SY205 Flashcards

1
Q

VOR stations transmit beams, called _________, in every direction. In the T-6A, these signals are detected by the VOR receiver and displayed in the ________.

A

radials; EHSI

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2
Q

Since TACAN operates in the UHF frequency range, the T-6A VOR receiver cannot receive signals from VORTAC stations.

A

False

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3
Q

The VOR signal is received through the __________ antennas mounted on each side of the _________.

A

NAV/GS/ILS; vertical stabilizer

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4
Q

The ILS _________ provides course guidance to the runway centerline

A

localizer

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5
Q

The ILS localizer and glideslope signals are received and processed through the same antennas and receiver as the __________ system.

A

VOR

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6
Q

For ILS operation, the _____________ frequency is entered on the RMU as the primary navigation frequency

A

localizer

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7
Q

The DME system measures the time required for the transmitted signal to reach ground station and return, and calculates a ____________ distance in nautical miles from the aircraft to the ground station.

A

slant range

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8
Q

When a navigation facility with DME capability is tuned in the RMU, the DME information is provided ____________.

A

automatically to the EHSI

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9
Q

DME information displayed on the EHSI includes slant range distance, time-to-go to the station and _____________.

A

groundspeed

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10
Q

When DME hold is activated, the words “DME HOLD” will display on the ___________ below the primary nav frequency.

A

RMU

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11
Q

Controllers will assign the same Mode A transponder code to all aircraft under their control

A

False

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12
Q

Any aircraft within line of sight and equipped with a transponder set to the same code as either the ground station’s or airborne interrogation system’s query responds __________ with a coded signal to the system interrogation it

A

automatically to the EHSI

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13
Q

When you are requested to “SQUAWK ALTITUDE”, you press the mode select switch on the right side of the field to change the mode from “ON” to “___________”

A

ALT

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14
Q

When requested to “IDENT”, press the “IDT” button on the RMU. The ident signal will transmit for ________and then return to the previous mode.

A

20 seconds

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15
Q

TAS traffic warnings and advisories are displayed on the alternate engine data display (AEDD) in both cockpits.

A

False

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16
Q

TAS range selections are 3, 5, 10, 20 and ______ NM

A

40

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17
Q

Proximity traffic is displayed as a filled white diamond indicating the intruding aircraft is within +/- __________ feet relative altitude

A

1200

18
Q

In Above mode, traffic from 9000 feet above to 2700 feet below the aircraft is displayed

A

False

19
Q

The front cockpit GPS unit must be on and functioning for either the front or rear unit to be used

A

True

20
Q

The information on the right side of the Self Test display of the GPS should usually be correct since it is stored in ____________ memory

A

battery-backed

21
Q

If on the first GPS system self-test attempt, TEST FAIL replaces ANNUN ON on the Self Test display, you must notify maintenance

A

False

22
Q

The large outer knobs on the left and right sides of the panel are used to select the _________ for the left and right sides of the screen respectively (GPS)

A

page types

23
Q

To change an item on a displayed page, first press the CRSR button, then use the __________ knob to move the cursor to the field to be changed.

A

outer

24
Q

To declutter a display, you would press the _________ button

A

CLR

25
Q

The GPS can store up to ___________ flight plans in memory each of which can contain up to __________ waypoints

A

25; 30

26
Q

The DME system displays ____________ from the aircraft to the ground station

A

slant range distance in nautical miles

27
Q

When the GPS first activates, the screen will display the __________ page as the default page for the left side of the display, and the right side will display the waypoint page for the last active waypoint

A

NAV 2

28
Q

The 360 degree radial of each VOR station is oriented to __________

A

magnetic north

29
Q

Automatic altitude reporting is provided by the transponder mode ____________

A

C

30
Q

When the NAV source on the EHSI reads LOC and a glideslope signal is being received, a __________ will be presented on the right side of the instrument

A

glideslope scale and pointer

31
Q

To use DME from one navigation facility while on approach to another facility, you should __________ before switching the primary navigation frequency to the approach facility

A

press the DMEH button on the RMU

32
Q

To transmit a special pulse to aid in immediate identification on a controller’s scope, you press the ________ button on the RMU

A

IDT

33
Q

An advantage of the GPS flight plan function is that desired routes can be created before flight

A

True

34
Q

TAS detects and tracks other aircraft by interrogating their transponders and the analyzing the replies to determine range, bearing and relative __________

A

altitude

35
Q

What types of traffic does the TAS track?

A

The system provides two levels of warning, proximate traffic and traffic advisory. It also tracks ‘other traffic’ which is not considered a threat.

36
Q

How is proximity traffic indicated and at what are the parameters?

A

Proximity traffic is displayed as a filled white
diamond indicating the intruding aircraft is within
±1200 feet relative altitude and within 5 NM
range, but not considered a threat.

37
Q

How and when are Traffic Advisories showed on the TAS?

A
Traffic advisories (TA) are shown as a filled 
yellow circle. 
TAS displays a TA when the time to closest point of 
intruder aircraft approach is 15 to 30 seconds.
38
Q

What are the two Sensitivity Levels for the TAS?

A

Sensitivity Level A & B

39
Q

When is the TAS in sensitivity level A?

A

TAS is in Sensitivity Level A when the landing gear is extended.

40
Q

When is the TAS in sensitivity level B?

A

TAS is in Sensitivity Level B when the landing gear is retracted.

41
Q

In TAS mode B when will a TA will be issued?

A
  1. if current closing rate with intruder aircraft is maintained, vertical separation of less than 800 feet will occur in 30 seconds;
  2. Vertical separation from intruder is less than 800 feet and horizontal separation is less than 0.55 NM;
  3. Horizontal separation from non-altitude reporting intruder is within 20 seconds or 0.55 NM.
42
Q

When will a TA will be issued in TAS mode A?

A
  1. If TAS calculates that if current closing rate with intruder aircraft is maintained, vertical separation
    of less than 600 feet will occur in 20 seconds;
  2. Vertical separation from intruder is less than 600 feet and horizontal separation is less than 0.2