Aug 01/05
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CES
CC Honeycomb Linings, Patch/Rivets - Damage Through Figure 831/TASK 25-00-00-991-045
R EFF : CES ALL 25-00-00 Page A860 Aug 01/05
(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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Aug 01/05
R
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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Aug 01/05
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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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