B.
C.
D.
E.
757
MAINTENANCE MANUAL
(c) Crowfoot Wrench AC34 (Utica Tool Company,
Orangeburg, South Carolina)
NOTE:____Commercially Available. Supplied
with the Torque Equipment B27064-1
only.
Consumable Materials
(1)
D00013 Grease, MIL-G-23827
(2)
C00259 Primer, BMS 10-11 - type 1
(3)
C00032 Enamel, BMS 10-60References
(1)
06-41-00/201, Fuselage Access Doors and Panels
(2)
24-22-00/201, Electrical Power - ControlAccess
(1)
Location Zones 211 Control Cabin (Left) 212 Control Cabin (Right) 113 Area Forward of NLG Wheel Well (Left )
(2)
Access Panel 113AL Flight/Landing Gear/Engine Control Components
Install Rudder Pedal Adjustment Crank (Fig. 401)
S 434-003
(1)
Do these steps to connect the cable to the rudder pedal jackshaft:
(a)
Put the grommet on the cable.
(b)
Push the cable through the grommet hole and the jackshaft support, then put the cable retaining nut and washer on the cable.
(c)
Apply a thin layer of grease to the outside diameter of the cable end before it is installed in the jackshaft.
(d)
Put the alignment tool through the hole in the bottom of the rudder pedal jackshaft. Hold the jackshaft universal joint and put the cable end into the jackshaft. Turn the cable end until it engages the jackshaft pin.
(e)
Hold the cable retaining nut with the crowfoot wrench. Use the flare nut wrench on the sleeve of the rudder pedal adjustment cable and tighten the retaining nut.
NOTE: Make sure the torque that is necessary to turn the
____ nut (before it touches the jackshaft support) is 90-400 pound-inches. When the nut touches the jackshaft support, turn it 1/4 to 1/2 of a turn more to tighten it.
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(2) S 434-016Install the cable clamps (7 locations). Make sure that the cable radius is not less than 5.0 inches (127 mm).
NOTE:____ A radius of less than 5.0 inches (127 mm) will cable to operate incorrectly. cause the
(3) S 434-017Install the stop plate and crank housing.
(4) S 434-018Tighten the four bolts, washers and nuts.
(5) S 434-004Do these steps to connect the cable to the crank lever assembly: (a) Push the cable end through the housing and tighten the cable retaining sleeve. (b) Put the washer on the cable that comes from the stop plate. Install the crank lever assembly, washer, and nut. Tighten the nut. (c) Install the lockwire. The location of the lockwire nut is optional.
NOTE:____ To get the best lockwire angle, make sure that the aft cable assembly can turn easily and smoothly.
(6) S 374-019Apply one layer of primer and 1 layer of enamel to the fasteners and the crank knob pin.
(7) S 094-020Remove these rig pins: (a) R1A and R1B (from the rudder pedals).
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(b) R2 (from the forward quadrant)
S 214-022
(8)
Turn the adjustment cranks full travel in each direction. Make sure that the rudder pedals move in a longitudinal direction.
F.
Put the Airplane Back to Its Usual Condition
S 864-023
(1)
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11:
(a)
11H17, FLT CONT SHUTOFF TAIL LEFT
(b)
11H18, FLT CONT SHUTOFF TAIL CTR
(c)
11H28, FLT CONT SHUTOFF TAIL RIGHT
S 864-024
(2)
Remove the DO-NOT-OPERATE tags and move the FLT CONTROL SHUTOFF switches L, C and R on the right side panel, P61, to ON.
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