Please provide explenation for the answer Thank you 3. In a compass coupler type

Question

Please provide explenation for the answer
Thank you 3. In a compass coupler type system, moving a switch to the position labelled "DG" will a. necessitate manual corrections. b. activate the stepper motor control. c. move the differential synchro rotor d. allow the pilot to change his or her heading. 4. On the captain's instrument panel of a Boeing 747, the auto throttle system and autopilot system warning lights are positioned directly below a. photoelectric illumination control cells. b. the airspeed/mach meter. c. two blank windows. d. the barometric altimeter 5. A flux valve a. is used primarily to correct compass source information. b. is free of northerly turning error c. generates signals comparable to a synchro rotor d. directly feeds the cockpit indicator. 6. Whether or not the aircraft has passed the nearest VOR station is indicated on a radial pictorial indicator by a. a line. b. a series of dots. c. an arrowhead. d. There is no indication of whether the aircraft has passed the station. 7·The main difference between True Heading (HDG) and Ground Track Angle (TK) has to do with a. true north vs. magnetic north. b. the difference between the aircraft's present position and desired track. calculations based on aircraft centerline vs. successive ground position points. present position of aircraft vs. next way point. c. d.

Explanation / Answer

13 d

14 a

15 a

16 c

17 a

Related Questions

Navigate

• Browse (All)
• Browse P
• Subjects

---

---

Integrity-first tutoring: explanations and feedback only — we do not complete graded work. Learn more.