B737 Warnings

The PSEU system on the ground monitors which of the following?. Takeoff/landing configuration warnings. Landing gear. Air/ground sensing. All of the above.

Which of the following will cause activation of the takeoff configuration warning horn?. Leading edge flaps in the extend position and trailing edge flaps at flaps 5. Leading edge flaps in the full extend position and trailing edge flaps at flaps 15. Spoilers not down with the speed brake lever in the DOWN position. SPEED BRAKE lever in the DOWN position.

Which of the following are correct with respect to Predictive Windshear Alerts. The weather radar provides windshear alerts for windshear events containing some level of moisture or particulate matter. The weather radar detects microbursts and other windshears with similar characteristics. The weather radar does not provide alerting for all types of windshear. ALL are correct.

While performing the LANDING checklist the PSEU light illuminates on recall. This indicates. a normal condition. a fault is detected in the landing gear locking system or the air/ground sensing system. the landing gear configuration warning horn will sound upon landing. a problem exists in the PSEU light, because this light should be inhibited in flight.

The mach/airspeed warning system can only checked on the ground. True. False.

The stall management yaw damper (SMYD) computers determine when the stall warning is required based on which of the following?. Anti-ice controls. ADIRU output. FMC outputs. All of the above.

How can you silence the Mach/airspeed warning in fight?. Reduce the airplane speed to below Vmo/Mmo. Press the Mach/airspeed warning test switch. Disconnect the autothrottle system. Press the Mach/airspeed override switch.

While flying an ILS approach 1.3 dots below glide slope, a BELOW G/S alert occurs. To cancel or inhibit the below glide slope alert: Correct the flight path back to the glide slope. Push either pilot's BELOW G/S P-INHIBIT light while in the alerting area. Push the BELOW G/S light when below 1,000 feet. Both a and c are correct.

The Ground Proximity Warning System Test is: inhibited in flight. performed from lift-off to 1000 feet radio altitude. performed momentarily on the ground, or above 1000 feet radio altitude in flight. performed anytime.

An intermittent takeoff configuration warning horn sounds if: stabilizer trim is not set in the takeoff range,. the leading edge flaps and trailing edge flaps are not configured for takeoff. the SPEED BRAKE lever is not in the DOWN position. All of the above are correct.

The GPWS terrain database, look-ahead terrain alerting, and terrain display do NOT account for man-made obstructions. True. False.

The Ground Proximity Warning System provides alerts for all of the following except: excessive rate of descent. unsafe terrain clearance when not in the landing configuration. terrain clearance is guaranteed with a ground proximity alert. excessive deviation, below an ILS glide slope.

When deviating by 200 feet from the selected altitude, a momentary tone sounds and the current altitude box turns amber, and begins to flash. Until the altitude deviation becomes less than 200 feet. Until a new altitude is selected. Until the altitude deviation becomes more than 900 feet. all are correct.