SY201/202 Flight Instruments 1&2 Flashcards

0
Q

VOR stations transmit signals which are subject to ____-___-_____ restricitions

A

line-of-sight

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1
Q

Where is the navigation receiver located?

A

In the right avionics bay

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2
Q

VOR broadcast on ____º radials and are oriented to ________ _________

A

360º

magnetic north

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3
Q

The ILS system is composed of what 3 distinct signals?

A

Localizer
Glideslope
Marker Beacons

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4
Q

DME is calculated on _______ ________ distance

A

slant range

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5
Q

The T-6 flight instruments consist of what 3 systems?

A

Electronic Flight Instrument System (EFIS)
Air Data System (ADS)
Standby Instruments

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6
Q

Both the EADI and the EHSI receive their information from the _____________

A

Attitude Heading and Reference System (AHRS)

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7
Q

The ADS consists of what 3 EIDs?

A

ASI, Altimiter, VSI

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8
Q

What instruments are connected to the pitot static systems?

A

Airspeed/Mach, Altitude, Vertical speed data

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9
Q

The standby instruments receive pressure from what two sources?

A

Secondary pitot tube

Secondary static source

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10
Q

Power for the EHSI and EIDs is supplied through the _________ bus

A

generator

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11
Q

Power for the EADI is supplied through the ___________ bus

A

battery

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12
Q

The standby instruments normally receive their power from the __________ bus

A

battery

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13
Q

If the primary source of power for the standby instruments fail, they are then powered by the ________________

A

auxiliary battery

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14
Q

At the bottom of the EADI is a ________________ composed of 3 evenly spaced unfilled white rectangles and a white filled T

A

rate of turn scale

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15
Q

The EADI will automatically declutter if the pitch angle exceeds +___º or -___º or the roll angle exceeds ___º

The normal EADI presentation will reappear when the aircraft returns to a pitch orientation of less than ___º up or ___º down and the bank angle is less than ___º

A

+30º, -20º, 65º

25º, 15º, 60º

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16
Q

The chevrons appear on the EADI when the pitch attitude is between ____ and ____º nose up or down.

A

40º-90º

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17
Q

Range scale selections on the inner range circle are __________________

A

2.5, 5, 10, 20, 40, 80, 120, 160, 500

double for outer ring

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18
Q

When the EHSI is in HSI normal mode, pressing the map button changes the display to the ________________

A

navigation map

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19
Q

Which display adds a marker beacon display in approach mode?

A

EADI

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20
Q

Marker beacons have a rated power output of ___ watts or less. Produce and ellliptical pattern with dimensions, at _____ feet above the antenna, of approximately _____ feet in width and ______ feet in length

A

3 watts
1000 above
2400 width
4200 length

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21
Q

Describe each marker beacon color and morse code

A

OM (blue) _ _ _
MM (amber) . _ . _
IM (white) . . . .

22
Q

The VSI shows climbs or descents in fpm up to ______ fpm

23
Q

The red barber pole on the ASI indicates _________

A

maximum operating airspeed (Vmo)

24
Q

The ASI displays Mach number beginning at _____ Mach

25
Q

Name the 5 standby instruments

A
Airspeed indicator
Attitude indicator
Altimeter
Turn and bank indicator
Magnetic compass
26
Q

The standby airspeed indicator displays airspeed from ____ to ____ knots

27
Q

When the standby attitude indicator has lost electrical power, the flag becomes visible and the indicator will continue to provide pitch and roll indications within __º for at least __ minutes

A

6º for at least 9 minutes

28
Q

Compass readings should only be taken when?

A

During level, unaccelerated flight

29
Q

Where is the AOA computer located?

A

On the avionics shelf under the front cockpit glareshield

30
Q

The AOA computer receives input from (3):

A
AOA vane
Flap position microswitch
Landing gear (when extended)
31
Q

The AOA gauges adjusts its signal according based on a discrete _____________

A

Flap position signal

32
Q

When the landing gear is down, the AOA computer activates the _____________

A

AOA indexers

33
Q

The AOA computer activates the stick shaker at ___-___ units

34
Q

Angle of attack can be used to fly the aircraft on __________________ in the landing pattern if cross-checked and verified with the airspeed.

A

optimum no-wind airspeed

35
Q

What does the white triangle and white diamond on the AOA gauge represent? What are their units?

A

White Triangle: Maximum range, 4.9 units

White Diamond: Maximum endurance, 8.8 units

36
Q

The AOA vane remains aligned with the relative airflow and, through a belt and pulley system, drives a _________ which provides an electronic signal to the AOA computer

A

potentiometer

37
Q

What is the green arc range on the AOA indicator?

A

10 to 11 units

38
Q

Where is the red radial on the AOA gauge?

39
Q

What does a green chevron on the AOA indexer indicate?

Red?

A

Green: The angle of attack is too high (slow approach speed)

Red: the angle of attack is too low (fast approach speed)

40
Q

A stick shaker provides stall warning at approximately ___ to ___ knots about stall speed (___ to ___ units)

A

5 to 10 knots

15 to 16 units

41
Q

The accelerometer displays instantaneous normal acceleration from ___ to ___ G

A

-6 to +10 Gs

42
Q

How does a pilot set the minutes on the LT setting on the clock?

A

Adjust the minutes on the GMT clock which will be synchronized to the LT

43
Q

What is the ET limited to on the clock?

A

99 hours 59 minutes

44
Q

Various pilot warning tones are output by an electronic tone generator located in the ______________.

A

AOA computer

45
Q

The AURAL WARN circuit breaker is located on which bus?

A

Generator Bus

46
Q

All Integrated Data Acquisition Recording System (IDARS) functions are ______ controlled.

47
Q

the FDR portion of IDARS is located in the _______________

A

left avionics bay

48
Q

The ______________ is a portable memory cartridge used for digital information storage, loading, and retrieval. It has the primary purpose of storing Individual Aircraft Tracking (IAT), structures, engine, documentary, and Built-In Test (BIT data in non-volatile memory.

A

Data Transfer Module (DTM)

49
Q

When does the green maintenance annunciator (MAINT) illuminate?

A

When the IDARS reaches approximately 80% full.

50
Q

What are the 3 EFIS modes?

A

Enroute, Approach, and Composite Mode

51
Q

When should you cage the standby attitude indicator?

A

Before applying or removing electrical power

Before engine start and shutdown

52
Q

The ARC Button presents a large scale view of either DG or normal mode and displays ___º of compass