A320飞机维护手册 AMM FUEL 燃油1(104)

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Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00) Material No. 19-004
 WHITE TALCUM POWDER (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003  Pressure Refuel with Automatic Control
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
 27-50-00-866-008  Extension of the Flaps on the Ground
 27-50-00-866-009  Retraction of the Flaps on the Ground
 27-60-00-866-002  Extension-Retraction of the Spoilers for Maintenance
 28-10-00-910-001  Safety Procedures When You Do Work in a Fuel Tank
 28-10-00-910-002  Access to the Fuel Tanks and the Work Areas
 28-12-47-000-001  Removal of the NACA Vent Intake
 28-12-47-400-001  Installation of the NACA Vent Intake
 28-25-00-650-001  Pressure Defuel
 28-25-00-650-003  To Drain Remaining Fuel from the Wing Tanks and the
 Center Tank
 28-25-00-869-001  Fuel Transfer
 31-60-00-860-001  EIS Start Procedure
 31-60-00-860-002  EIS Stop Procedure
 57-27-11-000-002  Removal of the Access Panel (540HB, 540JB, 540KB,
 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB,
 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB,
 ....)
 57-27-11-400-002  Installation of the Access Panel (540HB, 540JB,
 540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB,
 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB,
 ....)
 57-51-37-000-004  Removal of the Access Panels
 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB
 (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
 57-51-37-400-004  Installation of the Access Panels
 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB
 (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB) 

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28-11-00-991-010 Fig. 501
 3. Job Set-up
__________ Subtask 28-11-00-941-078
 A. Safety Precautions WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
 (1)
 You must obey the fuel safety procedures when you do work in a fuel tank (Ref. TASK 28-10-00-910-001).

 (2)
 Put a warning notice in the cockpit to tell persons not to operate the flight controls.

 (3) Put the safety barriers in position. Subtask 28-11-00-860-059
 B. Aircraft Maintenance Configuration
 (Ref. Fig. 501/TASK 28-11-00-991-010)

 (1)
 Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001).

 (2)
 On the ECAM control panel, push in the FUEL pushbutton switch (P/BSW).

 (3)
 Refuel the outer cell to full (Ref. TASK 12-11-28-650-003).

 (4)
 Get access to the intercell transfer valve actuators:

 (a) Put an access platform below the applicable access panels:
 -
For the left wing, below the access panels 522KB and 575DB

 -
For the right wing, below the access panels 622KB and 675DB.

 (b) Remove the applicable access panels:
 -522KB(622KB)
 -575DB(675DB) (Ref. TASK 57-51-37-000-004).

 (5)
 On the intercell transfer valve actuator, make sure that the valve position indicator shows valve closed.

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 Intercell-Transfer-Valve Actuators - Location and Detail
 Figure 501/TASK 28-11-00-991-010

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 (6)
 Remove the electrical connector (1) from the intercell-transfer-valve actuator (2)

 (7)
 Defuel or transfer fuel from the applicable wing tank inner cell (Ref. TASK 28-25-00-650-001).

 NOTE : This will leave the outer cell full.
____
 (8)
 On the intercell transfer valve actuator, make sure that the valve position indicator shows valve closed.

 (9)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

　
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