CAUTION
DO NOT USE METAL TOOLS TO REMOVE THE SEALANT. AN
APPROVED TOOL WILL PREVENT DAMAGE TO THE SKIN OF THE
AIRCRAFT.
(b) Use a hard resin phenolic scraper, STD-1064 to release the scuff plate [7] from the
structure.
(c) Remove the scuff plate [7] from the structure.
END OF TASK
TASK 53-11-02-420-801
3. Cargo Door Scuff Plate - Installation
A. References
Reference Title
20-30-88 P/B 201 AIRPLANE STRUCTURE CLEANING SOLVENTS (Series 88) -
MAINTENANCE PRACTICES
51-21-41-370-802 Bonderite M-CR 600 Aero, Bonderite M-CR Alcrm 1200 Aero or
Bonderite M-CR 1200S Aero Application Process (P/B 701)
51-31-00 P/B 201 SEALS AND SEALING - MAINTENANCE PRACTICES
SOPM 20-41-05 Application of Corrosion Inhibiting Compounds
SOPM 20-50-19 General Sealing
B. Consumable Materials
Reference Description Specification
A01024 Compound - Fairing - 3M EC-3587B BAC5530
A50250 Sealant - P/S 870 Class B-1/2 Corrosion
Inhibitive Sealant
BMS5-95 Class B-1/2
A50419 Sealant - Pressure And
Environmental-Chromate, Type I, Class B-2
BMS5-95 Type I Class
B-2
B00148 Solvent - Methyl Ethyl Ketone (MEK) ASTM D740
B00184 Solvent - Presealing, Cleaning Solvent BMS11-7
B00666 Solvent - Methyl Propyl Ketone BMS11-9
C00259 Coating - Chemical And Solvent Resistant
Finish, Corrosion Inhibiting Primer
BMS10-11 Type I
G00009 Compound - Organic Corrosion Inhibiting BMS3-23
G02185 Agent - Peelable Parting (Valspar - 4A-183
Green Strippable Coating)Manufacturing
discontinued, use stock until depleted
G50313 Agent - Non-Peelable Parting (Henkel Loctite -
Frekote 710-NC Mold Release)
BAC5000
G50365 Agent - Peelable Parting (AC Products -
AC962-73C) Production discontinued, use
stock until depleted.
BAC5000
G50366 Agent - Parting, Peelable, AZ 534-2B (0A3C8 -
Aztec Chemical, Inc., El Monte, CA)
BAC5000, PSD 6-187
G50367 Agent - Peelable Parting (Aztec Chemical AZ
634-2)
MIL-PRF-6799,
BAC5000
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-11-02
Page 405
D633A101-ILF Feb 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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