Operational Check of the ACT Manual Transfer System (AFT Cargo-Compartment)

TASK 28-28-00-710-008-A
Operational Check of the ACT Manual Transfer System (AFT Cargo-Compartment)

WARNING: OBEY THE FUEL SAFETY PROCEDURES.

1. Reason for the Job

NOTE: This procedure is only applicable if the aircraft is equipped with Additional Center Tank (ACT) in the aft cargo-compartment.

2. Job Set-up Information
A. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
192MB

B. 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 28-00-00-910-001-A	Fuel Safety Procedures
TASK 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure
TASK 32-12-00-010-001-A	Open the Main Gear Doors for Access
TASK 32-12-00-410-001-A	Close the Main Gear Doors after Access

3. Job Set-up
Subtask 28-28-00-860-100-B ** ON A/C NOT FOR ALL

A. Aircraft Maintenance Configuration
(1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
(2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(4) On the ECAM control panel push the FUEL pushbutton switch, on the lower ECAM DU the FUEL page comes into view.
(a) On the lower ECAM DU, make sure that the fuel quantity in ACT AFT1, ACT AFT2, and ACT FWD is 400 +50 kg or -150 kg (881.8488 +110.2311 lb or -330.6933 lb) in each ACT.
(b) On the lower ECAM DU, make sure that the fuel quantity in the RH and LH wing tanks is approximately 5000 +100 kg or -100 kg (11023.1100 +220.4622 lb or -220.4622 lb).
(c) On the lower ECAM DU, make sure that the fuel quantity in the center tank is approximately 250 kg (551.1555 lb).

NOTE: The 5000 kg fuel in the RH and LH wing tanks are used for ballast purposes. The weight of fuel in the wing tanks reduce the risk of a larger change on the longitudinal center of gravity, which can be caused by the higher load of fuel in the ACT(s), installed in the cargo compartment.

(5) Open the main gear doors for access (Ref. AMM TASK 32-12-00-010-001).
(6) Open refuel/defuel control panel door 192MB.

Subtask 28-28-00-865-077-A ** ON A/C NOT FOR ALL

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

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	ALSCU SPLY	66QJ	B10
121VU	FUEL/ACT XFR VLV/MOT2	66QH	J18
121VU	FUEL/ACT XFR VLV/MOT1	65QH	J17
121VU	FUEL/ALSCU/HI LEVEL/SPLY	64QJ	K21
121VU	FUEL/ALSCU/SPLY	65QJ	K20
121VU	FUEL/HI/LVL/SPLY	1QJ	L24
121VU	FUEL/ACT/FUEL PUMP/SPLY	25QH	Q29

4. Procedure
Subtask 28-28-00-710-061-B ** ON A/C NOT FOR ALL

A. Operational Test of the ACT Fuel Manual Transfer

ACTION	RESULT
1.On overhead FUEL ACT panel 28VU: Push the ACT XFR MODE SEL pushbutton switch.	On the overhead FUEL ACT panel 28VU: MAN legend in the ACT XFR MODE SEL pushbutton switch comes on.
2.On overhead FUEL ACT panel 28VU: Put the ACT XFR rotary switch to AFT1.	On the lower ECAM DU: The arrow symbol comes on green The fuel quantity of ACT AFT1 decreases.
	In the compartment of the main landing gear at FR 42 (Left port center tank access door): Make sure that the ACT fuel-transfer pump operates The position indicator of the ACT fuel-transfer-valve actuator shows the open position (in-line).
3.On overhead FUEL ACT panel 28VU: Put the ACT XFR rotary switch to AFT2.	On the lower ECAM DU: The arrow symbol comes on green The fuel quantity of ACT AFT2 decreases.
	In the compartment of the main landing gear at FR 42 (Left port center tank access door): Make sure that the ACT fuel-transfer pump operates The position indicator of the ACT fuel-transfer-valve actuator shows the open position (in-line).
4.On overhead FUEL ACT panel 28VU: Put the ACT XFR rotary switch to FWD.	On the lower ECAM DU: The arrow symbol comes on green The fuel quantity of ACT FWD decreases.
	In the compartment of the main landing gear at FR 42 (Left port center tank access door): Make sure that the ACT fuel-transfer pump operates The position indicator of the ACT fuel-transfer-valve actuator shows the open position (in-line).
5.On overhead FUEL ACT panel 28VU: Put the ACT XFR rotary switch to OFF Release the ACT XFR MODE SEL pushbutton switch.	On the overhead FUEL ACT panel 28VU: MAN legend in the ACT XFR MODE SEL pushbutton switch goes off.
	On the lower ECAM DU: The fuel transfer from the ACT to the center tank stops, The arrow symbol disappears.
	In the compartment of the main landing gear at FR 42 (Left port center tank access door): Make sure that the ACT fuel-transfer pump is stopped.

5. Close-up
Subtask 28-28-00-860-101-A ** ON A/C NOT FOR ALL

A. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(4) Close refuel/defuel control panel door 192MB.
(5) Close the MLG doors (Ref. AMM TASK 32-12-00-410-001).
(6) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.02 07:01:53 UTC