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1�I REVERSION " ' -< 1;j ARTIFlCIAL FEEL DEVICE, CAM AND SPRING-LOADED fOLLOWER SIMULATE PITCH! -" R @ L C! PWR EMER {L ! com � ( YAW CONTROL SYSTEM SCH EMATIC '" .. :\��'��L�\::��:�� THE INTEGRAL STABIUTY AUGMENTAnON SYSTEM iSA$) IS INCLUDED IN THE LINKAGE AT THE HYDRAULIC ACTUATORS IN THE EVENT OF HYDRAULIC FAILURE, AUTOMATICAllY ''0'' SIVITCH ... com (J THE MRFCS LOCK PROVIDES OIRECT MlCHANlCAl UNKAGl TO THE RUD[)(R " c ;; � RUDDER PEDALS " ... ,,/' / , ;'" ' ".....

ELEVATOR ACTUATOR AND LIN'ACTION KAGE SHOIVlNG ' GEARED' / ' , ' ' ,, ' ... , " -- ... ' ; ' , ... _ _ - ... , .... ' '" '" - , "' ... ' ' , if - , , ... .... ' , / , , ... / l> CAM & FOlLOIVfR SIMULATE ... __ / TRIM SWITCHES (SEE 0. �- - --\ �? � y .. , .... Cj - -l '.... - , NOTE THAT THEARETWOPOWERED ELIVATORBY ACTUATORS IHYDRAULI NDEPENDENTC PRESSURE SOURCES OF .... -"' ,'" � J ARTIACISPRIAL FEELNG LOADED DEVICE; ... � -- - - - ... POSI T - - � NOSE ON ] PWR EMER8 � � DfVlNCOfE ACTUATOR/ OVERRIDE NOSE UP TRIM ACTUATOR �� � 'J ,>-TRIM TAB, 02; " CONTROL STICK If M TABS WITPRESS IS LOST, HWillElECTRO-MECH TRIACTUATORS BY NORMBElOW)OR [MERBE CONTROLlED CROSSOVERS -tIEXCESSI THER VORE LOAD BOTH, WILEAVI LL SHEAR AT NG OPPOSITE SIDE FREE I ------ � {� • 'I'@J � FEEl.

When the T10 TRIM buuon is released, the TAKEOFF TRIM light will go off. Takeoff Trim light In the event of loss of one SAS channel or one hydraulic power supply, 500]0 yaw trim authority is retained through the powered SAS channel. TAKEOFF TRIM CONTROL SYSTEM When the TID TRIM button (figure 1-19) is de­ pressed, the pitch and roll trim motors and the two elevator tab trim motors are driven to neutral. With the TID TRIM button depressed, the yaw trim knob in neutral seuing, and the five trim motors at neutral setting, the TAKEDFF TRIM light comes on.

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A-10A Flight Manual


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