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 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 1. Reason for the Job
__________________
 Self Expanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice No specific access platform 3.0 m (9 ft. 10 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 01-001 USA ASTM-D-1655-93 (JET A-1) FUEL, TURBO (Ref. 20-31-00) Material No. 04-023 USA MIL-G-27617 GREASE-FUEL AND OXIDISER RESISTANT (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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 C. Expendable Parts -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ------------------------------------ |IPC-CSN----------------------------------
2  O-rings  28-15-42 02 -020
 9  O-ring  28-15-05 01 -090
 10  O-rings  28-15-42 02 -030
 D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003  Pressure Refuel with Automatic Control
 20-28-00-912-002  Electrical Bonding of Components With Conductive
 Bolts and Screws in the Tanks
 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
 28-15-00-740-002  Functional (BITE) Test of the Intercell Transfer
 Valves
 28-15-41-400-001  Installation of the Transfer Valve 27QM (29QM), 28QM
 (30QM)
 28-15-51-400-002  Installation of the Actuator 11QP(12QP)
 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
 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,
 ....)
 28-15-42-991-001  Fig. 401 

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 3. Job Set-up
__________ (Ref. Fig. 401/TASK 28-15-42-991-001) Subtask 28-15-42-941-058
 A. Safety Precautions
 (1)
 You must obey the fuel safety procedures (Ref. TASK 28-10-00-910-001) when you do work in a fuel tank.

 (2)
 Make sure that the safety barriers are in position.

 (3)
 Make sure that the warning notice is in position to tell persons not to operate the flight controls.

 Subtask 28-15-42-865-054
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/XFR VALVE1/WING/R 2QP A11 49VU FUEL/XFR VALVE1/WING/L 1QP A10 121VU FUEL/XFR VALVE2/WING/R 4QP M23 121VU FUEL/XFR VALVE2/WING/L 3QP M22
 Subtask 28-15-42-860-051
 C. Aircraft Maintenance Configuration 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)
 Make sure that the flaps are fully extended (Ref. TASK 27-50-00-866-008) and that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the slat/flap control lever.
　
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