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  • Chapter 3: Identifying Hazards & Associated Risks › Leading Accident Causes

    general aviation fatal accidents include loss of control in-flight (LOC-I), controlled flight into terrain (CFIT), system component failure of the powerplant (SCF-PP), and fuel-related issues. These causes often signify the final result of a chain ... Examples of loss of control scenarios include continued VFR into IMC, wake turbulence upsets, thunderstorm encounters, instrument failure, improper aircraft loading, loss of outside references during flight at night or over water, and conditions that exceed the pilot’s capability…

  • Chapter 7: Automation & Flight Path Management › Failure to Anticipate, Act, & Verify

    Failure to Anticipate, Act, & Verify Automation offers increased safety with enhanced situational awareness. However, these systems make it possible for a pilot to become complacent, unprepared, or lose situational awareness. If this occurs and an unexpected change in flight plan ... crew was unexpectedly cleared for an approach, lost situational awareness, and crashed into mountainous terrain. The accident summary cites failure of the flight crew to revert to basic radio navigation at the time when the FMS-assisted navigation became confusing…

  • Glossary

    their status in the near future. Stress. The body’s response to demands placed upon it. System component failure of the powerplant (SCF-PP). An accident caused by failure of an engine component that may lead to complete failure…

  • Chapter 6: Flight Controls

    control system feedback errors, IFCS provides adjustments to improve aircraft performance in normal flight, as well as with system failures. With IFCS, a pilot is able to maintain control and safely land an aircraft that has suffered a failure…

  • Chapter 13: Aviation Weather Services › Electronic Flight Displays (EFD) /Multi-Function Display (MFD) Weather › Flight Information Service- Broadcast (FIS-B)

    updated as well as the Data Link Service Providers (DLSP) update rate for particular products. • Indication of system failure—be aware of partial or total system failure indications. • Coverage areas/service volume—coverage limitations are associated with the type of data…

  • Chapter 5: Aerodynamics of Flight › Weight and Balance › Effect of Weight on Aircraft Structure

    case of utility and acrobatic category aircraft, which have load factor requirements of 4.4 and 6.0, respectively. Structural failures that result from overloading may be dramatic and catastrophic, but more often they affect structural components progressively in a manner that ... tends to cause cumulative stress and damage that may not be detected during preflight inspections and result in structural failure later during completely normal operations. The additional stress placed on structural parts by overloading is believed to accelerate the occurrence…