(3)
B00148 Solvent, Methyl Ethyl Ketone (AMM 20-30-02/201)
(4)
Dibutyl Tin Dilaurate (Thermolyte-12) (AMM 20-30-03/201)
(5)
A00964 Chemical and Solvent Resistant Finish, BMS 10-11, Type II, (QPL)
(6)
A01045 Insulation Coating, BMS 10-102, Type I, Class 1, Grade 28 (AMM 20-30-03/201)
(7)
A01045 Insulation Coating, BMS 10-102, Type I, Class 1, Grade 25 (AMM 20-30-03/201)
(8)
A01046 Insulation Coating, BMS 10-102, TYPE I, CLASS 2, GRADE 32 (AMM 20-30-03/201)
(9)
A01046 Insulation Coating, BMS 10-102, TYPE I, CLASS 2, GRADE 30 (AMM 20-30-03/201)
(10)
Silicone Primer, DC-1200 (AMM 20-30-03/201)
(11)
A01047 BMS 10-102, TYPE II Topcoat, Grade A
(12)
A01047 BMS 10-102, Type II Topcoat, Grade B
(13)
A01050 RTV 106
(14)
C00926 BMS 10-102QPL (TR28)
(15)
Thinner, Naphtha, BMS 3-2 Type II (AMM 20-30-02/201)
(16)
Tin Octoate (Nuocure 28) (AMM 20-30-03/201)
(17)
Teflon Sheet
(18)
Cleara Mold Release Wax (100% yellow carnuba base wax, no silicones) Cleara Products, Inc., P.O. Box 5724, Denver CO
(19)
Frekote 33 Aerosol Spray Frekote, Inc., Boca Raton, FL
(20)
KRAXO 1711 Aerosol Spray Contour Chemical Company, North Reading, MA
(21)
MS-122 Aerosol Spray Miller-Stephenson Chemical Company, Danbury, CN
(22)
Release-All No. 30 Aerosol Spray (blue) Airtech International, Carson CA
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-01
ALL ú ú N01 Page 802 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(23)
G00034 BMA15-5, Class A Wiper
C.
References
(1)
AMM 71-11-04/201, Fan Cowl Panels
(2)
AMM 71-11-06/201, Core Cowl Panels
(3)
AMM 78-31-00/201, Thrust Reverser System
(4)
Boeing Material Specification BMS 10-102
D.
Access
(1)
Location Zone
415 and 416 Engine 1 - Thrust Reverser Halves
425 and 426 Engine 2 - Thrust Reverser Halves
435 and 436 Engine 3 - Thrust Reverser Halves
445 and 446 Engine 4 - Thrust Reverser Halves
(2)
Access Panel
413 and 414 Fan Cowl Panels - Engine 1
417 and 418 Core Cowl Panels - Engine 1
423 and 424 Fan Cowl Panels - Engine 2
427 and 428 Core Cowl Panels - Engine 2
433 and 434 Fan Cowl Panels - Engine 3
437 and 438 Core Cowl Panels - Engine 3
443 and 444 Fan Cowl Panels - Engine 4
447 and 448 Core Cowl Panels- Engine 4
E.
Preparation for the Repair (Fig. 801 and 802)
S 018-037-N00
(1) Open the fan cowl panels (AMM 71-11-04/201).
S 048-038-N00
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.
(2)
Do the deactivation procedure for the thrust reverser for ground
maintenance (AMM 78-31-00/201).
(3)
Open the core cowl panels (AMM 71-11-06/201).
S 018-039-N00
S 018-040-N00
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.
(4)
Open the thrust reverser (AMM 78-31-00/201).
(5)
Examine all insulation.
S 218-041-N00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-01
ALL ú ú N01 Page 803 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
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