5-29. What component contains the operating switches and indicators for the AN/ASQ-81 MAD system? 1. AM-4535 2. DT-323 3. DT-355 4. C-6983 IN ANSWERING QUESTIONS 5-30 THROUGH 5-32, REFER TO FIGURE 4-27 IN THE TEXTBOOK. 5-30. 5-31. 5-32. 5-33. 5-34. What indicator number indicates an amplifier failure? 1. No. 1 2. No. 2 3. No. 3 4. No. 4 What knob inhibits system output when depressed? 1. 2. REC ZERO 3. BANDPASS (right) 4. BANDPASS (left) What knob is used to select sensitivity ranges or self-test? 1. 2. REC ZERO 3. BANDPASS (right) 4. BANDPASS (left) The SAD inhibit signal is generated in cases of excessive aircraft pitch and yaw rates. 1. True 2. False Compensation currents for the MAD boom compensation coils are provided by what component of the AN/ASA-65 magnetic compensator group? 1. AM-6459 2. C-8935 3. CP-1390 4. ID-2254 5-35. The potentiometers for adjusting the maneuver and correlated signals into compensating terms are located on what AN/ASA-65 system component? 1. AM-6459 2. C-8935 3. CP-1390 4. ID-2254 IN ANSWERING QUESTIONS 5-36 THROUGH 5-38, REFER TO FIGURE 4-28 IN THE TEXTBOOK. 5-36. The adjustment index for the potentiometer in the transverse, longitudinal, and vertical magnetometer circuits is provided by what set of index indicators? 1. The top three 2. The bottom three 3. The top six 4. The bottom SIX 5-37. Except when compensation is required, in what position must the MAG TERM knob be? 1. UP 2. DOWN 3. ON 4. OFF 5-38. What switch directly to selected? provides voltage the servomotor 1. POWER-OFF 2. UP-DOWN 3. RATE 4. SERVO-OFF 5-39. Three coils oriented to sense magnetic strength in each of the basic axes are contained in what component of the AN/ASA-65 magnetic compensator group? 1. DT-355 2. CP-1390 3. ID-2254 4. DT-323 34