(Continued)
AMM Item Description AIPC Reference AIPC Effectivity
2 (cont.) 53-52-00-03A-300 ILF 101, 151, 156-199,
331-399, 491-500, 535,
537, 553-557, 559-564,
567-569, 573-577, 581,
583, 585, 588-590,
592-599, 601-603, 606,
607, 610-615, 620,
625-627, 671, 672,
691-699, 709, 710,
803-813, 821, 822,
831-838, 841, 842, 851,
852, 854-858, 861-863,
871-874, 947, 948,
968-973, 980-999
F. Location Zones
Zone Area
111 Radome
G. Procedure
SUBTASK 53-52-03-100-006
(1) Clean the mating surfaces of the nose radome [1] and the applicable conductor straps [2] with
solvent, B00083.
SUBTASK 53-52-03-420-002
(2) Install applicable conductor straps [2] using adhesive, A00273, adhesive, A00435, adhesive,
A50355 or adhesive, A50081:
(a) To prepare the adhesive, do the following:
1) adhesive, A00273, before use, stir the individual components. Mix equal parts by
weight of components A and B.
NOTE: The pot life of adhesive, A00273 is approximately 2 hours below 80°F
(27°C). Prepare adhesive before use to maximize time for application.
2) adhesive, A00435, before use, stir the individual components. Mix equal parts by
weight of components A and B.
NOTE: The pot life of adhesive, A00435 is approximately 2 hours below 80°F
(27°C). Prepare adhesive before use to maximize time for application.
3) adhesive, A50355, before use, stir the individual components. Mix components in
accordance with the manufacturers instructions.
4) adhesive, A50081, before use, stir the individual components. Mix components in
accordance with the manufacturers instructions.
(b) Apply a thin continuous coat of blended adhesive to the faying surface of the conductor
straps [2] and nose radome [1].
NOTE: Application of adhesive on one surface is permitted on smooth faying surfaces of
less than 12 in
2
(77 cm
2
), if mating surfaces fit intimately and no voids are left in
the bond area.
(c) Align the conductor straps [2] holes with the nose radome [1] aft holes.
(d) Install the conductor straps [2] on the nose radome [1]:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-52-03
Page 408
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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