(g)
Move the rudder pedals through their full travel range 5 times and do these steps:
NOTE: Release the right rudder pedal last on the last cycle.
____
1) Make sure the rudder is no more than 0.15 inch (3.81 mm) away from the mark on the tail cone index plate (use the left side of the rudder trailing edge). If the rudder position is not correct do the rudder PCA adjustment procedure again.
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2) Put tape on the tail cone index plate and make a mark of the rudder position (use the left side of the rudder trailing edge).
NOTE: This mark is the "low speed" position for the rudder
____ ratio changer actuator.
3) Move the left RRCM test switch to TEST.
NOTE: This puts the ratio changer actuator in its "high
____
speed" position.
4) Make a mark of the rudder position and do this step (use the left side of the rudder trailing edge):
NOTE: This mark is the "high speed" position for the ratio
____ changer actuator.
a) If the two marks are more than 0.05 inch (1.27 mm) apart, do the full "Rudder Ratio Changer Mechanism and Rudder PCAs - Adjustment" procedure again.
5) Move the test switches on the left and right RRCMs to NORMAL. Stop for 30 seconds and do this check:
NOTE: This puts the ratio changer actuator in its "low
____
speed" position.
a) Make sure the rudder trailing edge is no more than 0.05 inch away from the "high speed" mark on the tail cone tape.
(h)
Move the yaw damper switches on the P5 overhead panel to their ON positions.
(i)
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P11 panel: 1) 11A18, YAW DAMPER LEFT 2) 11F34, YAW DAMPER RIGHT
N.
Autopilot Rollout Guidance Servo - Adjustment
S 825-124
(1)
Do the adjustment procedure for the autopilot rollout guidance servos (AMM 22-13-01/401).
O.
Rudder Position Transmitter - Adjustment
S 825-125
(1)
Do the adjustment procedure for the rudder position transmitter (AMM 27-28-00/501).
P.
Rudder Trim Indicator - Adjustment (Fig. 508)
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S 865-012
WARNING:_______ KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN
HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER,
FLAPS, SLATS, SPOILERS, AND STABILIZER ARE FULLY POWERED
SURFACES. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR
WHEN HYDRAULIC POWER IS SUPPLIED.
(1)
Supply pressure to the left, right, and center hydraulic systems (AMM 29-11-00/201).
S 865-126
(2)
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P11 panel:
(a) 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址:757 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 2(15)