SH.VIII.C.K4

From the FAA library

• Pilot's Handbook of Aeronautical Knowledgep. 11-17
  Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Landing Performance

  item that alters the landing speed or deceleration rate during the landing roll affects the landing distance. The effect of gross weight on landing distance is one of the principal items determining the landing distance. One effect of an increased ... gross weight is that a greater speed is required to support the aircraft at the landing AOA and lift coefficient. For an example of the effect of a change in gross weight, a 21 percent increase in landing weight requires…

• Pilot's Handbook of Aeronautical Knowledgep. 14-28
  Chapter 14: Airport Operations › En Route › Vortex Avoidance Procedures

  Vortex Avoidance Procedures The following procedures are in place to assist pilots in vortex avoidance in the given scenario. • Landing behind a larger aircraft on the same runway— stay at or above the larger aircraft’s approach flight path ... land beyond its touchdown point. [Figure 14-47A] • Landing behind a larger aircraft on a parallel runway closer than 2,500 feet—consider the possibility of drift and stay at or above the larger aircraft’s final approach flight…

• Helicopter Flying Handbookp. 10-6
  Chapter 10: Advanced Flight Maneuvers › Shallow Approach and Running/Roll-On Landing

  Shallow Approach and Running/Roll-On Landing Use a shallow approach and running landing when a high-density altitude, a high gross weight condition, or some combination thereof, is such that a normal or steep approach cannot be made because of insufficient ... power to hover. [Figure 10-5] To compensate for this lack of power, a shallow approach and running landing makes use of translational lift until surface contact is made. If flying a wheeled helicopter, a roll-on landing…

• Helicopter Flying Handbookp. 9-19
  Chapter 9: Basic Flight Maneuvers › Approaches › Technique

  Technique On final approach, at the recommended approach airspeed and at approximately 300 feet AGL, the helicopter should be on the correct ground track (or ground alignment) for the intended landing site, but the axis of the helicopter does ... have to be aligned until about 50-100 feet AGL to facilitate a controlled approach. [Figure 9-20] Just prior to reaching the desired approach angle, begin the approach by lowering the collective sufficiently to get the helicopter decelerating…

• Helicopter Flying Handbookp. 10-11
  Chapter 10: Advanced Flight Maneuvers › Pinnacle and Ridgeline Operations › Approach and Landing

  immediate turn away from the pinnacle to avoid being forced into the rising terrain. Groundspeed during a pinnacle approach is more difficult to judge because visual references are farther away than during approaches over trees or flat terrain. Pilots must ... continually perceive the apparent rate of closure by observing the apparent change in size of the landing zone features. Avoid the misperception of an increasing rate of closure to the landing site. The apparent rate of closure should be that…

• 14 CFR Part 91 — General Operating and Flight RulesOpen
  14 CFR § 91.1705 Required pilot training.

  limitations, procedures, aircraft performance, and MU-2B Cockpit Checklist procedures applicable to the MU-2B model being trained. A MU-2B training program must contain, at a minimum, the following flight training maneuver profiles applicable to the MU-2B model ... loss of directional control; (viii) Approach to stall in clean configuration and with wings level; (ix) Approach to stall in takeoff configuration with 15- to 30- degrees bank; (x) Approach to stall in landing configuration with gear down…