(b)
11J8, FLIGHT RECORDER DC
(c)
11S1, AIDS SENSOR
(2)
Set the rudder pedals in the neutral position.
S 864-003
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MAINTENANCE MANUAL
SEE A
113AL
RUDDER
JACKSHAFT
RUDDER
PEDAL
ARM
RUDDER FORWARD
QUADRANT
RIG PIN
HOLE R1A
(LEFT)
R1B
(RIGHT)
SEE B RIG PIN
HOLE R2
FWD LOCKWIRE ARM CRANK
MICRO
ADJUSTMENT
JACKSHAFT AND FORWARD QUADRANT ROD BRACKET
ROD
A ASSEMBLY
TRANSDUCER
TRANSDUCER INSTALLATION B Rudder Pedal Position Transducer Installation Figure 401
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S 864-034
(3)
Attach DO-NOT-OPERATE tags to the captain's and first officer's rudder pedals.
S 014-004
(4)
Open the forward access door to get to the forward quadrant (AMM 06-41-00/201).
S 834-005
(5)
Install the rig pin R2 into the forward quadrant.
S 834-006
(6)
Install the rig pins R1A and R1B into the rudder pedal arms through the rudder pedal housing.
S 034-007
(7)
Disconnect the transducer electrical connector.
S 034-008
(8)
Remove the screw from the crank arm assembly near the serrated shaft of the transducer.
S 034-009
(9)
Remove the screw from the bracket that holds the transducer in position.
S 034-010
(10)
Remove the transducer from the bracket.
TASK 31-31-10-404-011
3. Install the Rudder Pedal Position Transducer (Fig. 401)____________________________________________
A. Equipment
(1) 981-6301-002 Data Signal Display Unit (DSDU)
Alliedsignal Air Transport Avionics
P.O. BOX 97001
15001 NE 36TH ST
Redmond, WA 98073-9701
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MAINTENANCE MANUAL
(2)
A31007-49 Adapter Cable - Tester (recommended)
A31007-30 Adapter Cable - Tester (alternative)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 仪表 CHAPTER 31 - INSTRUMENTS 1(150)
