Tech Prep - Instumentation Flashcards

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1
Q

IAS

A

Indicated Airspeed
Dynamic pressure as displayed on the AIS

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2
Q

CAS

A

Calibrated Airspeed
IAS corrected for position and instrument errors
Larger modern ACFT ADCs display this, V speeds are in CAS

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3
Q

EAS

A

Equivalent Airspeed
CAS corrected for compressibility
Vmo is in EAS

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4
Q

TAS

A

CAS (EAS) corrected for temperature and pressure

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5
Q

Mach number formula

A

38.94*(T(Kelvin)^½

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6
Q

ASI errors (6 in total)

A

Instrument
Pressure
Density
Compressibility
Maneuver
Blocked pitot static system

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7
Q

ASI error: static probe blockage

A

At constant altitude ASI reads correctly
During descend the ASI will over read
During climb, ASI will under read

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8
Q

ASI error: dynamic probe blockage

A

At constant altitude the ASI is frozen
During descend the ASI will under read
During climb the ASI will over read

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9
Q

Altimeter errors (7)

A

Instrument
pressure
time-lag
barometric
density
temperature
blockage

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10
Q

Altimeter error: static port blockage

A

indicator stuck

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11
Q

VSI errors (4)

A

instrument
time-lag
pressure
maneuver

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12
Q

VSI error: statick probe blockage

A

indicator moves to 0 and does not change

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13
Q

Slip vs Skid

A

Slip is lateral force into the turn
Skid is lateral force out of a turn

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14
Q

Turn and slip indicator

A

2 degrees of freedom gyro
rotates about the horizon axis
one gimbal about the ACFTs lateral axis

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15
Q

Magnetic compass:
ANDS
UNOS

A

Accelerate North Decelerate South
Undershoot North, Overshoot South

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16
Q

Autopilot landing systems:
Fail-passive

A

In the event of a failure, controls handed back to the pilot without significant out of trim condition
typically:
Auto-monitored auto-pilot
Two autopilots auto-comparing eachother

17
Q

Autopilot landing systems:
Fail-operational

A

In the event of a failure, approach, flare and landing can still be completed by the remaining part of the system. Typically achieved via reverting back to fail-passive
Typical arrangements:
Two monitored APs, one remaining operative after failure
Three APs, two remaining operative after failure

18
Q

Fail-operational hybrid system

A

Typically one fail-passive system and a secondary independent guidance system enabling manual completion after a failure of the primary

19
Q

Frequency ranges:
NAV
COM
ILS
VOR
NAV aids enroute/terminal

A

NAV: 118.00-117.975
COM: 118.00-136.975
ILS: 108.000-111.975 ending 0/5 odd second digit
VOR 108.000-111.975 ending 0/5 even second digit
NAV aids enroute: 112.000-117.975