B737NG Warning Systems

Warning Systems 1. What is is the purpose purpose of the the Proximit Proximity y Switch Switch Electroni Electronicc Unit? Unit? Monitors the takeoff configuration warning. o Monitors the landing configuration warning. o Monitors the landing gear. o ll of the a!o"e. o #. $he PSEU PSEU system system on the ground ground monitor monitorss which which of the the followin following? g? $akeoff%landing $akeoff%landing configuration warnings o &anding gear  o ir%ground sensing o ll of the a!o"e. o '.  steady steady warning warning horn horn alerts alerts the crew crew when the landing landing gear gear is not down down and locked locked and a landing is attempted. $rue o (alse o ). When is the Proximi Proximity ty Switch Switch Electroni Electronicc Unit light light inhi!i inhi!ited? ted? *n flight. o (or 1 minute after landing. o ll of the a!o"e. o +. $he takeoff takeoff configurat configuration ion warning warning horn sounds when when the sta!ili, sta!ili,er er trim is not in in the takeoff  takeoff  range. $rue o (alse o -. Which of the the following following is an input into into the Stall Stall Management Management a aw /amper computers computers?? /*0U data. o ntiice controls. o ntiice controls. o ll of the a!o"e. o 2. Which of the the following following will cause cause acti"ation acti"ation of the takeoff takeoff configurat configuration ion warning warning system? system? &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/ 304E le"er in the /5W6 position. o 7. While While performing performing the &6/*68 &6/*68 checklist checklist the the PSEU light light illuminates illuminates on recall. recall. $his $his indicates9  normal condition o  fault is detected in the landing gear locking system or the air%ground sensing o systems $he landing gear configuration warning horn will sound upon landing. o  pro!lem exists in the PSEU system !ecause the light should !e inhi!ited in o flight :. *lluminati *llumination on of the PSEU light light on the the aft o"erhead o"erhead panel will acti"at acti"atee the MS$E0 MS$E0 ;U$*56 system. $rue o (alse. o

1<. $he landing gear configuration warning horn will acti"ate anytime a gear is not down and locked with the flaps set to 1+= one thrust le"er at idle and the other at a high power setting >a!o"e ') degrees9 $rue o (alse. o 11. $he 8PWS will pro"ide a warning%alert of slow descents into unprepared terrain while in the landing configuration. $rue o (alse. o 1#. $he SM/ computers recei"e inputs from9 nti ice controls. o /*0U@s o (M; o ll of the a!o"e. o 1'. $he 8round Proximity Warning System $est9 ;an !e performed only on the ground. o *s inhi!ited from liftoff to 1=<<< feet 0adio ltitude. o ;an !e performed only a!o"e 1=<<< feet 0adio ltitude. o ;an !e performed anytime. o 1). When are the 8PWS windshear warnings a"aila!le? 3elow 1+<< feet 8&. o 3elow #+<< feet 8&. o 3elow '<<< feet 8&. o 3elow +<<< feet 8&. o 1+. $he windshear warning mode of the 8PWS has priority o"er all other 8PWS modes. $rue o (alse. o 1-. When is a traffic ad"isory issued? When the other aircraft is within )< 6M. o When the other aircraft is within #< 6M. o When the aircraft is within )< seconds of the closest approach. o When the aircraft is within #< seconds of the closest approach. o 12. When is $;S inhi!ited? 3y windshear alerts. o 3y 8PWS. o t low altitudes where traffic a"oidance maneu"ers are inappropriate. o ll of the a!o"e. o 17. $he $akeoff ;onfiguration Warning horn sounds if9 Sta!ili,er trim is not in the green !and. o &eading edge flaps and trailing edge flaps are not in the correct position for o takeoff. Speed!rake le"er is not in the down position. o ll of the a!o"e is correct. o 1:. When does the &$ &E0$ light extinguish? When you le"el off at the selected altitude. o '<< feet !efore the selected altitude. o #<< feet !efore the selected altitude. o -<< feet !efore the selected altitude. o

