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(g) Note the location of the protractor on the spoiler panel.
(h) When measuring the UP position of right wing spoiler panel, note the +/- reading on the
protractor.
(i) Move the speed brake lever to the DOWN position.
(j) Measure and record the down position of spoiler panel #11.
NOTE: Make sure to place the protractor in the same location as noted on spoiler panel
11. Do not adjust the protractor zero for this measurement.
(k) Note the +/- reading on the protractor.
(l) Calculate the total travel for right wing spoiler panel by subtracting the DOWN position
measurement from the UP position measurement.
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(m) Verify there is not more than 1/2 degree difference between each corresponding spoiler
panel.
Table 507/27-61-00-993-814
Required Actual
Left Wing Spoiler Panel 15 +/- 1 Degree
Right Wing Spoiler Panel UP Measured
Right Wing Spoiler Panel DOWN Measured
Calculated Travel Right Wing
Panel
Calculated Figure
Verify Symmetry 1/2 Degree
SUBTASK 27-61-00-860-105
(12) Do the following steps to test Spoiler response at FLIGHT DETENT position:
(a) Adjust the spoiler panel protractor to read zero degrees on panel 2 in the DOWN position
(Table 508).
NOTE: Make sure to note the location of the protractor on the spoiler panel.
(b) Measure and record the position of spoiler panels 3, 4, 5, 8, 9, 10 and 11.
NOTE: Make sure to note the position of the protractor on each spoiler panel.
(c) Move the speed brake lever to the FLIGHT DETENT position.
(d) Measure and record the position of spoiler panels 3, 4, 5, 8, 9, 10 and 11.
NOTE: Make sure to place the protractor in the same positions as noted above. Do not
adjust the protractor zero for this measurement.
(e) Note the +/- reading on the protractor while measuring the UP position.
(f) Calculate and record the total travel for spoiler panels 2, 3, 4, 5, 8, 9, 10 and 11 by
subtracting the DOWN position measurement from the FLIGHT DETENT measurement.
Table 508/27-61-00-993-815
Panel Number Panels Down Flight Detent Calc. Travel
Panel 2
Panel 3
Panel 4
Panel 5
Panel 8
Panel 9
Panel 10
Panel 11
SUBTASK 27-61-00-860-106
(13) Make sure that there is no more than a one degree difference between opposite spoiler panel
pairs: 2 and 11, 3 and 10, 4 and 9, and 5 and 8 (Table 509).
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Table 509/27-61-00-993-816
Difference Required Actual
Panel 2 and 11 1 Degree Max.
Panel 3 and 10 1 Degree Max.
Panel 4 and 9 1 Degree Max.
Panel 5 and 8 1 Degree Max.
SUBTASK 27-61-00-860-107
(14) Do these steps to test spoiler response at Full Speed Brake.
NOTE: In order to complete these steps, you must have noted the measurements for the
DOWN position of spoiler panels 3, 4, 5, 8, 9, 10 and 11.
(a) Move the Speed Brake lever into the FULL UP position.
(b) Measure and record the position of Spoiler panels 2, 3, 4, 5, 8, 9, 10 and 11 (Table 510).
NOTE: Make sure to place the protractor in the same positions as noted above. Do not
adjust the protractor zero for this measurement.
(c) Note the +/- reading on the protractor as this value must be used to calculate total panel
travel.
(d) Calculate the total travel for each spoiler panel by subtracting the DOWN position
measurement from the full UP position measurement.
Table 510/27-61-00-993-817
Panel Number Panels Down Full Up Calc. Travel
Panel 2 zero
Panel 3
Panel 4
Panel 5
Panel 8
Panel 9
Panel 10
Panel 11
(e) Make sure that there is no more than 2 degrees difference between symmetric spoiler
panel pairs: 2 and 11, 3 and 10, 4 and 9, 5 and 8.
(f) Turn the captain’s control wheel clockwise to 87 degrees and hold.
(g) Measure and record the position of flight spoilers 8, 9, 10 and 11 (Table 511).
NOTE: If spoiler panels 8, 9, 10 and 11 do not move, use the calculated panel travel from
above instead.
(h) Make sure spoiler panels 2, 3, 4 and 5 are partially raised.
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Table 511/27-61-00-993-818
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737-600-700-800-900 飞机维护手册6 AIRCRAFT MAINTENANCE MANUA(19)
