SARON 10-1
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Questions and Answers

What requires reporting an aviation accident? Select all that apply

  • Missing aircraft (correct)
  • Passenger gets severely injured by aircraft (correct)
  • All passengers safely disembarked
  • Aircraft suffers severe damage that effects performance (correct)
  • What do you do when Balanced field length reaches V1

  • You are allowed to return to the gate
  • You should immediately abort takeoff
  • Continue take off you, you can reject and continue climb to 35 feet end of the runway (correct)
  • You reduce speed significantly
  • What does a capabilical fuel gauge measure?

  • Fuel mass and independent temperature influence (correct)
  • Fuel efficiency rating
  • Fuel temperature only
  • Total fuel capacity
  • Which of the following is not part of the preventions for CFIT?

    <p>Using autopilot exclusively</p> Signup and view all the answers

    What does the Dihedral stabilize?

    <p>Horizontal axis</p> Signup and view all the answers

    What is the effect of increased density altitude on buffet speeds?

    <p>High buffet speeds decrease, low buffet speeds increase</p> Signup and view all the answers

    What is the purpose of jet engine thrust reversal?

    <p>To redirect exhaust gas forwards</p> Signup and view all the answers

    Compressor stall is caused by?

    <p>Excessive A of A on the compressor blades</p> Signup and view all the answers

    Study Notes

    Aviation Accidents and Safety

    • Report aviation accidents if an aircraft is missing, people are severely injured by an aircraft, or an aircraft suffers severe damage that affects its performance.

    Balanced Field Length

    • If V1 is reached, continue the takeoff and climb to 35 feet at the end of the runway.

    Fuel Measurement

    • A capacitable fuel gauge measures fuel mass and is independent of temperature influences.
    • Note: A capacitable fuel gauge provides a margin against buffet.

    Minimum Equipment List (MEL)

    • MEL is used during a defect period.

    Density Altitude

    • An increase in density altitude decreases the high buffet speed and increases the low buffet speed, resulting in a decrease in the buffet range margin.

    Aircraft Design

    • Dihedral provides stability about the longitudinal axis.

    Marshaling Signals

    • Marshaling signals are used to identify the gate, indicate when to stop, and when to move chocks; they also signal left engine fire (refer to AIM).

    Precision Approach Path Indicators (PAPI)

    • PAPI has an eye-to-wheel distance (ETW) of 12.5ft, which is suitable for runways CFS R/W 01 and 19 only.
    • There are different types of PAPI:
      • P1: ETW up to 10ft
      • P2: ETW up to 25ft
      • P3: ETW up to 45ft
    • VASIS (Visual Approach Slope Indication System) is used in conjunction with PAPI:
      • Wide body AC: use upper and middle bar
      • Normal AC: use downwind and middle bar

    Controlled Flight into Terrain (CFIT)

    • To prevent CFIT, maintain situation awareness, know the terrain, and understand the function of the Ground Proximity Warning System (GPWS).

    Jet Engine Thrust Reverse

    • Thrust reverse in a jet engine involves redirecting exhaust gases forward.

    Causes of Compressor Stall

    • Inadequate fuel flow to primary fuel nozzles due to improper scheduling by the fuel control unit can trigger compressor stall.
    • Below-normal temperatures in the power turbine section impact compressor performance, potentially leading to stall.
    • Excessive angle of attack on compressor blades can disrupt airflow and contribute to stall conditions.
    • Stator blade warping, especially at high Engine Pressure Ratio (EPR) settings, can result in compressor stall.

    Identifying Compressor Stall Symptoms

    • Predominant symptoms include:
      • Loud explosive bangs indicating sudden disruptions in engine operation.
      • Lower Exhaust Gas Temperature (EGT) or Interstage Turbine Temperature (ITT) readings signal reduced engine performance.
      • Higher than normal fuel flow can occur as the system attempts to compensate for airflow disruptions.
      • Engine surging, characterized by rapid fluctuations in engine power and performance, reflects instability during stall.
    • Other potential indicators of compressor stall may include high oil temperature, lower torque or N1 readings, and altered compressor readings, but these are less definitive.

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    Description

    Quiz about aviation safety regulations, aircraft performance, and fuel measurement. Topics include reporting accidents, balanced field length, and fuel gauges.

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