B737NG Warning Systems

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    Warning Systems

    1. What is the purpose of the Proximity Switch Electronic Unit?

    o Monitors the takeoff configuration warning.

    o Monitors the landing configuration warning.

    o Monitors the landing gear.

    o ll of the a!o"e.

    #. $he PSEU system on the ground monitors which of the following?o $akeoff%landing configuration warnings

    o &anding gear

    o ir%ground sensing

    o ll of the a!o"e.

    '. steady warning horn alerts the crew when the landing gear is not down and locked and alanding is attempted.

    o $rue

    o (alse

    ). When is the Proximity Switch Electronic Unit light inhi!ited?

    o *n flight.

    o (or 1 minute after landing.o ll of the a!o"e.

    +. $he takeoff configuration warning horn sounds when the sta!ili,er trim is not in the takeoff

    range.

    o $rue

    o (alse

    -. Which of the following is an input into the Stall Management aw /amper computers?

    o /*0U data.

    o ntiice controls.

    o ntiice controls.

    o ll of the a!o"e.

    2. Which of the following will cause acti"ation of the takeoff configuration warning system?o &eading edge flaps in the extend position and trailing edge flaps at flaps +.

    o &eading edge flpas in the full extend position and trailing edge flaps at 1+.

    o Spoilers partially extended.

    o SPEE/ 304E le"er in the /5W6 position.

    7. While performing the &6/*68 checklist the PSEU light illuminates on recall. $his

    indicates9

    o normal condition

    o fault is detected in the landing gear locking system or the air%ground sensing

    systems

    o $he landing gear configuration warning horn will sound upon landing.

    o pro!lem exists in the PSEU system !ecause the light should !e inhi!ited inflight

    :. *llumination of the PSEU light on the aft o"erhead panel will acti"ate the MS$E0;U$*56 system.

    o $rue

    o (alse.

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    1a!o"e ') degrees9

    o $rue

    o (alse.

    11. $he 8PWS will pro"ide a warning%alert of slow descents into unprepared terrain while in

    the landing configuration.

    o $rue

    o (alse.1#. $he SM/ computers recei"e inputs from9

    o nti ice controls.

    o /*0U@s

    o (M;

    o ll of the a!o"e.

    1'. $he 8round Proximity Warning System $est9

    o ;an !e performed only on the ground.

    o *s inhi!ited from liftoff to 1=

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    #

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    o 6one of the statements a!o"e are correct

    '7. 5n takeoff the config warning sounds. What can !e the cause?o $railing edge flaps set to #

    o $railing edge flaps are in a skew condition

    o Sta!ili,er set in the takeoff range

    o $akeoff power not set on !oth engines

    ':. When can you expect the E8PWS C(i"e AundredC call?

    o When descending through the +

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    o $he traffic is descending at 2