(9)
A01046 Insulation Coating, BMS 10-102, TYPE I, CLASS 2, GRADE 30 (AMM 20-30-11/201)
(10)
C00870 Silicone Primer, DC-1200, Red Tinted (AMM 20-30-41/201)
(11)
Topcoat, BMS 10-102, Type II (AMM 20-30-11/201)
(12)
Topcoat, BMS 10-102, Type II w/ fiber re-enforcement (AMM 20-30-11/201)
(13)
Thinner, Naphtha, BMS 3-2 Type II (AMM 20-30-31/201)
(14)
A00308 Tin Octoate (Nuocure 28) (AMM 20-30-41/201)
(15)
Teflon Sheet
(16)
D00576 Cleara Mold Release Wax (100% yellow carnuba base wax, no silicones) Cleara Products, Inc., P.O. Box 5724, Denver CO
(17)
Frekote 33 Aerosol Spray Frekote, Inc., Boca Raton, FL
(18)
KRAXO 1711 Aerosol Spray Contour Chemical Company, North Reading, MA
(19)
A00937 MS-122 Aerosol Spray Miller-Stephenson Chemical Company, Danbury, CN
(20)
Release-All No. 30 Aerosol Spray (blue) Airtech International, Carson CA
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-01
ALL ú ú C02 Page 802 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(21)
Silica Fibers, Hitco F100-A25, Hitco Division of Armco Steel,
Gardena, California (CMM 20-60-04).
C.
References
(1)
AMM 71-11-02/201, FAN COWL PANELS
(2)
AMM 78-31-00/201, Thrust Reverser System
(3)
Boeing Material Specification BMS 10-102
D.
Preparation for the Repair (Fig. 801 and 802)
S 048-031-C00
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1)
Do the deactivation procedure for the thrust reverser for ground
maintenance (AMM 78-31-00/201).
S 018-032-C00
(2)
Open the (left, right) fan cowl panel (AMM 71-11-02/201).
S 018-033-C00
WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO OPEN THE THRUST
_______
REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS WHEN YOU OPEN
THE THRUST REVERSERS, INJURIES TO PERSONS OR DAMAGE TO
EQUIPMENT CAN OCCUR.
(3)
Open the (left, right) thrust reverser (AMM 78-31-00/201).
S 218-003-C00
(4)
Examine all insulation.
S 358-004-C00
(5)
If you can put a one-inch diameter dowel into the area where there
is no insulation, do these steps:
(a)
Examine the honeycomb panel face sheet for delamination. 1) Repair the honeycomb if delamination has occured.
(b)
Repair the loose insulation before the insulation falls off.
(c)
Replace the insulation with the same or more than the initial thickness.
(6)
Examine the insulation for damage.
(7)
Seal all of the damaged areas with BMS 10-102, Type II.
S 358-007-C00
(8)
Use the major damage repair procedure if the damaged areas of the
insulation are less than two inches between the dowel centers.
S 218-005-C00
S 398-006-C00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-01
ALL ú ú C02 Page 803 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 358-008-C00
(9) The thicknesses of the insulation layer are shown on Fig. 802.
(a)
The areas coated to keep the structure serviceable during operation are shown.
(b)
Other areas are coated to decrease the damage and repair costs if a duct rupture or fire occurs.
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