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110 (43) `F (`C) TEMPERATURE 1 123 (55.8) TENSION IN POUNDS (kg) 2 3 CABLE RIG LOAD-SPOILER SYSTEM
90 (32) 114 (51.7)
80 (27) 110 (49.9)
70 (21) 106 (48.1)
60 (16) 102 (46.3)
50 (10) 97 (44)
40 (4) 93 (42.2)
30 (-1) 89 (40.4)
10 (-12) 80 (36.3)
-10 (-23) 72 (32.7)
-30 (-34) 64 (29)
-40 (-40) 58 (26.3)
TO MAKE SURE THAT YOU GET THE CORRECT
CABLE TENSION, LET THE AMBIENT TEMPERATURE
OF THE AIRFRAME STAY CONSTANT (|5`F) (-15`C)
FOR A MINIMUM OF 1 HOUR.
THE SYSTEM MUST BE ADJUSTED WHEN
THE CABLE LOADS ARE MORE THAN |15 LBS (|6.8 kg)
FROM THE TABLE VALUES.
WHEN RIGGING THE SYSTEM, CABLE LOADS SHOULD
BE |5 LBS (|2.27 kg) FROM THE TABLE VALUES.
SPOILERS NO. 1 AND 12 QUADRANT RIG PINS
SPOILERS NO. 3 AND 10A/S-18 AND A/S-20 QUADRANT RIG PINSSEE FIGURE 503
Flight Spoiler Control System - Rig Pin Locations and Cable Tensions
Figure 501 (Sheet 1)
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CABLE AB
CABLE AA
SEE A
TURNBUCKLES CABLE WS1B
CABLE WS2B
LEFT SPOILER DIFFERENTIAL MECHANISM RIG PINS CABLE WS1A
A/S-4, A/S-14 AND A/S-16 SEE FIGURE 502
RIGHT SPOILER DIFFERENTIAL MECHANISM RIG PINS A/S-5,A/S-15 AND A/S-17 CABLE WS2A SEE FIGURE 502
CABLE AA TURNBUCKLES
CABLE AB
A
Flight Spoiler Control System - Rig Pin Locations and Cable Tensions
Figure 501 (Sheet 2)
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SEE A
SPOILER
DIFFERENTIAL
MECHANISM
(2 LOCATIONS) RIG PIN
A/S-4
RIG PIN RIG PIN
WS1B CABLE WS2B CABLE QUADRANT A/S-14 RIG PIN A/S-12 A/S-16
(4 LOCATIONS) RIG PIN
RIG PIN A/S-5 RIG PIN
A/S-2 A/S-13
RIG PIN A/S-15
RIG PIN A/S-17
CABLE
WS2A
CABLE CABLE CABLE CABLE CABLE
WS1A WS2A WS1A WS2B WS1B
SPOILER DIFFERENTIAL MECHANISM AND
QUADRANT RIG PIN LOCATIONS
A
Spoiler Differential Mechanism and Quadrants - Rig Pin Locations
Figure 502
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SEE B
SEE A
OUTBOARD FLIGHT SPOILER
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