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4) Make sure the gap between the bushings and the washers [65] is 0.01 inch (0.25
millimeter) minimum.
5) Install the new pins [63].
(c) Attach the hinge seals [7] to the balance panels [5]:
1) Attach the hinge seals [7] to the balance panels [5].
a) Make sure the correct number of balance weights [28] are installed on balance
panels 3 and 4 (SRM 51-60-01).
2) Apply compound, C00528 to bolts [3], [4], [6], and [27].
3) Install balance weights [28] with bolts [3].
4) Install balance weights [26] with the bolts [8] with collars [9], bolts [27], bolts [6], and
bolts [4].
(d) Connect the tab control rods [41] to the forward fittings.
1) Install the bolts [50], washers [49], bushings [48], washers [47] and nuts [46].
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2) Tighten the nuts [46] to 50-80 pound-inches (5.6 9.0 newton-meters).
NOTE: Tighten the nut [46] to the lower end of the torque range. Continue to tighten
the nut until the next castellation aligns with the hole in the bolt [50].
3) Install the pins [45].
(e) At hinge 1, do these steps:
1) Install the radial seal retainer [16], washers [14] and bolts [15];
2) Install the radial seal [25], radial seal retainer [24], washers [14] and bolts [23];
3) Connect the bonding jumper [13] with washer [12] and nut [11].
(f) At hinge 2, do these steps:
1) Install the radial seal [31], radial seal retainer [33], washers [14] and bolts [29];
2) Install the radial seal [39], radial seal retainer [37], washers [14] and bolts [35].
(g) At hinge 3, do these steps:
1) Install the radial seal [32], radial seal retainer [34], washers [14] and bolts [30];
2) Install the radial seal [40], radial seal retainer [38], washers [14] and bolts [36].
(h) At hinge 4, do these steps:
1) Install the radial seal [42], radial seal retainer [44], washers [14] and bolts [43];
2) Install the radial seal [87], radial seal retainer [85], washers [14] and bolts [86].
(i) At hinge 5, do theses steps:
1) Install the radial seal [54], radial seal retainer [53], washers [14] and bolts [52];
2) Install the radial seal retainer [62], washers [14] and bolts [61].
SUBTASK 27-11-11-720-001
(7) Do the aileron surface friction and motion test.
(a) With a push/pull scale 0-25 pound (0-11 kilogram), STD-753, measure the force at 8.75 +/-
0.25 inch (222.25 +/- 6.35 millimeters) aft of the hinge centerline and perpendicular to the
aileron chord plane.
(b) Write down the (positive) forces necessary to move each aileron through the neutral
position.
(c) Write down the (negative) forces necessary to prevent movement of the aileron through the
neutral position.
(d) Add these forces together.
(e) Make sure the result is not more than 5 pounds (22.2 newtons).
1) If the result is more than 5 pounds (22.2 newtons), do these checks;
a) Make sure that all the hinge bolts are sufficiently lubricated.
b) Make sure the torque values of the hinge bolts are as specified.
(f) Measure the force necessary to move the aileron through full travel in each direction, then
back to the neutral position.
NOTE: The movement of the aileron must be free and smooth.
1) Apply the force perpendicular to the aileron chord plane 8.75 +/- 0.25 inches (222.25
+/- 6.35 millimeters) aft of the aileron hinge line.
2) Make sure the maximum force is not more than 13 pounds (57.8 newtons) for aileron
down and 3 pounds (13.3 newtons) for aileron up.
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SUBTASK 27-11-11-420-003
(8) Connect the aileron control rod [67] to the aileron [1].
(a) Put the aileron control rod [67] in its position;
(b) Install the bolt [71], washer [72], bushing [75], washer [76], nut [78] and new pin [77].
SUBTASK 27-11-11-420-004
(9) Install the removable fairing [74]:
(a) Connect the bonding jumper [84] with washer [83] and nut [82];
(b) Put the removable fairing [74] in its position;
(c) Install the bolts [73] to attach the removable fairing [74] to the aileron [1].
SUBTASK 27-11-11-280-002
(10) Use the aileron control wheel to manually operate the aileron through a minimum of two full
cycles, to full travel.
(a) Make sure the aileron can move smoothly and freely.
SUBTASK 27-11-11-220-002
(11) Do a check of the aileron clearances and mismatch (Figure 403).
(a) Make sure the clearances for the upper and lower surfaces of the aileron and the fixed
　
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