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Descending through light or trace icing with FQR greater than ________ pounds may result in engine flameout. A. 2000 B. 5000 C. 700 D. 3000 - answerB The effectiveness of the anti-icing system to prevent ice accumulation has not been . Current restrictions assume the anti-icing system provides full prevention of ice accumulation A. TRUE B. FALSE - answerB The _____________ function used for IP links establishes the creation of VoIP stream(s) between the UA and MCS. A. Call Home B. Phone Home C. Text Home D. DAMA override - answerA Which of the following is not considered a BLOS voice or data link on the MQ-4C. A. UHF satellite communications (SATCOM) B. Common data link (CDL) C. International Maritime Satellite (INMARSAT) D. Wideband SATCOM (WBSC) - answerB Start Bus A or Start Bus B power failure through the AFT PDC will be indicated by an ___________. A. IMMC 78 B. IMMC 80 C. ELEC PWR 34 D. ELEC PWR 202 - answerA _________ commands are sent to the UA continuously and rapidly until the UA acknowledges, or the AVO commands the UAVC2 to stop sending the command. A. Detailed Status B. Machine Gun C. Confirmed D. Heading and altitude - answerB In most circumstances, the safest course of action when the UA has experienced an engine malfunction is to _______________________________________ A. secure the engine when within glide range B. continue engine operation through landing C. enter climb mode D. none of these - answerB The risk of a seized engine damaging the airframe and jeopardizing UA airworthiness is ______________ A. likely B. impossible C. probable D. minimal - answerD _________________ failures may result in misleading sensor readings being reported to the IMMC and erroneous fault codes reported on the AVC2 display. A. Engine B. Electrical C. Comms sytem D. ECS - answerB The FAF altitude is approximately 2,400 feet above the touchdown elevation for a ______° glide slope. A. 3 B. 3.75 C. 4.5 D. 5.75 - answerC If the UA is in an engine out CONT-3 approach, the FAF waypoint altitude is approximately 3,060 feet above the touchdown waypoint elevation and the glide slope is _______°. A. 3 B. 3.75 C. 4.5 D. 5.75 - answerD A waveoff may be commanded from the MCS at any time up until the aircraft reaches ______ ft AGL or when the UA transitions
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