33-12-00-710-001).
(2) Do the operational test of the electrical release strike (Ref. AMM TASK 52-51-12-400-001) Para. 4.D.

Subtask 31-10-00-710-079-A

AF. Test Program after Removal/Installation of Panel 112VU
(1) Do the operational test of the general illumination (Ref. AMM TASK 33-12-00-710-001).

Subtask 31-10-00-710-080-A

AG. Test Program after Removal/Installation of Panel 114VU
(1) Do the operational test of the WTB and the POB (Ref. AMM TASK 27-51-00-710-001).
(2) Do the operational test of the flap system (Ref. AMM TASK 27-54-00-710-001).

Subtask 31-10-00-710-081-A ** ON A/C NOT FOR ALL

AH. Test Program after Removal/Installation of Panel 115VU
(1) Do the operational check of the loop/squib (Ref. AMM TASK 26-12-00-710-001).
(2) Do the functional test of the ECU (Ref. AMM TASK 73-21-60-720-040).

Subtask 31-10-00-710-081-B ** ON A/C NOT FOR ALL

AH. Test Program after Removal/Installation of Panel 115VU
(1) Do the operational Check of the loop/squib (Ref. AMM TASK 26-12-00-710-001).
(2) Do the operational test of the EEC (Ref. AMM TASK 73-22-34-710-040).

Subtask 31-10-00-710-081-E ** ON A/C NOT FOR ALL

AH. Test Program after Removal/Installation of Panel 115VU
(1) Do the operational Check Of the loop/squib (Ref. AMM TASK 26-12-00-710-001).
(2) Do the Engine EEC operation test (self-test) (Ref. AMM TASK 73-21-00-710-806).

Subtask 31-10-00-710-082-A

AI. Test Program after Removal/Installation of Panel 117VU

(1) Do the uploading of the maintenance filter data-base to the CFDIU with the PDL (Ref. AMM TASK 31-32-00-600-001).

Subtask 31-10-00-710-089-A

AJ. Test Program after Removal/Installation of Panel 119VU
(1) Do the operational test of the CDLS (Ref. AMM TASK 52-51-00-710-002).

Subtask 31-10-00-710-083-A

AK. Test Program after Removal/Installation of Panel 130VU
(1) Do the operational test of the general illumination (Ref. AMM TASK 33-12-00-710-001).
(2) Do the operational test of the LAND CAT III capability (Ref. AMM TASK 22-97-00-710-001).
(3) Do the operational test of the audio management (if the RADIO PTT pushbutton switch is installed) (Ref. AMM TASK 23-51-00-710-001).
(4) Do the operational test of the side stick priority (Ref. AMM TASK 27-96-00-710-003).
(5) Do the operational test of the FWC (Ref. AMM TASK 31-50-00-710-002).
(6) Do the operational test of the SDAC (Ref. AMM TASK 31-50-00-710-003).

Subtask 31-10-00-710-084-A

AL. Test Program after Removal/Installation of Panel 131VU
(1) Do the operational test of the general illumination (Ref. AMM TASK 33-12-00-710-001).
(2) Do the operational test of the LAND CAT III capability (Ref. AMM TASK 22-97-00-710-001).
(3) Do the operational test of the audio management (if the RADIO PTT pushbutton switch installed) (Ref. AMM TASK 23-51-00-710-001).
(4) Do the operational test of the side stick priority (Ref. AMM TASK 27-96-00-710-003).
(5) Do the operational test of the FWC (Ref. AMM TASK 31-50-00-710-002).
(6) Do the operational test of the SDAC (Ref. AMM TASK 31-50-00-710-003).
(7) Do the operational test of the HUD (if installed) (Ref. AMM D/O 34-35-00-71).

Subtask 31-10-00-710-085-A ** ON A/C NOT FOR ALL

AM. Test Program after Removal/Installation of Panel 301VU
(1) Do the operational test of the general illumination (Ref. AMM TASK 33-12-00-710-001).
(2) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).
(3) Do the operational test of the EFIS/ECAM switching functions (Ref. AMM TASK 31-60-00-710-002).
(4) Do the brightness test of the PFD/ND/upper and lower ECAM DU (Ref. AMM TASK 31-60-00-710-003).
(5) Do the operational test of the angle of attack warning (Ref. AMM TASK 34-10-00-710-007).
(6) Do the operational test of the (enhanced, if applicable) GPWS ground self-test function (if available) (Ref. AMM TASK 34-48-00-710-001) or do the BITE test of the T/TISS (TAWS part) (if available) (Ref. AMM D/O 34-72-00-74).
(7) Do the operational test of the back-up speed and altitude scales (if installed) (Ref. AMM D/O 34-13-00-71).

Subtask 31-10-00-710-085-B ** ON A/C NOT FOR ALL

AM. Test Program after Removal/Installation of Panel 301VU
(1) Do the operational test of the general illumination (Ref. AMM TASK 33-12-00-710-001).
(2) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).
(3) Do the brightness test of the PFD/ND/upper and lower ECAM DU (Ref. AMM TASK 31-60-00-710-003).
(4) Do the operational test of the angle of attack warning (Ref. AMM TASK 34-10-00-710-007).
(5) Do the operational test of the enhanced GPWS ground self-test function (if available) (Ref. AMM TASK 34-48-00-710-001) or do the BITE test of the T/TISS (TAWS part) (if available) (Ref. AMM TASK 34-72-00-740-001).
(6) Do the operational test of the back-up speed and altitude scales (if installed) (Ref. AMM TASK 34-13-00-710-009).

