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Boeing 737-600 - Subtask 53-52-00-100-005; Subtask 53-52-00-400-001; Subtask 53-52-00-400-002; Subtask 53-52-00-400-003

Boeing 737-600
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C. Consumable Materials
Reference Description Specification
B50073 Alcohol - Isopropyl ASTM D 770
G00034 Cotton Wiper - Process Cleaning Absorbent
Wiper (Cheesecloth, Gauze)
BMS15-5 Class A
G02219 Tape - Yellow Vinyl Adhesive, Scotch Brand
No.471, 1.5 Inches (38.1 mm) Wide
G50220 Pad - Abrasive, Scotch- Brite 7447
D. Location Zones
Zone Area
111 Radome
E. Procedure
SUBTASK 53-52-00-100-005
(1) Clean the nose radome area for the radome boot installation.
NOTE: Use a clean cloth to clean the area to keep from contamination.
SUBTASK 53-52-00-400-001
(2) Cut the radome boot 0.25 in. (0.64 cm) above the cut line. The cut line (end line) is at STA
138.6.
NOTE: Make the cuts as smooth as possible and avoid jagged edges.
SUBTASK 53-52-00-400-002
(3) Put the radome boot on the nose radome.
(a) Align the radome boot to the center of the nose radome.
SUBTASK 53-52-00-400-003
(4) Apply Scotch Brand No.471 tape, G02219 at 3 locations on the nose radome and the radome
boot (Figure 202).
NOTE: The markings will be used to align the radome boot to the same location after the
protective lining is removed.
SUBTASK 53-52-00-400-004
(5) Apply the wet solution to the radome boot.
NOTE: The wet solution is made from 25% isopropyl alcohol, 75% water, and 1 teaspoon of a
dishwashing liquid per 1 gallon (3.8 liters).
NOTE: The wet solution prevents the adhesive from sticking to itself.
SUBTASK 53-52-00-400-005
(6) Turn the inner surface of the radome boot out.
SUBTASK 53-52-00-000-005
(7) Remove the protective lining:
(a) Slowly and carefully remove the protective lining.
(b) Apply the wet solution to the nose radome adhesive during the lining removal.
NOTE: The wet solution is made from 25% isopropyl alcohol, 75% water, and 1
teaspoon of a dishwashing liquid per 1 gallon (3.8 liters).
NOTE: The wet solution prevents the adhesive from sticking to itself.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-52-00
Page 206
D633A101-ILF Jun 15/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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