022.12 Alerting Systems, Proximity Systems Flashcards
GPWS Mode 1 is associated with (…). The initial aural alerts is (…), then if the situation intensifies an aural alert (…).
GPWS Mode 1 is associated with (Excessive Descent Rate). The initial aural alerts is (SINKRATE, SINKRATE), then if the situation intensifies an aural alert (WHOOP WHOOP PULL UP).
On a CS-25 aircraft, the regulatory margin between the stall and the stall warning is (…).
On a CS-25 aircraft, the regulatory margin between the stall and the stall warning is (5 kts or 5% of the CAS, whichever is greater).
On an EGPWS display, high and low density yellow refers to terrain, which is (…).
On an EGPWS display, high and low density yellow refers to terrain, which is (between 1000 ft above and 500 ft below the aircraft altitude, 250 ft below with gear extended).
Your aircraft is TCAS II equipped. To be able to generate a TA, the intruder must be at least equipped with a transponder mode (A/C/S).
Your aircraft is TCAS II equipped. To be able to generate a TA, the intruder must be at least equipped with a transponder mode (A).
Anti-collision logic of a TCAS II is based on (…).
Anti-collision logic of a TCAS II is based on (time).
For TCAS information on a ND, Threat Aircraft - Traffic Advisory (TA) are depicted as a(n) (…) of the colour (…). The traffic is (…-…) seconds from a collision.
For TCAS information on a ND, Threat Aircraft - Traffic Advisory (TA) are depicted as a(n) (solid (full) circle) of the colour (yellow or amber). The traffic is (35-45) seconds from a collision.
GPWS Mode 6 is associated with (…). The alert for the latter is (…).
GPWS Mode 6 is associated with (Callouts + Excessive Bank Angle). The alert for the latter is (BANK ANGLE, BANK ANGLE).
When a TCAS RA climb instruction is generated, it (does/does not) take into account the stall margin.
When a TCAS RA climb instruction is generated, it (does not) take into account the stall margin.
If immediate recognition and corrective or compensatory action by the crew is required, the FWS generates a (warning/caution/urgency/advisory) message.
If immediate recognition and corrective or compensatory action by the crew is required, the FWS generates a (warning) message.
When the EGPWS terrrain caution alert sounds, the pilot has (… to …) seconds left to respond.
When the EGPWS terrrain warning caution sounds, the pilot has (40 to 60) seconds left to respond.
For TCAS information on a ND, Threat Aircraft - Resolution Advisory (RA) are depicted as a(n) (…) of the colour (…). The traffic is (…-…) seconds from a collision.
For TCAS information on a ND, Threat Aircraft - Resolution Advisory (RA) are depicted as a(n) (solid (full) square) of the colour (red). The traffic is (20-30) seconds from a collision.
On an EGPWS display, the colour magenta refers to (…).
On an EGPWS display, the colour magenta refers to (areas without available terrain data in the EGPWS database).
GPWS Mode 5 is associated with (…). The first level aural alert is (…), then if the situation intensifies a second level alert (…).
GPWS Mode 5 is associated with (Excessive deviation below the glide slope). The first level aural alert is (GLIDESLOPE), then if the situation intensifies a second level alert (GLIDESLOPE, GLIDESLOPE).
If crew awareness is required and subsequent crew action may be required, the FWS generates a (warning/caution/urgency/advisory) message.
If crew awareness is required and subsequent crew action may be required, the FWS generates a (advisory) message.
If immediate crew awareness is required and subsequent crew action will be required, the FWS generates a (warning/caution/urgency/advisory) message.
If immediate crew awareness is required and subsequent crew action will be required, the FWS generates a (caution) message.