TM 55-1520-240-T7-9.4 INTEGRATED LOWER CONTROL ACTUATOR (lLCA)FAILS TEST 3 (CROSS EXTENSIBLE LINKTRANSDUCER NULL VOLTAGE TEST (SPARE))FAULT ISOLATION PROCEDUREINITIAL SETUPApplicable Configurations:AllTools:Aircraft Mechanic’s Tool Kit,NSN 5180-00-323-4692MultimeterMaterials:NonePersonnel Required:68H20 Aircraft Pneudraulics Repairer35K20 Avionic MechanicReferences:TM 55-1520-240-23Equipment Condition:Visual Check of Integrated Lower Control Ac-tuator (ILCA) Performed (Task 7-9.2)PER FORM CROSS FEEDBACKTRANSDUCER ADJUSTMENTTASK. REFER TO TM 55-1520-240-23. CAN TRANSDUCERNULL BE SET?DISCONNECT CONNECTORFROM TRANSDUCER THATFAlLED TEST. CHECK FOR CON-TINUITY BETWEEN CONNEC-TOR AND RECEPTACLE AT ENDOF ACTUATOR. REFER TO WIR-ING DIAGRAM 7-9.1. lS CON-TINUITY PRESENT ON ALLPOINTS BETWEEN CONNECTORAND RECEPTACLE?45 x 547-9.4D145-12462-SPAEND OF TASK7-225
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