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Intrument Rating > Instrument Flying > Flashcards

Instrument Flying Flashcards

1
Q

Instrument cross check

A
  • scan

- logical or systematic observation of instrument panel

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2
Q

Radial check

A

Spending 80 to 90% of time on attitude indicator

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3
Q

Common cross check errors

A
  • fixation, applying full attention on a single instrument .
  • omission, exclusion of one or more secondary instrument for given task.

Emphasis, relying on an instrument that you really understand. Even when it provides inadequate information for given task.

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4
Q

Instrument interpretation

A
  • Understanding the limitations of each instrument, knowing which other instrument to cross check to complet picture.
  • results from cross checking and interpreting the flight instrument.
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5
Q

Control and Performance Method

A
  • Control, Performance, Navigation
  • use control instruments by accurately establishing a specific attitude and power setting.
  • performance instruments will indicate how the airplane will responds to altitude and power setting.
  • navigations displays where the airplane is.
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6
Q

Control and performance method

what are the control instruments?

A

Attitude indicator
Tachometer
Manifold pressure

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7
Q

Control and performance method

what are the performances instruments?

A 
Airspeed 
Turn Coordinatoor 
Heading indicator 
Altimeter 
VSI
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8
Q

Control and Performance Method

Steps

A 
Set altitude 
Set power 
Trim 
Cross check performance 
Correct with attitude or power settings

Tip set power, then control speed with pitch

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9
Q

Primary and supporting method

Pitch instruments

A

Airspeed
Attitude indicator
VSI

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10
Q

Primary and supporting method

Bank instruments

A

Attitude indicator
Turn coordinator
Heading indicator

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11
Q

Primary and supporting method

Power instruments

A

Airspeed
Tachometer
Manifold pressure

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12
Q

Primary and Supporting Method

Straight and level flight - POWER CONTROL
Establishing

A

Attitude indicator (P)

Airspeed indicator (S)
Altimeter (S)
VSI (S)

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13
Q

Primary and Supporting Method

Straight and level flight - POWER CONTROL
Maintaining

A

Airspeed indicator (P)

Tachometer (S)

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14
Q

Primary and Supporting Method

Straight and level flight - PITCH CONTROL
Establishing

A

Attitude indicator (P)

Airspeed (S)
Altimeter (S)
VSI (S)

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15
Q

Primary and Supporting Method

Straight and level flight - PITCH CONTROL
Maintaining

A

Altimeter (P)

VSI (S)

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16
Q

Primary and Supporting Method

Straight and level flight - BANK CONTROL
Establishing

A

Heading indicator (P)

Attitude indicator (S)

17
Q

Primary and Supporting Method

Standard Rate Turn- BANK CONTROL
Establishing

A

Rate turn indicator (P)
Trend (P)

HSI (heading indicator) (s)

18
Q

Primary and Supporting Method

Standard Rate Turn- BANK CONTROL
Maintaining

A

Rate turn indicator (P)
Trend (P)

Attitude (S)

19
Q

Primary and Supporting Method

Standard Rate Turn- PITCH CONTROL
Establishing

A

Attitude indicator (P)

Altimeter (S)

20
Q

Primary and Supporting Method

Standard Rate Turn- PITCH CONTROL
Maintaining

A

Altimeter (P)

Attitude indicator
VSI

21
Q

Primary and Supporting Method

Standard Rate Turn- POWER CONTROL
Establishing

A

Airspeed indicator (P)
Tachometer (P)
Manifold pressure

22
Q

Primary and Supporting Method

Steep Turn- PITCH CONTROL

A

BANK - Attitude indicator
PITCH - Altimeter
PITCH - VSI (S)
POWER - Airspeed indicator to add appropriate power.

23
Q

Primary and Supporting Method

Constant airspeed climbs - PITCH CONTROL
Establishing

V(y)
V(x)

A

Attitude indicator (P)
Airspeed indicator
Altimeter
VSI

24
Q

Primary and Supporting Method

Constant airspeed climbs - PITCH CONTROL
Maintain

V(y)
V(x)

A

Airspeed for pitch control (p)
VSI
Altimeter

25
Q

Primary and Supporting Method

Constant Rate climbs -
Establishing

V(y)
V(x)

A

Attitude indicator (P)
Airspeed indicator until 6 seconds have passed and VSI establishes rate
VSI
Altimeter

26
Q

Primary and Supporting Method

Constant Rate climbs - PITCH CONTROL
Maintaining

V(y)
V(x)

A

VSI
Watch for airspeed changes, make sure it’s adequate careful with stall.
Tachometer - add power as needed
Heading indicator

27
Q

Primary and Supporting Method

Constant airspeed descents - PITCH CONTROL
Establishing

V(y)
V(x)

A 
Attitude indicator (P) simultaneously 
Power reduction (P) simultaneously 
Airspeed indicator/ altimeter VSI to establish descent speed
28
Q

Primary and Supporting Method

Constant airspeed descents - PITCH CONTROL
Maintaining

V(y)
V(x)

A

Control airspeed with pitch. Watch for yellow arch.

Attitude indicator

29
Q

Primary and Supporting Method

Constant Rate descents - PITCH CONTROL
Establishing

A

Attitude indicator

Power reduction

30
Q

Primary and Supporting Method

Constant Rate descents - PITCH CONTROL
Maintaining

A

VSI
correct using attitude indicator
Airspeed indicator for power

31
Q

Lead the end of the descent by____%

A

10%

Ex. 500/ft per second with 50ft

32
Q

Suspect failure in heading indicator if

A

Attitude indicator has failed

33
Q

Standard rate turn

A

45 degrees in 15 seconds
90 degrees in 30 seconds
180 degrees in 1 minute
360 degrees in 2 minutes

34
Q

Nose high unusual altitude

A

Add power
Lower nose
Level wing
Establish straight and level flight

35
Q

Nose low unusual attitude

A

Reduce power
Level wings
Rise nose to horizon
Establish straight and level flight

Intrument Rating (7 decks)

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