Pressing either MASTER CAUTION light extinguishes both lights and ______________. resets the annunciator light for further cautions places the associated system into the alternate mode places the associated system into the standby mode.
Single failures in dual/redundant systems do not illuminate MASTER CAUTION light, however, ___________ recalls the system failure. pressing either MASTER CAUTION light pressing either MFD switch pressing either system annunciator light panel.
Pressing ____________________extinguishes both Master Fire Warning lights, silences fire warning bell, and resets system for additional warnings. either the MASTER FIRE WARNING light or the MASTER CAUTION light either the MASTER CAUTION light, MASTER FIRE WARNING light, or the BELL CUTOUT switch either MASTER FIRE WARNING light or the fire warning bell cutout switch.
The Cabin Altitude and takeoff Configuration Warnings use __________ when activated. the MASTER CAUTION light the same intermittent tone either the MASTER CAUTION light, or the MASTER FIRE WARNING light and bell.
The takeoff configuration warning horn sounds for the following conditions __________. 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
All answers are correct.
______________ anytime the aircraft is below 800 feet AGL, in landing configuration and any gear not down and locked. A steady horn sounds The MASTER CAUTION light illuminates The MASTER FIRE WARNING light and bell sound.
Pushing the Landing Gear Warning Cutout Switch silences landing gear configuration warning aural indications at ___________. flaps up through 10 and below 800 feet RA flaps 15 through 25 and below 800 feet RA flaps 30 through 40 and below 800 feet RA.
WARN6.150.8
The Proximity Switch Electronic Unit (PSEU) monitors _____________. takeoff and landing configuration warnings landing gear and air / ground sensing all answers are correct.
On the ground an illuminated Proximity Switch Electronic Unit (PSEU) indicates_____________. a fault is detected in the PSEU, or an overwing exit flight lock fails to disengage when commanded an EEC fault has occurred and automatic switching to the alternate mode has occurred
all answers are correct.
In flight the Proximity Switch Electronic Unit (PSEU) _____________. will illuminate for an air / ground sensing disagree
will illuminate during a landing gear configuration warning is inhibited from thrust lever advance for takeoff until 30 seconds after landing.
As the throttles are advanced, the Takeoff Configuration Warning Light illuminates red, this indicates ______________. the airplane has a high cabin altitude
the airplane is not configured correctly for takeoff
the airplane has encountered windshear.
An illuminated Cabin Altitude Warning Light indicates at 10,000 feet if the cabin has not been pressurized at 12,000 feet if the cabin has not been pressurized at 14,000 feet if the cabin has not been pressurized.
Any time the maximum operating airspeed of Vmo/Mmo is exceeded, the Mach / airspeed warning system provides an aural warning (clacker)
a red airspeed warning is displayed across the lower EADI
all answers are correct.
What is the indication of an impending stall? an automated aural warning horn an automated aural “stall, stall, stall” annunciated over the aft overhead speaker
an artificial stall warning device (stick shaker).
The MACH AIRSPEED WARNING TEST switches and the STALL WARNING TEST switches ____________________. must be tested after complete IRS alignment
reset the stall warning computer for non-icing conditions are inhibited while airborne.
Altitude alerting is inhibited ____________________. when the trailing edge flaps are extended to 25 or greater, or while G/S is captured, or while in VNAV PATH on an RNAV approach
when the trailing edge flaps are extended to 25 or greater, or while G/S is captured
below 2500 feet.
_______ 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 500 feet 900 feet
1000 feet.
When deviating by ____ feet from the selected altitude, a momentary tone sounds, the current altitude box turns amber and ____________. 300; begins to flash 300; shows steady
300; extinguishes.
Depressing the Takeoff Warning Test Switch will activate the takeoff warning horn if _____________________. any of the flight control surfaces or their associated proximity switches are not in the proper position for takeoff
both engines are not running all answers are correct.
Ground Proximity Warning System look ahead terrain and radio altitude based alerts are inhibited by _____________. altitude loss after takeoff actual windshear warning excessive terrain closure rate.
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. 20 to 30 secs 40 to 60 secs more than 60 secs.
The look ahead terrain alert “Caution, terrain” will sound approximately ________ from the projected impact with terrain shown in solid amber on the navigation display. 20 to 30 secs 40 to 60 secs more than 60 secs.
“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. high speed low speed stall speed.
The “__________” aural alert occurs when the aircraft experiences excessive altitude loss after a takeoff or go-around. “GLIDESLOPE”
“TOO LOW, FLAPS”
“DON’T SINK”.
The “GLIDESLOPE” aural alert occurs when the aircraft deviates below the glideslope. Volume and repetition rate _____________ as deviation _______________. increase; decrease decrease; increase increase; increase.
During takeoff and landing, new predictive windshear warning alerts are inhibited _____________. passing 80 knots between 100 knots and 50 ft RA continuously.
An illuminated Inoperative (INOP) light on the Ground Proximity panel alerts the pilot that ________________. the flap inhibit switch needs to be placed to flap inhibit
a GPWS computer malfunction or power loss has occurred.
the GPWS computer has automatically switched to the alternate mode.
The Ground Proximity System Test (SYS TEST) Switch is ______ in flight.
inhibited operative delayed by 30 seconds.
Placing the Ground Proximity FLAP INHIBIT Switch to FLAP INHIBIT, inhibits _______________. all ground proximity alerts ground proximity TOO LOW GEAR alert ground proximity TOO LOW FLAPS alert.
Placing the Ground Proximity TERRAIN INHIBIT Switch to TERRAIN INHIBIT, inhibits _______________. ground proximity TOO LOW GEAR alert
look-ahead terrain alerts and terrain displays
all answers are correct.
The weather radar automatically begins scanning for windshear when ____________________________. the thrust levers are set for takeoff
in flight below 2,300 feet RA
all answers are correct.
Traffic advisories sound a(n) ____________ aural, and a message is annunciated on the traffic display. “TRAFFIC TRAFFIC”
“WHOOP, WHOOP, PULL UP”
“OBSTACLE, OBSTACLE”.
Resolution advisories provide aural warning, and____________________to maintain or increase separation from traffic. an airspeed restriction or maneuver on the EADI
maneuver guidance all answers are correct.
Placing the Transponder Mode Selector to TA (traffic advisory) ONLY __________________.
enables the display of traffic advisory targets and resolution advisory (RA) targets enables the display of traffic advisory targets disables the display of traffic advisory targets.
Placing the Transponder Mode Selector to TA/RA __________________. enables the display of traffic advisory targets and resolution advisory (RA) targets
enables the display of traffic advisory targets disables the display of traffic advisory targets.
Pressing the Absolute Altitude Display Selector on the TCAS Controls (Transponder Panel) __________________. displays absolute altitude of terrain displays absolute altitude for RA TCAS targets only displays absolute altitude of TCAS targets.
Placing the TCAS Altitude Range Switch to _______ sets TCAS display from 2700 feet below to 7000 feet above own aircraft. Above (ABV)
Normal (N)
Below (BLW).
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. red and green
all red
all yellow.
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