A320飞机维护手册 AMM FUEL 燃油2(116)

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 Subtask 28-21-00-941-067
 A. Safety PrecautionsPressure Refuel with Manual ControlEnergize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerExtending the Slats on the GroundRetracting the Slats on the GroundPressure DefuelFuel TransferEIS Start ProcedureEIS Stop ProcedureOpen the Main Gear Doors for AccessClose the Main Gear Doors after AccessRemoval of the Access Panels 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB)Installation of the Access Panels 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB)Removal of the Engine Interface Unit (EIU) (1KS1,1KS2)Installation of the Engine Interface Unit (EIU) (1KS1,1KS2)Operational Test of the Engine Interface Unit (1KS1,1KS2)
 (1)
 Put the safety barriers in position.

 (2)
 Make sure that the ground safety locks are installed on the landing gear.

 (3)
 Put a warning notice in position to tell persons not to operate the flight controls.

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 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED
_______ BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001), then:

 (a)
 On the ECAM control panel (CP), push (in) the FUEL P/BSW.

 (b)
 Make sure that the FUEL page shows on the ECAM lower display unit (DU).

 

 (3)
 Do a refuel (Ref. TASK 12-11-28-650-004) or a fuel transfer (Ref. TASK 28-25-00-869-001) to obtain these fuel levels:

 -wing tanks less than 5000 kg (11023.1100 lb)
 -the center tank more than 250 kg (551.1555 lb).
 (4) Make sure that the refuel/defuel panel door is closed. Subtask 28-21-00-010-058
 C. Get Access
 (1)
 Open the applicable access panel 522JB, 622JB (Ref. TASK 57-41-37-000-006).

 (2)
 Open the RH MLG door (Ref. TASK 32-12-00-010-001).

 (3)
 Make sure that the GROUND LOCK SLEEVE is installed on the RH MLG door actuator.

 (4)
 Put the access platform in position at the refuel valve 10QU.

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 D. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU FUEL/CTR TK/PUMP2 SPLY 30QA P26 121VU FUEL/CTR TK/PUMP1 SPLY 29QA P23 121VU FUEL/CTR TK/AUTO/CTL 47QA R27 121VU FUEL/CTR TK/PUMPS1 AND 2/CTL AND IND 32QA R26 121VU FUEL/CTR TK/PUMPS1 AND 2/CTL AND IND 31QA R25
 Subtask 28-21-00-860-074
 E. Preparation For Test
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 (1)
 Extend the slats to 16 deg. or more (Ref. TASK 27-80-00-866-004).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the slat/flap control lever.

 (3)
 On the panel 40VU, make sure that these pushbutton switches (P/BSW) are set as follows:

 -CTR TK MODE SEL released out, MAN
 -L TK PUMPS 1 & 2 released out, OFF
 -R TK PUMPS 1 & 2 released out, OFF
 -CTR TK PUMP 1 & PUMP 2 released out, OFF
 -X-FEED released out, lights off.
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 4. Procedure
_________ Subtask 28-21-00-720-050
 A. Functional Test of the Center-Tank Fuel Control (Manual Mode)
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the panel 40VU:
-make sure that the CTR TK PUMP 1 and PUMP 2 P/BSWs are in the OFF position.
 2. On the panel 121VU:
 -remove the safety clip and the tag and close the circuit breakers 29QA and 32QA.
 3. On the panel 40VU:
-push (in) the CTR TK PUMP 1 P/BSW.
4. On the panel 121VU:
　
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