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T h e speed b r a k e s a r e i s o l a t e d fro m system pressure when the speed brake s\Nit c h i s in hold o r selecting S P D B K E M R R E T R o n t h e e mergency flight c o n t ro l pan e l . Flaps can be FLAP from t h e l e ft hydrau l i c system E M E R R E T R o n t he emergency HYD R AULI C POWER SUPPLY SYSTEM c o n t ro l - emergency wheel associated acc u mulators T w o hydraul i c pressure gauges (46, FO- l ) per­ m i t the p i l ot to cont i n u ou s l y m o ni t o r both hydraulic H Y D SYS L and systems , These gauges arc H Y D S Y S R a n d i n dicate p r e s s u r e i n T h e gauges are powered b y the i ns t r u m e n t t ra n s former b u s .

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. " ;;; " o ' � CONTROL snCK / ". ". , ) ' ". " ,, , ... ,, " ... " / ,, '" ". /" , / ,.. / I iO\ , ....

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 " ... ,,/' / , ;'" ' "..... / ... - ,,'" , , ........

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