(2)
Make sure that the access covers are removed (Ref. TASK 57-17-11-000-001).
(3)
Make sure that the applicable inner wing tank is defueled (Ref. TASK 28-25-00-650-001) or the fuel is moved from the applicable inner wing tank (Ref. TASK 28-25-00-869-001).
4. Procedure
_________ Subtask 57-17-11-914-050
A. Preparation for the Installation of the Access Door at RIB1
(1)
Clean the contact surface of the seal (12) on the access door (11) with a CLEANING AGENTS (Material No. 11-003) and a lint free cloth.
(2)
Apply SEALANTS (Material No. 09-026) on the seal (12), on the face in contact with the door (11).
(3)
Put a new seal (12) on the frame of the door (13).
(4)
Clean the surface around the door (13) with CLEANING AGENTS (Material No. 11-003) to remove the excess of the sealant.
Subtask 57-17-11-420-051
B. Installation of the Access Door at RIB1
(Ref. Fig. 402/TASK 57-17-11-991-002)
(1)
Put the access door (13) in position on the frame at RIB1. NOTE : Hold the access door (13) in position when you install the
____
fasteners.
(2)
Install the washers (17), (15) and the bolts (18), (16).
(3)
TORQUE the bolts (18), (16) to between 0.8 and 0.9 m.daN (70.79 and
79.64 lbf.in)
NOTE : When you install the bolts (18) do an electrical bonding at
____ each end of the 4 bolts (Ref. TASK 20-28-00-912-002).
(4)
Install the washers (12) and the bolt (11).
(5)
TORQUE the bolts (11) to between 1.6 and 1.8 m.daN (11.79 and 13.27 lbf.ft).
5. Close-up
________ Subtask 57-17-11-650-052
A. Pressure Refuel
(1) Do a pressure refuel of the applicable tanks (Ref. TASK 12-11-28-650-003).
Subtask 57-17-11-420-052
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the access covers 147AZ, 148AZ (Ref. TASK 57-17-11-400-001).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
OUTER WING - DESCRIPTION AND OPERATION
______________________________________
R 1. General
_______ The outer wing is a cantilever structure, attached to the center wingbox at RIB1. The main structure is the wingbox, which tapers from RIB1 to RIB27, and makes the integral fuel tank and the vent surge tank.
The outer wing is in zone 500(600).
2. Component Location
__________________
Each outer wing includes:
-
the wing box (Ref. 57-21-00)
-
the wing tip (Ref. 57-30-00)
-
the leading edge and leading edge devices (Ref. 57-40-00)
-
the trailing edge and trailing edge devices (Ref. 57-50-00).
OUTER WING - INSPECTION/CHECK_____________________________
R TASK 57-20-00-200-001
R Detailed Inspection of Outer Wing, Bottom Skin, Upper and Lower Surfaces,
R around Access Door Cutouts in Rib Bay 2-3 and Rib Bay 6-7
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU_______
R START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______
R GEAR.
R 1. Reason for the Job__________________
R Refer to the MPD TASK: 572040-01
R 2. Job Set-up Information______________________
R A. Fixtures, Tools, Test and Support Equipment
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R No specific safety barriers
R No specific warning notices
R No specific adjustable access platform 2.5 m (8 ft. 2 in.)
R 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
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