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FAULT ISOLATION/MAINT MANUAL
PUSHRODS PEDAL RUDDER ESEE E HOLE RIG PIN SEE
113AL COMPARTMENT ACCESS, FORWARD EQUIPMENT DSEE HOUSING RUDDER PEDAL HOUSING COVER FSEE JACKSHAFT ASSEMBLY QUADRANT AND RUDDER FORWARD RUDDER PEDAL SHAFT SUPPORT PEDAL RUDDER
PEDALS RUDDER INBD
FWD D RUDDER PEDAL HOUSING
ARMS RUDDER PEDAL
HOLE R-1 RIG PIN
INBD
PUSHRODS RUDDER PEDAL FWD
BRAKE PUSHRODS NOSE WHEEL INTERCONNECT STEERING INBD FWD
RUDDER FORWARD QUADRANT AND CAPTAIN'S RUDDER PEDALS
JACKSHAFT ASSEMBLY EF Rudder and Rudder Trim Control System - Component Location Figure 102 (Sheet 2)
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FAULT ISOLATION/MAINT MANUAL
FIN INSPECTION
OPENING FROM
THE STABILIZER
COMPARTMENT
AFT SERVICE
ACCESS PANEL,
311AL
RUDDER
YAW DAMPER 324CL
SUMMING LEVER RUDDER PCA
ASSEMBLY SEE K SHT 4
SEE J SHT 4
RUDDER RATIO CHANGER
324BL MECHANISM
324AL SEE I SHT 4
AFT QUADRANT,
FEEL, CENTERING, RUDDER TRIM ACTUATOR,
AND TRIM M515
MECHANISM
SEE H CONTROL RODS TO
THE RUDDER RATIO
CHANGER
MECHANISM
SEE I SHT 4
RUDDER
CONTROL
CABLES
(REF) CONTROL ROD
TO THE
AUTOPILOT
ROLLOUT
GUIDANCE
AFT SERVO (REF)
QUADRANT FEEL AND
ASSEMBLY CENTERING
FWD SPRING
AFT QUADRANT, FEEL, CENTERING, AND TRIM MECHANISM H Rudder and Rudder Trim Control System - Component LocationFigure 102 (Sheet 3)
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FAULT ISOLATION/MAINT MANUAL
RRCA SCREEN (IN THE HYDRAULIC RRCA
LINE HIDDEN FROM VIEW) SOLENOID
VALVE RUDDER RATIO CHANGER POGO ROD
RUDDER RATIO CHANGER ACTUATOR (RRCA)
SHEAR PIN
CONTROL RODS
M626 TO THE RUDDER PCA
RUDDER RATIO CHANGER POGO ROD
YAW DAMPERRRCA SUMMING LEVEREHSV
ASSEMBLY RUDDER RATIO CHANGER LVDT, TS194
CONTROL RODS FROM THE AFT QUADRANT, FEEL CENTERING AND TRIM MECHANISM (REF)
RUDDER RATIO CHANGER MECHANISM
I CONTROL ROD
YAW DAMPER TO THE RUDDERSERVOS RATIO CHANGER(REF) MECHANISM (REF)
CONTROL ROD YAW DAMPER
TO THE UPPER
BIAS POGO
PCA (REF) (REF)
PCA PRESSURE DIFFERENTIAL SENSOR (REF)
YAW DAMPER SUMMING LEVER ASSEMBLY
J
PCA
CONTROL ROD TO THE LOWERPCA (REF)
MIDDLE RUDDER POWER CONTROL ACTUATOR (PCA)
K
Rudder and Rudder Trim Control System - Component Location (Details from Sht 3) Figure 102 (Sheet 4)
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RUDDER TEMPERATURE COMPENSATING
LINKAGE
Rudder and Rudder Trim Control System - Component Location
Figure 102 (Sheet 5)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 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 飞行操纵 FLIGHT CONTROLS 1(143)