#<. Aow can you silence the Mach%irspeed warning inflight? Slow the airplane speed to !elow Bmo%Mmo o Press the Mach%airspeed warning test switch o /escent to a lower altitude. o ;lim! to a higher altitude. o #1. $he mach%airspeed warning system can only !e checked on the ground9 $rue o (alse. o ##. While flying an *&S approach !elow 1=<<< feet 0adio ltitude= a 3E&5W 8%S alert occurs. $o cancel the alert9 ;orrect the flight path !ack to the glide slope. o Press either pilot@s 3E&5W 8%S P*6A*3*$ light o $he alert cannot !e cancelled o $he first two statements are correct. o #'. Which of the following will illuminate a landing gear configuration warning? &anding gear disagrees with the position of the landing gear le"er. o &anding gear is not down and locked. o Either or !oth thrust le"ers are at idle and the aircraft is !elow 7<< feet 8&. o ll of the a!o"e. o #). $he 8PWS pro"ides a C364 68&EC warning when the roll rate exceeds #+ degrees= '< degrees= and '+ degrees. $rue o (alse. o #+. Which of the following is 65$ a 8PWS mode? Excessi"e descent rate. o Excessi"e terrain closure. o Unsafe terrain clearance when in the landing configuration. o Windshear. o #-. While flying an *&S approach !elow 1= <<< feet 0adio ltitude= a 3E&5W 8%S alert occurs. $o cancel the alert9 Press 0E;&&. o Press either pilotD@s 3E&5W 8%S P*6A*3*$ light= or correct the flight path !ack o to the glide slope. $he alert cannot !e cancelled. o Select another mode on M;P. o $he "olume of the aural alert and the repetition rate increase as de"iation increases. #2. $he 8round Proximity Warning System $est9 ;an !e performed only on the ground. o *s inhi!ited from liftoff to 1= <<< feet 0 o ;an !e performed only a!o"e 1= <<< feet radio altitude. o ;an !e performed any time. o #7. $he Predicti"e Windshear alerts are issued9 When $E00 switch on E(*S control panel is pressed. o When WP$ switch on E(*S control panel is pressed. o utomatically !elow 1= #<< feet 0. o utomatically !elow #= +<< feet 0. o

#:. Predicti"e windshear alerts are triggered from9 E8PWS. o Weather 0adar System. o ural Warning Module. o '<. Ser"icea!ility of the tailskid cartridge is shown !y9  green decal. o  green indicator light o Wear dimples. o  green and red decal. o '1. *n the e"ent of an o"er rotation= which part of the tailskid structure contacts the runway? $he skirt. o $he fairing. o $he shoe. o $he cartridge. o '#. $he terrain displayed in the &ookhead $errain lerting system is generated from9 Weather 0adar correlated with *0S position. o 8PWS na" data !ase correlated with *0S position. o 8PWS na" data !ase correlated with 8PS position. o (M; na" data !ase correlated with 8PS position. o ''. When is a traffic ad"isory issued? When the other aircraft is within #< 6M o When the aircraft is within #< seconds of the closest approach. o When the other aircraft is within )< 6M. o When the aircraft is within )< seconds of the closest approach. o '). $he &ookhead $errain alerting system will show for terrain9 Within #=<<< feet 0. o 3elow 1=<<< feet !arometric altitude. o !o"e 1=<<< feet 0. o Within #=<<< feet !arometric altitude. o '+. *n what mode will the $;S automatically show if a $%0 occurs and the $(; switches are selected 5((. *n P&6= MP= B50 or PP modes o *n MP= center MP= P&6 or PP modes o *n center MP= B50 or PP modes. o *n MP= center MP= B50= or PP modes. o '-. What is correct a!out the color on the terrain display? /otted green  terrain #+<
 6one of the statements a!o"e are correct '7. 5n takeoff the config warning sounds. What can !e the cause? $railing edge flaps set to # o $railing edge flaps are in a skew condition o Sta!ili,er set in the takeoff range o $akeoff power not set on !oth engines o ':. When can you expect the E8PWS C(i"e AundredC call? When descending through the +<< feet am!er !and on the &$ tape on a sta!le o *&S approach. When descending through +<< feet 0 outside # dots of the &&H o *f descending through +<< feet 0 on a ;$ *** approach for the (&0E 0M o check. 5n an *&S approach descending through the am!er !and and the 8S is 1 dot from o the glideslope !eam. )<. $;S $ES$ is displayed on the na"igation display during the test followed !y $;S $ES$ PSSE/ or $;S $ES$ (*&E/. $his test remains in "iew for IIIII then !lanks. n aural annunciation sounds at the completion of the test. ' seconds o + seconds o 7 seconds o 1< seconds o )1. $he area>s inside the red lines indicate>s the pitch region>s to a"oid in order to resol"e the traffic conflict. $he airplane sym!ol must !e outside the $;S pitch command area>s to ensure traffic a"oidance. $rue o (alse o )#. $he 0 aural alert C;&*M3  ;&*M3 65WC means9 *ncrease clim! rate from initial pitch attitude. o ;lim! at displayed pitch. irplane clim!s through trafficFs altitude. o ;lim! at the displayed pitch. o 0e"ersal maneu"er from initial descent 0. o )'. When performance is limited= such as with an inoperati"e engine= to pre"ent recei"ing 0s  !eyond the airplaneFs capa!ilities9 Select &$ 5(( o Select $;S 5(( o Select $%0 o Select $ o )). ll $;S alerts are inhi!ited9 3elow approximately +<< feet radio altitude. o 3y 8PWS and windshear warnings. o 3elow approximately 1=1<< feet radio altitude. o Until the flaps are fully retracted after takeoff. o )+. $he $;S sym!ol for proximate traffic is9  red sJuare o n am!er circle o  white solid diamond o  white hollow diamond o )-.  $ sym!ol showing on the 6/ has= alongside it= a down arrow and C<2C. $his means9 o

$he traffic is descending at 2<