(4)
 Make sure that the AFT CARGO COMPT light switch 8LU is set to the ON position.

R (5) FOR 7504MM
 -Make sure that the access panel 151KW is removed.
R (6) FOR 7505MM
 -Make sure that the access panel 152KW is removed.
 (7) Make sure that the applicable inflation reservoir (2) is installed (Ref. TASK 25-62-46-400-001) and safetied:
 WARNING : MAKE SURE THAT THE SAFETY/LOCK PIN IS CORRECTLY INSTALLED
_______ IN THE REGULATOR VALVE ASSEMBLY OF THE INFLATION RESERVOIR. THIS PREVENTS ACCIDENTAL:
 -DISCHARGE OF THE INFLATION RESERVOIR
 -DEPLOYMENT OF THE ESCAPE-SLIDE WHICH CAN CAUSE INJURY AND/OR DAMAGE.
 (a) Make sure that the lockpin assembly (4) is installed in the valve/regulator assembly (3).
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 CES

 (8) If the inflation reservoir (2) is removed, make sure that the pressure seal cap (5) is installed:
 WARNING : MAKE SURE THAT YOU INSTALL THE PRESSURE SEAL CAPS ON THE
_______ DISCONNECTED LINE ENDS. THE ESCAPE-SLIDE CAN DEPLOY IF THE AIRCRAFT IS PRESSURIZED AND THE PRESSURE SEAL CAPS ARE NOT INSTALLED. UNWANTED DEPLOYMENT OF THE ESCAPE-SLIDE CAN CAUSE INJURY AND/OR DAMAGE.
 (a) Make sure that the pressure seal cap (5) is installed on the bulkhead union (6).
 (9) Make sure that in the cockpit:
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______ BEFORE YOU START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 (a)
 The flap/slat control lever is set to the 0 position (Ref. TASK 27-50-00-866-009).

 (b)
 The LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever.

 (c)
 A WARNING NOTICE is in position on the flap/slat control lever to tell persons not to operate the flaps.

R (10) FOR 7504MM
 (a) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position adjacent to the panel 193AT.
R (11) FOR 7505MM
 (a) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position adjacent to the panel 194AT.
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 CES  4. Procedure

_________ Subtask 25-62-42-210-055
 A. Detailed Visual Inspection before Installtion
 (Ref. Fig. 402/TASK 25-62-42-991-005)

 (1)
 Do a detailed visual inspection of the enclosure door (8) and the ball locking mechanisms (13).

 (2)
 Make sure:

 -the enclosure door (8) has a flush surface with the outside surface of its escape slide enclosure (7).
 -that all 3 ball lock pins (18) are flush with the outside surface of each ball lock mechanism (13).
 -Make sure that the slide enclosure ball locks are clean and free of paint.
 NOTE : If the enclosure door (8) and the ball lockpins (18) are not
____ in the correct position, you must replace the escape slide enclosure (7).
 Subtask 25-62-42-420-052
 B. Installation of the Escape Slide Enclosure
 (Ref. Fig. 402/TASK 25-62-42-991-005)

 (1)
 Put the escape slide enclosure (7) in position.

 (2)
 Move the top of the escape slide enclosure (7) outboard at an angle and hold it.

 (3)
 Remove the blanking plugs from the disconnected line ends.

 (4)
 Connect the inflation hose (16) to the fuselage union (15), and TORQUE to between 3.0 and 3.2 m.daN (22.12 and 23.59 lbf.ft).

 (5)
 Remove the blanking caps from the electrical connectors.

 (6)
 Connect the emergency lighting electrical connector (14).

 (7)
 Close the escape slide enclosure (7) and tighten the studs (17).

 (8)
 Put the seal strips (9) and the seal attach plate (12) in position, and install the countersunk washers (11) and the screws (10).

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 CES  Subtask 25-62-42-710-050

 C. Do the operational test of the emergency lighting system (Ref. TASK 33-51-00-710-001).
 5. Close-up
________
 Subtask 25-62-42-410-051

 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 In the cockpit:

 (a)
 Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) from the flap/slat control lever.
　
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