SARON 6-12
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Questions and Answers

What is the limitation after scuba diving above 8000ft?

  • 24 (correct)
  • 36
  • 12
  • 18
  • What is spatial disorientation?

  • Confusion due to incorrect instrument readings
  • Inability to control aircraft altitude
  • Loss of situational awareness
  • Body's inability to determine position (correct)
  • What is the IFR fuel requirement (Jet) fuel for arriving at an alternate plus?

  • Fuel to fly to the alternate and an additional 15 minutes
  • Fuel to descend and circle for 20 minutes
  • Fuel to fly to the alternate and do approach there and 30 mins (correct)
  • Fuel to remain at the destination for an additional hour
  • How do Mach and IAS change when descending with TAS 450 kts maintained?

    <p>Mach decreases, IAS increases</p> Signup and view all the answers

    What is the attitude of the aircraft if the trim tab indicator indicates the down position (up position on the right wing)?

    <p>Nose up, left up</p> Signup and view all the answers

    What are common symptoms of a compressor stall? (Select all that apply)

    <p>Engine surge</p> Signup and view all the answers

    What rate of descent is required to descend from FL 180 to FL 100 in 20 NM if the ground speed is 250 kts?

    <p>1700 ft/min</p> Signup and view all the answers

    What will happen if the cabin pressurization system fails at FL 250?

    <p>Noise, fog, dust in the cabin</p> Signup and view all the answers

    Principal for fire detection

    <p>Reduce heat</p> Signup and view all the answers

    Study Notes

    Threat and Error Management (TEM)

    • A scenario is presented to identify the Threat and Error Management (TEM)

    Aviation Miscellaneous

    Limitations

    • Scuba diving above 8000ft has a limitation of 24 hours

    Aviation Physiology

    Spatial Disorientation

    • Spatial disorientation refers to the body's inability to sense its position and motion

    IFR Flight Planning

    Fuel Requirements

    • IFR fuel requirement for a Jet is fuel for flying to the Alternate airport, completing an approach, and 30 minutes of holding

    Aircraft Performance

    Mach and IAS Relationships

    • During descent with a constant TAS of 450 kts, Mach number decreases, and IAS increases

    Aircraft Systems

    Trim Tab Indication

    • A down position on the trim tab indicator on the right wing indicates a nose-up, left-wing-up attitude of the aircraft

    Engine Systems

    Compressor Stall Issues

    • Compressor stall issues include HIGH ITT, LOW N1, and ENGINE SURGE

    Aircraft Performance

    Descent Gradient

    • A descent from FL 180 to FL 100 in 20 NM requires a descent gradient of 1700 ft/NM

    Aircraft Systems

    Cabin Pressurization Failure

    • Cabin pressurization system failure at FL 250 results in dust entering the cabin due to sudden decompression

    Aircraft Systems

    Fire Detection Principle

    • The principle of fire detection is based on heat, which reduces sensitivity to false alarms

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    Description

    Test your knowledge on Threat and Error Management (TEM) concepts in aviation, including scuba diving limitations, spatial disorientation, IFR fuel requirements, and descent procedures.

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