FH.VI.B.S4
SkillAnalyze and correct common errors related to this Task.
From the FAA library
- Chapter 7. Safety of Flight › Section 2. Barometric Altimeter Errors and Setting Procedures › 7-3-5. Cold Temperature Airport Procedures
Pilots that have a system unable to calculate a temperature corrected DA or MDA will manually calculate an altitude correction for the MDA or DA. NOTE-Some systems apply temperature compensation only to those altitudes associated with an instrument approach ... passed the last altitude constraint associated with the active STAR. 2. Individual Segment(s) Method: Pilots are allowed to correct only the marked segment(s) indicated in the CTA list (https://www.faa.gov/air_traffic/flight_info/aeronav/digital_products/dtpp/search/). Pilots using the Individual Segment(s) Method…
- Chapter 2: Aerodynamics of Flight › Airflow and Reactions in the Rotor Disk › Resultant Relative Wind
highest. As blade speed decreases nearer the center of the disk, downward velocity is less. Figure 2-19. Rotational relative wind. Resultant Relative Wind The resultant relative wind at a hover is rotational relative wind modified by induced flow. This ... inclined downward at some angle and opposite the effective flightpath of the airfoil, rather than the physical flightpath (rotational relative wind). The resultant relative wind also serves as the reference plane for development of lift, drag, and total aerodynamic force…
- Chapter 2: Aerodynamics of Flight › Airflow and Reactions in the Rotor Disk › Rotational Relative Wind (Tip-Path Plane)
Airflow and Reactions in the Rotor Disk Relative Wind Knowledge of relative wind is essential for an understanding of aerodynamics and its practical flight application for the pilot. Relative wind is airflow relative to an airfoil. Movement of an airfoil ... through the air creates relative wind. Relative wind moves in a direction parallel to but opposite of the movement of the airfoil. [Figure 2-15] There are two parts to wind passing a rotor blade: • Horizontal part—caused…
- Chapter 7. Safety of Flight › Section 2. Barometric Altimeter Errors and Setting Procedures › 7-3-6. Examples for Calculating Altitude Corrections on CTAs
intersect the 5000 ft height above airport column. The approximate value is 500 ft. (13) Add correction to holding fix final altitude: b. Temperature Compensating System: Operators using a temperature compensating RNAV system to make altitude corrections will ... airport temperature (-12°C) and activated prior to passing the IAF. A manual calculation of the cold temperature altitude correction is required for the MDA/DA. 1. Individual Segments Method: Missoula requires correction in the intermediate and final segments. However…
- Chapter 6: Threat and Error Management › Causes of Errors › Insufficient Training & Experience
Chapter 6: Threat and Error Management Introduction Threats What is an Error? Causes of Errors Insufficient Training & Experience Introduction Pilots use risk management as described in earlier chapters to analyze the likelihood and potential severity of an incident or accident ... encounter unforeseen hazards or threats. In addition, a pilot may respond inappropriately to a given condition, thus making an error. This chapter provides strategies pilots may use once flight begins. Threats Threats have the following characteristics: • Threats occur outside…
- Chapter 3: The Learning Process › Errors › Learning from Error
Error Recovery Given that the occasional error is inevitable, it is a worthwhile exercise to practice recovering from commonly made errors, or those that pose serious consequences. All flight learners need to learn and practice a lost procedure to ensure ... which they have lost their way. It is useful to devote the same sort of preparation to other common learner errors. Learning from Error Error can be a valuable learning resource. Learners naturally make errors, which instructors can utilize…