With both engines operating and one forward thrust lever set below approximately 20 degrees thrust lever angle, the landing gear warning horn can be silenced with the landing gear warning HORN CUTOUT switch:
The Stall Warning requirement is determined by what system component?
Two independent, identical stall management yaw damper (SMYD) computers provide outputs for all stall warning to include stick shaker and signals to the pitch limit indicator and airspeed displays and the GPWS windshear detection and alert.
Altitude alerting, consisting of a tone and highlighted boxes, occurs at a set distance before reaching the selected attitude. How many feet before the selected altitude do the altitude alert highlighted boxes no longer show?
The TCAS symbol for proximate traffic is:
The windshear warning mode of the GPWS has priority over all other GPWS modes.
A TA symbol showing on the ND has, alongside it, a down arrow and '-07'. This means:
Once an alert has occurred for deviating from the selected altitude, how is it cancelled?
RAs can only be generated if the other airplane has a working:
The Ground Proximity Warning System Test:
When carrying out the Stall Warning Test, which of the following statements is correct?
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At what altitude are the TCAS INCREASE DESCENT RAs inhibited?
Takeoff configuration warning is armed when the airplane is on the ground and either or both forward thrust levers are advanced for takeoff.
What is correct about the color on the terrain display?
Crew are warned of exceeding the maximum allowed airspeed by which of the following?
The GPWS provides a 'BANK ANGLE' warning when the roll rate exceeds 25 degrees, 30 degrees, and 35 degrees.
The predictive windshear aural alerts will be heard through flightdeck speakers and the headsets at a pre-set volume. They cannot be controlled or turned off by the crew.
The Look-Ahead Terrain alerting system will show for terrain:
Pushing the ground proximity BELOW G/S P-INHIBIT light cancels or inhibits the alert when below 1,000 feet RA.
What is the first Radio Altitude Callout given during the approach?
On airplanes with Airspeed Low aural, an alert 'AIRSPEED LOW, AIRSPEED LOW' provides the flight crew with low airspeed awareness. The aural annunciates when the current airspeed decreases into the minimum maneuver speed amber bar.
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How far from projected impact will the 'TERRAIN, TERRAIN, PULL UP' aural warning be given?
20 to 30 seconds from projected impact with terrain shown solid red on the navigation display (in expanded MAP, center MAP, expanded VOR, or expanded APP modes only).
The terrain displayed in the Look-Ahead Terrain Alerting system is generated from:
When performance is limited, such as with an inoperative engine, to prevent receiving RAs beyond the airplane’s capabilities:
The stall warning test can only be carried out on the ground, the No1 and No2 systems must be carried out separately to ensure the clacker sounds when each system is tested.
Which of the following will cause activation of the takeoff configuration warning system?
The PSEU light, located on the forward overhead panel, will illuminate on the ground if a fault is detected in the PSEU or if an overwing exit flight lock fails to disengage when commanded.
All TCAS voice annunciations are inhibited below approximately:
When configured for landing, the GPWS will NOT alert if attempting an off-airport landing.
The Cabin Altitude and Takeoff Configuration Warnings use the same intermittent tone when activated.
The PSEU light will illuminate along with a Master Caution and an OVERHEAD annunciator light, under which of the following situations?
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Which statement is correct?
When will the landing gear config warning horn give an intermittent warning sound?
A steady warning horn is provided to alert the flight crew whenever a landing is attempted and any gear is not down and locked.
Which two displays cannot be selected and shown simultaneously on the Navigation DU?
RAs are indicated by one or more aural listed in the RA aural table. The TRAFFIC annunciation and RA symbol which depicts the traffic’s relative bearing, range, altitude, and vertical motion are on the navigation display similar to the TA symbol.
Serviceability of the tailskid cartridge is shown by:
The tail skid is serviceable when the cartridge warning decal shows both green and red. The green disappears gradually as the cartridge is crushed. When the warning decal is all red, the cartridge must be replaced.
Illumination of the PSEU light on the aft overhead panel will activate the MASTER CAUTION system.
Vertical motion information is indicated by an arrow depicting a climb or descent if a change of greater than _____ is detected.
How can the Fire Warning Bell be silenced on the flight deck?
As well as providing outputs for all stall warnings, the SMYD computers also provide outputs for GPWS Windshear Detection and Alert.
Altitude alerting occurs when approaching or departing from the MCP selected altitude. When is the altitude alerting system inhibited?
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How are crew alerted to a deviation from the selected altitude?
The EGPWS displays terrain within 2,500 feet of the aircraft barometric altitude on the Navigation display.
When is a traffic advisory issued?
At what altitude (in feet) do the RA callouts begin?
In the event of an over rotation, which part of the tailskid structure contacts the runway?
The shoe is what contacts the runway in the event of an over rotation. The shoe surface displays 'wear dimples' which serve as a reference for shoe replacement.
When are the GPWS windshear warnings available?
Terrain ahead of the airplane may exceed available climb performance. A ground proximity alert does not guarantee terrain clearance.
The RA aural alert 'CLIMB – CLIMB NOW' means:
What is significant about the layout of the Annunciator Panel lights.
Predictive windshear alerts are triggered from the:
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In what mode will the TCAS automatically show if a TA/RA occurs and the TFC switches are selected OFF.
TCAS TEST is displayed on the navigation display during the test followed by TCAS TEST PASSED or TCAS TEST FAILED. This test remains in view for _____ then blanks. An aural annunciation sounds at the completion of the test.
On takeoff the config warning sounds. What can be the cause?
The TCAS system generates a Traffic Advisory, whenever another aircraft is what distance from point of closest approach?
The Stall Warning System Stick Shaker can be tested by pressing the STALL WARNING TEST buttons on the AFT overhead panel. Pressing No1 switch will activate the Captain's Stick Shaker and the Captain's column will vibrate. Pressing N02 switch will activate the FO's Stick Shaker and the FO's column will vibrate.
Which of the following is NOT a GPWS mode?
The EGPWS contains a terrain database, which it uses for look-ahead terrain alerting. Which of the following statements is correct for this terrain database?
What does the TCAS Symbol that is a solid amber circle indicate?
Which systems does the Proximity Switch Electronic Unit (PSEU) monitor
When testing the Mach-Airspeed warning system in flight, the No1 and No2 systems must be tested separately to identify that the clacker sounds for both systems independently.
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Which of the following statements is true for the CABIN ALTITUDE Warning?
The Predictive Windshear alerts are issued:
While performing the LANDING checklist the PSEU light illuminates on recall. This indicates:
The GPWS will provide an aural alert of 'BANK ANGLE, BANK ANGLE' under which of the following circumstances?
Once sounded, the alert is silent for that bank angle (35, 40, or 45 degrees) until the system is reset by decreasing bank angle to 30 degrees or less.
While flying an ILS approach below 1, 000 feet Radio Altitude, a BELOW G/S alert occurs. To cancel the alert:
The volume of the aural alert and the repetition rate increase as deviation increases.