-(Ref. TASK 25-00-00-340-029).
 (3) For the repair of floor panel
 (Ref. ASRM 53-02-00-208).

 Subtask 25-00-00-210-056
 B. General Procedure
 (1) Identify the damage type.
 (a) Damage to the edge(s).
 (Ref. Fig. 819/TASK 25-00-00-991-033)

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 CC Honeycomb Linings, Protection Patch - General Information
 Figure 818/TASK 25-00-00-991-048

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 CC Honeycomb Linings - Example of Edge Damage Figure 819/TASK 25-00-00-991-033
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 (b)
 Damage through the panel.
 (Ref. Fig. 820/TASK 25-00-00-991-034)

 (c)
 Damage not through the panel.
 (Ref. Fig. 821/TASK 25-00-00-991-035)

 (2)
 Measure the damaged area.

 L: Length of the damage (biggest dimension)
 W: Width of the damage
 D: Diameter of the damage

 (3)
 Select the appropriate repair method. (Ref. Fig. 822/TASK 25-00-00-991-027)

 (a)
 Do the repair within 100 flight hours if the "damage not through" has:

 -
a maximum diameter of 30 mm (1.18 in.)
 or

 -
a maximum length of 200 mm (7.87 in.) and a maximum width of 25 mm (0.98 in.).

 (b)
 Do the repair immediately if:

 -
the damage goes through the panel.

 -
the edge(s) is damaged.

 -
the dimension(s) are more than the limits for the repair within 100 flight hours.

 NOTE : Repair of dents (without cracks) in the skin of the view
____ side of the lining panel is not required, except in . If the area of the edge filler is damaged it is classified as a damage to the edge.
 (c)
 The total damaged area of a lining panel must be less than 25% of its surface.

 (d)
 If the damage is more than the permitted limits, replace the panel (Ref. TASK 25-00-00-340-019).

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 CC Honeycomb Linings - Example of Damage Through Figure 820/TASK 25-00-00-991-034
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 CC Honeycomb Linings - Example of Damage Not Through Figure 821/TASK 25-00-00-991-035
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 General Damage/Repair Identification Chart Figure 822/TASK 25-00-00-991-027
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 Subtask 25-00-00-020-085
 C. Removal of the Damaged Lining(s)
 (1) Remove the damaged linings if necessary for the selected repair procedure.
 (a)
 FWD cargo compartment:

 -
(Ref. TASK 25-54-11-000-001)

 -
(Ref. TASK 25-54-12-000-001)

 -
(Ref. TASK 25-54-12-000-002)

 -
(Ref. TASK 25-54-12-000-003)

 (b)
 AFT cargo compartment:

 -
(Ref. TASK 25-55-11-000-001)

 -
(Ref. TASK 25-55-11-000-002)

 -
(Ref. TASK 25-55-11-000-003)

 -
(Ref. TASK 25-55-12-000-001)

 -
(Ref. TASK 25-55-12-000-002)

 -
(Ref. TASK 25-55-12-000-003)

 Subtask 25-00-00-210-064
 D. Do an inspection of the component interface and/or the adjacent area.
 (1)
 Examine the support struts behind the removed linings and replace them if necessary:

 (a)
 FWD cargo compartment

 -(Ref. ASRM 532300)

 (b)
 AFT cargo compartment

 -
(Ref. TASK 53-43-11-000-001)

 -
(Ref. TASK 53-43-11-400-001)

 -
(Ref. ASRM 534300)

 (2)
 Make sure that all the equipment components are not damaged and in correct condition.

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 E. Repair of the Damaged Lining(s)
 (1) Do the repair of the damaged lining(s) as described in the tasks that follow:
 -Filler Repair Method (Damage Not Through) - All Cargo Compartment Linings with Honeycomb Core (Ref. TASK 25-00-00-340-004)
 -Patch and Filler Repair Method (Damage Not Through) - All Cargo Compartment Linings with Honeycomb Core (Ref. TASK 25-00-00-340-005)
　
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