Instruments Flashcards

0
Q

How does warm air affect indicated altitude?

A

Will cause indicated altitude to be > true altitude (warm air increases press) [altimeter does not correct for nonstandard temp]
“from hot to cold, look out below”

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1
Q

Press change with altitude?

Change with temp?

A

Decrease as increase elevation at 1’ per 1000 feet

More rapid in colder air

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2
Q

Field elevation should read XX feet when baro is set to ATIS

A

= or - 75 feet

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3
Q

Standard rate turn

How to calculate for gyro?

A

2 min to complete 360 deg (or 3 deg/sec)

For gyro:
drop zero, add 7
eg 100 –> 17 deg, 110 –> 18 deg, 120 –> 19 deg

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4
Q

Dip/compass errors

  • acceleration
  • northern turning error
A

ANDS: Acceleration (on West-East headings) :
accel –> shows turn to the North,
decel –> shows turn to the South

UNOS: North turning error 
Undershoots (lag) north
Overshoots south
(if you turn while heading south, compress will show faster rate)
or
UNOS (undershoot N, overshoot S)
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5
Q

Blocked pitot

Blocked pitot and drain

A
Airspeed = constant and dropping, all else OK.  
Airspeed = reads high if climbing, low in decent*, all else normal

*Trapped press is making air speed act like an altimeter

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6
Q

Blocked static

A

altimeter -stuck at altitude when blocked
and VSI - stuck
airspeed - reads low during climb and vice versa (expected)

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7
Q

If you use the Alternate Static, what do you see?

A

press in cockpit is lower, so performances “improves”

Altimeter - higher; Airspeed - greater; VSI- climbs

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8
Q

VOR check
VOT
Airborne
dual

A

VOT (at airport, see AFD): turn TO, then FROM, must be +-4 deg

airborne: +-6 degrees
dual: tune to same VOR, max is 4 degree

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9
Q

VOR scale and full deflection

A

each dot is 2 deg

“30 Mile Rule” Each dot = 1 mile at 30 miles

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10
Q

ILS contains 4 elements

Outer, middle, inner markets

A

Glideslope, localizer, marker beacons, approach lites
Outer: 3-7 miles out; blue, hear dashes
Middle: 0.5 mile, 200 feet; amber, dash/dots
Inner: white, fast dot sound

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11
Q

Cold air altimeter effects

A

Indicated can be much lower than actual because cold air is extremely dense. See Correction Chart in AIM (7-2-3)

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12
Q

How does an altimeter work?

A

aneroid wafers expand or contract with changing atmospheric conditions

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13
Q

Limitations of altimeter with temp and nonstandard pressure?

A

Low standard press (or cold day) - reads higher than actual

Remember: High to low, or hot to cold - look out below

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14
Q

Errors of an airspeed indicator?

A

1) static port affected by air flow
2) density error: (change in altitude or temp not compensated)
3) Compressibility error: air packs in static at speeds > 180 kts

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15
Q

Standard lapse rate is?

eg what is freezing level at airport that is 1200 AGL, 6deg C?

A

2 deg per 1000 feet

0 degrees is at 3000, so 3000+1200=4200 feet

16
Q

Which instruments use a gyro?

A

attitude indicator
heading indicator
turn coordinator

17
Q

Slip skid

A

Slip - ball inside turn, not enough rudder

Skid - ball outside turn, too much rudder

18
Q

Types of compass errors

A

Deviation - demons inside
Variation - earth mag disturbance, corrected by isogonic lines
Oscillation - cause by turbulance
Dip errors

26
Q

if you change heading 360 to 330, how long is this turn?

A

30 deg / 3 = 10 sec

28
Q

How do you check VOR with a VOT (VOR test signal)?

A

remember cessna 182

turn to 108, should show 180 and TO

29
Q

Emergency transponder codes?

A

7500 - hijack
7600 - comm
7700 - emergency

30
Q

What altitude does Mode C transponder transmit?

A

not the one on your altimeter. it is preset to 29.92

31
Q

Full deflection of VOR is

Full deflection of CDI for a localizer?

A

10 degrees

2.5 degree (4x greater than VOR)

32
Q

What if you receive VOR code every 30 seconds

A

DME is operative, VOR is NOT.

33
Q

VOR effective distances? What’s max distance if off an airway?

A

terminal - 25 miles
low - 40
high - 40 to 130

below 18000, no more that 80 NM

34
Q

Elements of GPS
What is RAIM?
If RAIM is lost, can you continue IRF?

A

24 Navstar satellites, at least 5 in view
Receiver autonomous integrety monitoring - checks status and if corrupted info is present.
No, must have RAIM capability for accuracy.

35
Q

Standard take off climb slope and distance

A

1:40 or 200 ft/nm

calculate by: GS/60 x 200 —> 120 kts GS = 400 FPM

36
Q

If pitot block, only one instrument is affected?

A

Airspeed
if ram port blocked, drain open: slowly goes to 0
if both blocked: acts like an alterimeter

37
Q

VSI basis?

A

has a “calibrated leak” that sensing pressure differential

38
Q

block static shows?

A

airspeed: low in climb, hi in decent

altimeter & VSI: freeze

39
Q

VOR distance off course

A

at 30 miles from VOR, each dot = 1 mile (at 60 miles, each is 2 miles)

40
Q

WAAS full scale sensitivity

RNP

A

WAAS RNP (requd nav performance)
en route: 5 miles 2
terminal: 1 1
approach: 0.3 0.3

41
Q

WAAS level of precision?

A

from 100 meters (non WAAS) to about 2 meters horizontal/vert