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 CES

 CC Honeycomb Linings, Patch/Rivets - Damage Through Figure 831/TASK 25-00-00-991-045
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 (2)
 Smooth and deburr the repair with emery cloth grade 80-120.

 (3)
 Clean the repair area with CLEANING AGENTS (Material No. 11-010) and a lint free cotton cloth MISCELLANEOUS (Material No. 19-003)

 (4)
 Make sure that the repair area is dry.

 (5)
 Cut two patches BONDING AND ADHESIVE COMPOUNDS (Material No. 08-083) to the applicable dimensions.

 NOTE : The repair patches must be 38 mm (1.5 in.) larger than the
____
 damaged area in all directions.

 NOTE : The overlap of patches is not allowed
____
 (6)
 Deburr the edges of the patches with emery cloth grade 80-120.

 (7)
 Use a heat blanket between 100 DEG.C (212.00 DEG. F) and 110 DEG.C

 (230.00 DEG.F) with a soft force to bond the first repair patch to the rear side of the panel.

 (8)
 Fill the

 -
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115)
 or

 -
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115A)
 or

 -
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115B)
 or

 -
BONDING AND ADHESIVE COMPOUNDS (Material No. 08-115C)
 into the prepared area.

 NOTE : Obey the manufacturers instructions.
____
 (9) Use a heat blanket between 100 DEG.C (212 DEG.F) and 110 DEG.C (230 DEG.F) with a soft force to bond the second repair patch to the view (cargo compartment) side of the panel.
 (10) From the view (cargo compartment) side of the panel:
 (a) Drill holes along the edges of the patch, through the entire patch/panel/patch assembly, regularly spaced with a 3.3 mm (0.128 in.) to 3.5 mm (0.137 in.) drill..
 NOTE : The distance to the edges should not be less than 15 mm
____ (0.5 in.).
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 CES  NOTE : The distance between the holes should not be more than 100

____
 mm (3.8 in.).

 (11) Install the rivets from the view (cargo compartment) side of the panel with the necessary rivet length.
 NOTE : In order to select the correct length for the rivets refer to
____ the thickness of the panel with the patches.
 (a) Install the rivets:
 -
Monel Rivet (NAS 1919 M 04 S 06 U)
 or

 -
Monel Rivet (NAS 1919 M 04 S 07 U)
 or

 -
CRES rivets (NAS 1919 C 04 S 06 U)
 or

 -
CRES rivets (NAS 1919 C 04 S 07 U)
 with the GUN - FASTENER

 5. Close-up
________
 Subtask 25-00-00-410-081
 A. Close Access
 (Ref. TASK 25-00-00-200-001)

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 CES  TASK 25-00-00-340-025

 Speed Patches and Filler Repair Method (Damage not Through) - All Cargo Compartment Linings with Honeycomb Core
 1. Reason for the Job
__________________
 Refer to the AMM task 25-00-00-200-001
 2. Job Set-up Information
______________________
 A. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific emery cloth grade 80-120. No specific GILLFAB 1367P-013 No specific GILLPATCH III Material No. 08-066 D DAN 319, DAN 1202
 ACRYLIC PRESSURE SENSITIVE ADHESIVE FILM
 (Ref. 20-31-00) Material No. 08-115 AIB AIMS 08-08-001
 CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 08-115A AIB AIMS 08-08-001
 CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 08-115B AIB AIMS 08-08-001
 CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 08-115C D DAN 1282
 CORE FILLER AMBIENTTEMPERATURE CURING (Ref. 20-31-00) Material No. 11-010 USA TT-I-735 GRADE A
 ISOPROPYL ALCOHOL (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-00-00-200-001 Cargo Compartment Linings with Honeycomb Core -
General Repair/Protection Information 25-00-00-991-044 Fig. 832
　
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