(a)
Make sure the IN TEST light stays on for a maximum of 18 seconds.
(b)
After 30 seconds, make sure all the RRCM faultballs are black.
S 865-098
(12)
Move the right RRCM test switch on the E4 equipment shelf to TEST and do these checks:
(a)
Make sure the IN TEST light stays on for a maximum of 18 seconds.
(b)
After 30 seconds, make sure all the RRCM faultballs are black.
S 215-099
(13) Make sure that rig pins R5 and R6 can be easily installed at the same time. If they cannot be installed at the same time, replace the LVDT (AMM 27-21-12/201).
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MAINTENANCE MANUAL
ú
ú S 095-624
ú (14) Remove rig pins R3, R5, and R6.
S 865-100
(15) Move the right RRCM test switch to NORMAL and do these checks:
(a) Make sure the IN TEST light stays on for a maximum of 18
seconds.
(b) After 30 seconds, make sure all the RRCM faultballs are black.
S 865-101
(16) Remove the power from the left hydraulic system (AMM 29-11-00/201).
J. Rudder Thermal Compensating Linkage - Adjustment
NOTE: Before this procedure is done, make sure the airplane is____
stable at ambient air temperature |10.0 degrees F (|5.5 degrees
C). Before adjustments or adjustment checks are made, make sure
the temperature has been stable for at least one hour.
S 825-104
(1) Adjust the top compensating rod until these conditions are
satisfactory:
(a) Make sure the top and bottom gaps on the input crank hammer are
not more than 0.09 inch (2.3 mm) (Fig. 510).
(b) Make sure the top and bottom gaps of the input crank hammer are
the same (use a tolerance of |0.01 inch (+/- 0.25 mm)).
S 435-105
(2) Tighten the jamnuts and do this check:
(a) Make sure that control rod threads can be seen in at least
one-half of the control rod inspection hole.
K. Yaw Damper Pogo - Adjustment (Fig. 507)
S 865-106
(1) Remove the power from the left, right, and center hydraulic systems
(AMM 29-11-00/201).
S 865-107
(2) Move the FLT CONTROL SHUTOFF L, R, and C switches on the P61 panel
to OFF. Attach DO-NOT-OPERATE tags and make sure the switch
position lights come ON.
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MAINTENANCE MANUAL
S 865-108
(3)
Open these circuit breakers on the P11 panel and attach DO-NOT-CLOSE tags:
(a)
11H17, FLT CONT SHUTOFF TAIL LEFT
(b)
11H18, FLT CONT SHUTOFF TAIL CTR
(c)
11H28, FLT CONT SHUTOFF TAIL RIGHT
S 215-109
(4) AIRPLANES WITH SHEAR PINS; Make sure that rig pin R9 can be easily installed through the inspection hole in the yaw damper shear pin (Fig. 507).
NOTE: If rig pin R9 can not be installed through the shear pin,
____
you must examine it for damage.
S 215-619
(5) AIRPLANES WITH SHEAR RIVETS; Make sure that rig pin R9 can be easily installed through the inspection hole that is located below the yaw damper shear rivets (Fig. 507).
NOTE: If rig pin R9 can not be installed through the inspection
____ hole, you must examine the shear rivets for damage.
S 825-110
(6)
Make sure that rig pin R8 can be installed in the yaw damper pogo. Do these steps if it can not be installed:
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