IL.II.F.R5
Risk managementOther hazards specific to the powered-lift make and model.
From the FAA library
- Chapter 2: Aeronautical Decision-Making › The Programming › Perceive, Process, Perform (3P) Model
Perceive, Process, Perform (3P) Model The Perceive, Process, Perform (3P) model for ADM offers a simple, practical, and systematic approach that can be used during all phases of flight. To use it, the pilot will: • Perceive the given ... Perform by implementing the best course of action Use the Perceive, Process, Perform, and Evaluate method as a continuous model for every aeronautical decision that you make. Although human beings will inevitably make mistakes, anything that…
- Chapter 3: Identifying Hazards & Associated Risks › Aircraft Hazards › Performance
example, fatigue may degrade cognitive skills and decision-making ability. 11828 • Emotion–Has the pilot experienced an event or received information that creates strong feelings? Emotions may affect normal pilot ability to focus. The IMSAFE checklist, which is an acronym ... Illness, Medication, Stress, Alcohol, Fatigue, and Emotion, can help a pilot identify these hazards. [Figure 3- 3] Note that some publications combine Emotion with Stress as the “S” in IMSAFE and leave the “E” to remind pilots about “Eating.” Since…
- Chapter 11: Aircraft Performance › Climb Performance Factors › Region of Reversed Command
normal command. Flight in the region of reversed command means flight in which a higher airspeed requires a lower power setting and a lower airspeed requires a higher power setting to hold altitude. It does not imply that a decrease ... power produces lower airspeed. The region of reversed command is encountered in the low speed phases of flight. Flight speeds below the speed for maximum endurance (lowest point on the power curve) require higher power settings with a decrease…
- Chapter 11: Aircraft Performance › Climb Performance Factors › Range Performance
NOTE: The straight line that is tangent to the sea level power curve is also tangent to the altitude power curve. The effect of altitude on specific range can also be appreciated from the previous relationships. If a change ... altitude causes identical changes in speed and power required, the proportion of speed to power required would be unchanged. The fact implies that the specific range of a propeller-driven aircraft would be unaffected by altitude. Actually, this is true…
- Chapter 8: Aeronautical Decision-Making in Flight › Analytical Decision-Making
improvements in training and technology, human error remains an issue. ADM provides a foundation, which should help pilots avoid making errors in judgment. Aeronautical decision-making (ADM) provides pilots with a structured framework of processes and procedures, which have ... positive effect on managing hazards. ADM does not eliminate hazards, but helps the pilot address hazards and associated risks that threaten the safety of flight. ADM describes the ongoing process used by pilots to determine the best course of action…
- 14 CFR § 91.1505 Repairs assessment for pressurized fuselages.
Repairs assessment for pressurized fuselages. (a) No person may operate an Airbus Model A300 (excluding the -600 series), British Aerospace Model BAC 1-11, Boeing Model 707, 720, 727, 737 or 747, McDonnell Douglas Model DC-8, DC-9/MD-80 ... Fokker Model F28, or Lockheed Model L-1011 airplane beyond applicable flight cycle implementation time specified below, or May 25, 2001, whichever occurs later, unless repair assessment guidelines applicable to the fuselage pressure boundary (fuselage skin, door skin, and bulkhead…