_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
CAUTION : DO NOT REFUEL OR DEFUEL THROUGH THE TWO REFUEL/DEFUEL COUPLINGS AT
_______
THE SAME TIME.
THIS IS TO PREVENT PRESSURE DIFFERENCE PROBLEMS.
1. Reason for the Job
__________________
R R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform
No specific safety barriers
1EFF : ALL 1 28-00-00Page 407 1 1 Aug 01/04 1 1 1CES 1 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. 04-012 USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (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)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control
R 20-28-00-912-006 Electrical Bonding of Pipes 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 28-25-00-650-001 Pressure Defuel 28-25-00-650-003 To Drain Remaining Fuel from the Wing Tanks and the
Center Tank 28-25-00-710-002 Operational Test of the Defuel System 28-25-00-710-003 Operational Test of the Refuel System 28-25-00-869-001 Fuel Transfer 57-17-11-000-001 Removal of the Covers 147AZ (148AZ) 57-17-11-400-001 Installation of the Covers 147AZ (148AZ) 57-27-11-000-001 Removal of the Access Panel (540AB, 540BB, 540CB,
540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)
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, ....)
57-27-11-400-001 Installation of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)
1EFF : ALL 1 28-00-00Page 408 1 1 Aug 01/04 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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, ....)
57-31-21-000-001 Removal of the Wing-Tip Structure 57-31-21-400-001 Installation of the Wing-Tip Structure FPRM Check (for corrective action) FPRM Description (for corrective action) 28-00-00-991-001 Fig. 401
3. Job Set-up
__________
(Ref. Fig. 401/TASK 28-00-00-991-001)
Subtask 28-00-00-941-055
A. Safety Precautions
WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
(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.
Subtask 28-00-00-860-052
B. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is below the applicable access panel.
(2)
Make sure that the applicable fuel tank is defueled (Ref. TASK 28-25-00-650-001).
(3)
Make sure that the remaining fuel has been drained from the applicable fuel tank (Ref. TASK 28-25-00-650-003).
(4)
Get access to the applicable fuel tanks and work areas (Ref. TASK 28-10-00-910-002).
(a) For the LH and RH wing (Ref. TASK 57-27-11-000-001), (Ref. TASK 57-27-11-000-002).
1EFF : ALL 1 28-00-00Page 409 1 1 Feb 01/00R 1 1 1CES 1
R R (b) If applicable, make sure that the wing tip has been removed (Ref. TASK 57-31-21-000-001).
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