SARON 7-12
6 Questions
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SARON 7-12

Created by
@SaintlyCloisonnism

Questions and Answers

What is the weight shift value?

  • 8868 (correct)
  • 8000
  • 8500
  • 9200
  • Under what conditions can you do an approach at an alternate with PROP in the TAF of the A/D?

  • Always
  • If visibility is above 1 mile
  • Never
  • Only if the weather in PROP meets landing minimum (correct)
  • What is the worst case for aircraft performance?

  • Low temperature, high dew point, high pressure
  • High temperature, low dew point, high pressure
  • High temperature, high dew point, low pressure (correct)
  • Low temperature, low dew point, low pressure
  • Can you continue taxiing if visibility becomes lower than the operator limit after starting to taxi?

    <p>Yes, if you started to taxi before</p> Signup and view all the answers

    What is the L/D weight if an aircraft weighs 220,000lbs, burns 1200lbs of fuel for descent and approach, has a TAS of 485kts, a wind factor of 60kts, and will have a one-hour flight?

    <p>196800lbs</p> Signup and view all the answers

    If Airdrome elevation is 140 ft, one ALT shows 120 ,another one shows 190, can you still use that?

    <p>Yes, one is in limit</p> Signup and view all the answers

    Study Notes

    Airplane Flight Notes

    Alternate Airport Approaches

    • A "PROP" show in the TAF of an Alternate Airport (A/D) does not prevent an approach; the approach can be made if the weather conditions meet the landing minimum.

    Weight and Performance

    • The weight shift is 8868.
    • The worst-case scenario for aircraft performance is a combination of high temperature, high dew point, and low pressure.

    Taxiing in Low Visibility

    • If visibility becomes lower than the operator's limit while taxiing, taxiing can be continued if it began before the visibility decreased.

    Takeoff Weight Calculation

    • The takeoff weight calculation result is 11800.

    Landing Weight Calculation

    • The landing weight (L/D weight) can be calculated by subtracting the fuel burn from the takeoff weight; in this case, the aircraft's weight is 220000lbs, fuel burn for descend and approach is 1200lbs, and fuel burn per hour is given, so after a one-hour flight, the L/D weight is 196800lbs, considering a TAS of 485kts and a wind factor of 60kts.

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    Description

    Test your knowledge of airplane flight operations with these questions on topics such as weather conditions, weight calculations, and taxiing procedures.

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