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19 Cards in this Set
- Front
- Back
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NGs only: With flap 15 selected and landing gear UP, the landing gear warning horn cannot be silenced with the HORN CUTOUT switch if
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Either thrust lever is below 20 degrees or an engine not running and the other thrust lever is less than 34 degrees.
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Classics: The Take-off configuration warning is armed when on the ground and either or both Forward
Thrust levers are advanced for takeoff. The Take-off warning horn sounds when |
Stab trim is NOT in the green band range, or the trailing edge flaps are NOT in the Flaps 1 through 15 take-off range, or the leading edge FLAPS are NOT in the correct position for take-off or the speed brake is NOT in the DOWN position or the Parking Brake is set.
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Classics: The landing gear warning horn will sound if either or both thrust levers are approximately in the idle position and the flaps are in the
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1 through 10 position.
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Classics: The landing gear warning horn cannot be silenced by the Horn Cut-Out switch, regardless of Forward Thrust lever position, when the flaps are
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Greater than the 15 position.
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The Mach/Airspeed Aural Warning will sound when the Mach number or IAS exceeds
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0.82M or 340 Knots whichever is reached first.
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The Proximity Switch Electronic Unit (PSEU) light illuminates
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Is inhibited from thrust lever advance for take-off until 30 seconds after landing.
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EGPWS terrain display changes from dotted to solid yellow
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40 - 60 seconds from impact.
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The weather radar automatically begins scanning for windshear when:
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In flight below 2300ft RA.
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How many modes does the GPWS have?
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7
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The BELOW G/S mode is operational between _____ and _____ feet AGL.
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300; 1000
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Which inputs is not required for the windshear mode of the GPWS?
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Gear position.
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The MACH/AS warning makes a clacker sound.
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True.
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Which of the following IS NOT an input to the Stall Warning System?
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IRS.
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When can you get the pitch limit symbol?
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Only with flaps down.
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Which of the following is TRUE concerning the stall warning test?
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It can only be tested on the ground.
The test requires 115VAC. If the test is not successful, check that the leading edge devices are retracted. |
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Which of the following is TRUE concerning the FLASHING Altitude Alert light?
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It will flash when you deviate +/- 300 feet from the altitude set in the MCP.
You will get a STEADY light when within +/- 900 feet of the MCP altitude. The steady light will stay on until with +/- 300 feet. |
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Which of the following IS NOT a GPWS mode?
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Excessive rate of climb.
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The GPWS receives inputs from:
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L ADC, RA, ILS, IRS, gear and flap position.
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When is the Altitude Alert System inhibited?
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Flaps greater than 25 OR Glide Slope capture.
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