Subtask 31-10-00-710-086-A

AN. Test Program after Removal/Installation of Panel 402VU

CAUTION: DO NOT CONTINUE THE TEST FOR MORE THAN ONE MINUTE TO PREVENT DAMAGE TO THE PROBES.

(1) Landing gear indication test

ACTION	RESULT
1.On MCDU 1(2): Adjust the brightness of the MCDU screen.	MCDU 1(2) is on.
2.On MCDU 1(2): Push MCDU MENU mode key.	On MCDU 1(2): The MCDU MENU page comes into view.
3.On MCDU 1(2): Push the line key adjacent to the CFDS indication.	On MCDU 1(2): The CFDS MENU page comes into view.
4.On MCDU 1(2): Push the line key adjacent to the SYSTEM REPORT/TEST indication.	On MCDU 1(2): The SYSTEM REPORT/TEST page comes into view.
5.Push the line key adjacent to the L/G indication	On MCDU 1(2): The SYSTEM REPORT TEST L/G page comes into view.
6.Push the line key adjacent to the LGCIU1 indication.	The LGCIU1 page comes into view.
7.Push the NEXT PAGE key.	The LGCIU1 page comes into view.
8.Push the line key adjacent to the LANDING GEAR SIMULATION indication.	On MCDU 1(2): The LGCIU1 LANDING GEAR SIMULATION page comes into view.
9.Push the line key adjacent to the NOSE + LH + RH indication.	On MCDU 1(2): The LGCIU1 NOSE + LH + RH page comes into view.
10.Push the line key adjacent to the UP LOCKED indication	On MCDU 1(2): The LGCIU1 NOSE + LH + RH page comes into view.
	On panel 402VU: The three UNLK legends come on (red) The three downlock symbols go off
11.Push the line key adjacent to the DOWN LOCKED indication.	On MCDU 1(2): The LGCIU1 NOSE + LH + RH page comes into view.
	On panel 402VU: The three UNLK legends go off The three downlock symbols come on (green).
12.Push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.

(2) Do the operational test of the antiskid inhibition (Ref. AMM TASK 32-42-00-710-003).
(3) Do the operational test of the autobrake-deceleration rate arming (Ref. AMM TASK 32-42-00-710-005).
(4) Do the operational test of the (enhanced, if applicable) GPWS ground self-test function (if available) (Ref. AMM TASK 34-48-00-710-001) or do the BITE test of the T/TISS (TAWS part) (if available) (Ref. AMM TASK 34-72-00-740-001).

Subtask 31-10-00-710-087-A

AO. Test Program after Removal/Installation of Panel 403VU
(1) Do the operational test of the (enhanced, if applicable) GPWS ground self-test function (if available) (Ref. AMM TASK 34-48-00-710-001) or do the BITE test of the T/TISS (TAWS part) (if available) (Ref. AMM TASK 34-72-00-740-001).

Subtask 31-10-00-710-088-A ** ON A/C NOT FOR ALL

AP. Test Program after Removal/Installation of Panel 500VU
(1) Do the operational test of the general illumination (Ref. AMM TASK 33-12-00-710-001).
(2) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).
(3) Do the operational test of the EFIS/ECAM switching functions (Ref. AMM TASK 31-60-00-710-002).
(4) Do the brightness test of the PFD/ND/upper and lower ECAM DU (Ref. AMM TASK 31-60-00-710-003).
(5) Do the operational test of the angle of attack warning (Ref. AMM TASK 34-10-00-710-007).
(6) Do the operational test of the (enhanced, if applicable) GPWS ground self-test function (if available) (Ref. AMM TASK 34-48-00-710-001) or do the BITE test of the T/TISS (TAWS part) (if available) (Ref. AMM D/O 34-72-00-74).
(7) Do the operational test of the back-up speed and altitude scales (if installed) (Ref. AMM D/O 34-13-00-71).

Subtask 31-10-00-710-088-B ** ON A/C NOT FOR ALL

AP. Test Program after Removal/Installation of Panel 500VU
(1) Do the operational test of the general illumination (Ref. AMM TASK 33-12-00-710-001).
(2) Do the operational test of the audio management (Ref. AMM TASK 23-51-00-710-001).
(3) Do the operational check of correct operation of EFIS and ECAM DMC automatic and manual transfer (Ref. AMM TASK 31-60-00-710-005).
(4) Do the brightness test of the PFD/ND/upper and lower ECAM DU (Ref. AMM TASK 31-60-00-710-003).
(5) Do the operational test of the angle of attack warning (Ref. AMM TASK 34-10-00-710-007).
(6) Do the operational test of the enhanced GPWS ground self-test function (if available) (Ref. AMM TASK 34-48-00-710-001) or do the BITE test of the T/TISS (TAWS part) (if available) (Ref. AMM TASK 34-72-00-740-001).
(7) Do the operational test of the back-up speed and altitude scales (if installed) (Ref. AMM TASK 34-13-00-710-009).

Subtask 31-10-00-710-092-A

AQ. Test Program after Removal/Installation of Panel 619VU
(1) Do the operational test of the cabin/cockpit incident alert system (cockpit part) (if installed) (Ref. AMM TASK 23-73-00-710-040).

Subtask 31-10-00-710-093-A

AR. Test Program after Removal/Installation of Panel 620VU
(1) Do the operational test of the cabin/cockpit incident alert system (cockpit part) (if installed) (Ref. AMM TASK 23-73-00-710-040).

[Rev.10 from 2021] 2026.04.01 00:33:13 UTC