(2)
Transfer/drill all holes from the lining before you install the protection patch.
(3)
Clean the mating surfaces.
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(a) Clean the mating surfaces of the lining and the protection patch with CLEANING AGENTS (Material No. 11-010) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
(4) Apply the adhesive.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING AND RUBBER GLOVES.
(a) Apply 200 g (7.05 oz) (fluid weight) of BONDING AND ADHESIVE COMPOUNDS (Material No. 08-001) per 1 m2 (10.76 ft.2) to the mating surface of the protection patch with a SCRAPER - NON METALLIC.
(5) Install the protection patch.
WARNING : MAKE SURE THAT THE PROTECTION PATCH DOES NOT TOUCH:
_______
-
THE FASTENERS AND THE WASHERS
-
THE FLANGES AND H-PROFILES
OF THE DECOMPRESSION PANEL.
IF THE PATCH TOUCHES THESE ITEMS, IT IS POSSIBLE THAT THE
DECOMPRESSION PANEL WILL NOT OPERATE CORRECTLY.
(a)
Carefully put the protection patch in position on the view side of the lining.
(b)
Make sure that all holes are aligned and that there is a
sufficient clearance to the adjacent components (e.g.
decompression panel).
(c)
If necessary move the protection patch to the correct position.
(d)
Carefully push the protection patch onto lining with a ROLLER -RUBBER.
NOTE : Move the roller from the center to the edges to avoid or
____
remove air bubbles.
(e)
Remove the unwanted sealant with a SCRAPER - NON METALLIC.
(f)
Make sure that all interface holes and cutouts are in the correct position so that you can install the panel and/or the related equipment.
(g)
Attach the protection patch in position with BONDING AND ADHESIVE COMPOUNDS (Material No. 08-060) for 3 hours.
(h)
Remove the tape after the adhesive has cured.
5. Close-up
________ Subtask 25-00-00-420-084
A. Installation of the Lining(s) if Removed to do the Procedure
(1) Install the linings.
(a)
FWD cargo compartment:
-
(Ref. TASK 25-54-11-400-001)
-
(Ref. TASK 25-54-12-400-001)
-
(Ref. TASK 25-54-12-400-002)
-
(Ref. TASK 25-54-12-400-003)
(b)
AFT cargo compartment:
-
(Ref. TASK 25-55-11-400-001)
-
(Ref. TASK 25-55-11-400-002)
-
(Ref. TASK 25-55-11-400-003)
-
(Ref. TASK 25-55-12-400-001)
-
(Ref. TASK 25-55-12-400-002)
-(Ref. TASK 25-55-12-400-003) Subtask 25-00-00-918-051
B. Put the aircraft back to its initial configuration.
(1) If necessary install new placards to the protected linings (Ref. TASK 11-00-00-400-007) and
-FWD cargo compartment (Ref. AMM 11-35-25 P.Block 001)
-AFT cargo compartment (Ref. AMM 11-36-25 P.Block 001) Subtask 25-00-00-410-090
C. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3) Close the cargo compartment door (Ref. TASK 52-30-00-860-002). Subtask 25-00-00-862-085
D. De-energize the ground service network
(Ref. TASK 24-42-00-862-001).
R R Handrail - OHSC Figure 837/TASK 25-00-00-991-050
EFF : ALL 25-00-00 Page A887 Aug 01/05
CES
COCKPIT - DESCRIPTION AND OPERATION___________________________________
R R R R R R R 1. General Description___________________ The cockpit comprises the area above the floor structure between frames 1 and 12. Access to the cockpit is gained via the left forward passenger/crew door and the cockpit door. The cockpit is equipped with adjustable seats for two crew members, a third occupant seat and a folding seat for a fourth occupant. Various furnishings and equipment are fitted in the cockpit for the comfort, convenience and safety of the occupants.
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