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STD-3911 Brush - Bristle, Medium Nylon
C. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
C00259 Primer - Chemical And Solvent Resistant Finish,
Epoxy Resin
BMS10-11,
Type I
C00528 Compound - Corrosion Preventive, Petroleum Hot
Application (Soft Film)
MIL-C-11796,
Class III
G00009 Compound - Organic Corrosion Inhibiting BMS3-23
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
10 Pin 27-11-31-01-069 GUN 001-028, 101-121,
155-157, 201-999
27-31-41-01-110 GUN ALL
22 Panel assembly 27-11-31-01-519 GUN 001-028, 101-121,
155-157, 201-999
27-11-31-01-522 GUN 001-028, 101-121,
155-157, 201-999
23 Panel assembly 27-11-31-01-366 GUN 001-028, 101-121,
155-157, 201-999
27-11-31-01-369 GUN 001-028, 101-121,
155-157, 201-999
24 Panel assembly 27-11-31-01-213 GUN 001-028, 101-121,
155-157, 201-999
27-11-31-01-216 GUN 001-028, 101-121,
155-157, 201-999
25 Panel assembly 27-11-31-01-063 GUN 001-028, 101-121,
155-157, 201-999
27-11-31-01-066 GUN 001-028, 101-121,
155-157, 201-999
E. Location Zones
Zone Area
572 Left Wing - Aileron
672 Right Wing - Aileron
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-31
Page 406
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
F. Access Panels
Number Name/Location
571BB Lower Outboard Fixed Trailing Edge Access Panel
571CB Lower Outboard Fixed Trailing Edge Access Panel
571DB Lower Outboard Fixed Trailing Edge Access Panel
671BB Lower Outboard Fixed Trailing Edge Access Panel
671CB Lower Outboard Fixed Trailing Edge Access Panel
671DB Lower Outboard Fixed Trailing Edge Access Panel
G. Aileron Balance Panels Installation
SUBTASK 27-11-31-220-001
(1) If you install used bolts, bushings or other components that have worn areas, do this task:
Aileron Balance Panel Seals Visual Inspection, TASK 27-11-31-210-801.
SUBTASK 27-11-31-420-001
(2) Install the balance panel assembly [22], balance panel assembly [23], balance panel
assembly [24] or balance panel assembly [25]:
(a) Install the bolts [26], washers [7], washers [8], and nuts [9] to attach the balance panel
assembly [22], balance panel assembly [23], balance panel assembly [24] or balance panel
assembly [25] to the wing structure.
(b) Tighten the nuts [9] to 25-35 pound-inches (2.8-4.0 newton-meters).
NOTE: Tighten the nut [9] to the lower end of the torque range. Continue to tighten the nut
[9] until the next castellation aligns with the hole in the bolt [26].
1) Make sure the gap between the bushing face and the washer [8] under the nut [9] is
0.010 inch (0.25 millimeter) minimum after torque up.
(c) Install the pins [10].
(d) Make sure the washers [7] is bonded to the hinge half.
1) If it is necessary, bond the washers [7] to the hinge half with sealant, A00247.
(e) Install the bolts [6], washers [7], washers [8], and nuts [9] to attach the aileron balance
panel assembly [22], panel assembly [23], panel assembly [24] or panel assembly [25] to
the aileron.
(f) Tighten the nuts [9] to 25-35 pound-inches (2.8-4.0 newton-meters).
NOTE: Tighten the nut [9] to the lower end of the torque range. Continue to tighten the nut
[9] until the next castellation aligns with the hole in the bolt [6].
1) Make sure the gap between the bushing face and the washer [8] under the nut [9] is
0.010 inch (0.25 millimeter) minimum after torque up.
(g) Install the pins [10].
(h) Make sure the aerodynamic seals [15], hinge seals [20] and [29] are not damaged.
(i) Install the seal retainer [18] to the hinge seal [20] with the bolts [16] and washers [17].
(j) Attach the hinge seal [29] to the balance panel assembly [22], balance panel assembly [23],
balance panel assembly [24] or balance panel assembly [25].
(k) Install the balance weights [19] to the balance panel assembly with the bolts [4],[5],[21] and
bolts [2] with collars [3].
1) Apply primer, C00259 to the holes of the balance weights [19].
2) Apply compound, C00528 to the bolts [2],[4], [5], and [21].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-31
Page 407
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
3) Tighten the bolts [2],[4],[5] and [21] to 35-50 pound-inches (4.0-5.0 newton-meters).
(l) Make sure there are the same number of balance weights [11] on the new balance panel
　
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