Instrument Flying Flashcards

(35 cards)

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
Primary and Supporting Method Constant Rate climbs - Establishing V(y) V(x)
Attitude indicator (P) Airspeed indicator until 6 seconds have passed and VSI establishes rate VSI Altimeter
26
Primary and Supporting Method Constant Rate climbs - PITCH CONTROL Maintaining V(y) V(x)
VSI Watch for airspeed changes, make sure it’s adequate careful with stall. Tachometer - add power as needed Heading indicator
27
Primary and Supporting Method Constant airspeed descents - PITCH CONTROL Establishing V(y) V(x)
``` Attitude indicator (P) simultaneously Power reduction (P) simultaneously Airspeed indicator/ altimeter VSI to establish descent speed ```
28
Primary and Supporting Method Constant airspeed descents - PITCH CONTROL Maintaining V(y) V(x)
Control airspeed with pitch. Watch for yellow arch. | Attitude indicator
29
Primary and Supporting Method Constant Rate descents - PITCH CONTROL Establishing
Attitude indicator | Power reduction
30
Primary and Supporting Method Constant Rate descents - PITCH CONTROL Maintaining
VSI correct using attitude indicator Airspeed indicator for power
31
Lead the end of the descent by____%
10% | Ex. 500/ft per second with 50ft
32
Suspect failure in heading indicator if
Attitude indicator has failed
33
Standard rate turn
45 degrees in 15 seconds 90 degrees in 30 seconds 180 degrees in 1 minute 360 degrees in 2 minutes
34
Nose high unusual altitude
Add power Lower nose Level wing Establish straight and level flight
35
Nose low unusual attitude
Reduce power Level wings Rise nose to horizon Establish straight and level flight