Warning System

Question 1

Pressing either MASTER CAUTION light extinguishes both lights and ______________.

Answer 1

resets the annunciator light for further cautions

Question 2

Single failures in dual/redundant systems do not illuminate MASTER CAUTION light, however, ___________ recalls the system failure.

Answer 2

pressing either system annunciator light panel

Question 3

Pressing ____________________extinguishes both Master Fire Warning lights, silences fire warning bell, and resets system for additional warnings.

Answer 3

either MASTER FIRE WARNING light or the fire warning bell cutout switch

Question 4

The Cabin Altitude and takeoff Configuration Warnings use __________ when activated.

Answer 4

the same intermittent tone

Question 5

The takeoff configuration warning horn sounds for the following conditions __________.

Answer 5

All answers are correct
() Stabilizer trim not set in the takeoff range, flaps not in the takeoff range, LE devices are not configured for takeoff, or the parking brake is set.
() Trailing edge flaps skew or asymmetry, speed brake lever not in the DOWN position,
or spoiler control valve is open providing pressured hydraulic fluid to the ground spoiler interlock valve

Question 6

________________ anytime the aircraft is below 800 feet AGL, in landing configuration and any gear not down and locked.

Answer 6

A steady horn sounds

Question 7

Pushing the Landing Gear Warning Cutout Switch silences landing gear configuration warning aural indications at ___________.

Answer 7

flaps up through 10 and below 800 feet RA

Question 8

The Proximity Switch Electronic Unit (PSEU) monitors _____________.

Answer 8

() all answers are correct
() takeoff and landing configuration warnings
() landing gear and air / ground sensing

Question 9

On the ground an illuminated Proximity Switch Electronic Unit (PSEU) indicates_____________.

Answer 9

() a fault is detected in the PSEU, or an overwing exit flight lock fails to disengage when commanded

Question 10

In flight the Proximity Switch Electronic Unit (PSEU) _____________.

Answer 10

is inhibited from thrust lever advance for takeoff until 30 seconds after landing

Question 11

As the throttles are advanced, the Takeoff Configuration Warning Light illuminates red, this indicates ______________.

Answer 11

the airplane is not configured correctly for takeoff

Question 12

An illuminated Cabin Altitude Warning Light indicates

Answer 12

at 10,000 feet if the cabin has not been pressurized

Question 13

Any time the maximum operating airspeed of Vmo/Mmo is exceeded

Answer 13

the Mach / airspeed warning system provides an aural warning (clacker)

Question 14

What is the indication of an impending stall?

Answer 14

an artificial stall warning device (stick shaker)

Question 15

The MACH AIRSPEED WARNING TEST switches and the STALL WARNING TEST switches ____________________.

Answer 15

are inhibited while airborne

Question 16

Altitude alerting is inhibited ____________________.

Answer 16

when trailing edge flaps are extended to 25 or greater, or while G/S captured

Question 17

_______ before reaching the selected altitude, a white box shows around the selected altitude display, the box around the current altitude becomes bold and a momentary tone sounds

Answer 17

900ft

Question 18

When deviating by ____ feet from the selected altitude, a momentary tone sounds, the current altitude box turns amber and ____________.

Answer 18

300; begins to flash

Question 19

Depressing the Takeoff Warning Test Switch will activate the takeoff warning horn if _____________________.

Answer 19

any of the flight control surfaces or their associated proximity switches are not in the proper position for takeoff

Question 20

Ground Proximity Warning System look ahead terrain and radio altitude based alerts are inhibited by _____________.

Answer 20

actual windshear warning

Question 21

The look ahead terrain alert “Terrain, terrain, pull up” will sound approximately _______ from the projected impact with the terrain shown in solid red on the navigation display.

Answer 21

20 to 30 sec

Question 22

The look ahead terrain alert “Caution, terrain” will sound approximately ________ from the projected impact with terrain shown in solid amber on the navigation display.

Answer 22

40 to 60 sec

Question 23

“Too low, terrain” aural alert occurs if the aircraft is at an unsafe terrain clearance at ________ with either the landing gear not down or flaps not in the landing configuration.

Answer 23

high speed

Question 24

The “__________” aural alert occurs when the aircraft experiences excessive altitude loss after a takeoff or go-around.

Answer 24

DON`T SINK

Question 25

The “GLIDESLOPE” aural alert occurs when the aircraft deviates below the glideslope. Volume and repetition rate _____________ as deviation _______________.

Answer 25

increase; decrease

Question 26

During takeoff and landing, new predictive windshear warning alerts are inhibited _____________.

Answer 26

between 100kt and 50ft RA

Question 27

An illuminated Inoperative (INOP) light on the Ground Proximity panel alerts the pilot that ________________.

Answer 27

a GPWS computer malfunction or power loss has ocurred

Question 28

The Ground Proximity System Test (SYS TEST) Switch is ______ in flight

Answer 28

inhibited

Question 29

Placing the Ground Proximity FLAP INHIBIT Switch to FLAP INHIBIT, inhibits _______________.

Answer 29

ground proximity TOO LOW FLAPS alert

Question 30

Placing the Ground Proximity TERRAIN INHIBIT Switch to TERRAIN INHIBIT, inhibits _______________.

Answer 30

look-ahead terrain alerts and terrain displays

Question 31

The weather radar automatically begins scanning for windshear when ____________________________.

Answer 31

all answers are correct:

• the thrust levers are set for takeoff
• in flight below 2300 ft RA

Question 32

Traffic advisories sound a(n) ____________ aural, and a message is annunciated on the traffic display

Answer 32

TRAFFIC TRAFFIC

Question 33

Resolution advisories provide aural warning, and____________________to maintain or increase separation from traffic.

Answer 33

maneuver guidance

Question 34

Placing the Transponder Mode Selector to TA (traffic advisory) ONLY __________________.

Answer 34

enables the display of traffic advisory targets

Question 35

Placing the Transponder Mode Selector to TA/RA __________________.

Answer 35

enables the display of traffic advisory targets and resolution advisory (RA)

Question 36

Pressing the Absolute Altitude Display Selector on the TCAS Controls (Transponder Panel) __________________.

Answer 36

displays absolute altitude of TCAS targets

Question 37

Placing the TCAS Altitude Range Switch to _______ sets TCAS display from 2700 feet below to 7000 feet above own aircraft.

Answer 37

above (ABV)

Question 38

The -800, and -900 series airplanes have a cartridge assembly (Tail Skid) to protect against a tail strike. When the warning decal is ______, the cartridge must be replaced.

Answer 38

all red