IL.VIII.C.S10

From the FAA library

• Pilot's Handbook of Aeronautical Knowledgep. 11-6
  Chapter 11: Aircraft Performance › Performance › Climb Performance

  Positive climb performance occurs when an aircraft gains PE by increasing altitude. Two basic factors, or a combination of the two factors, contribute to positive climb performance in most aircraft: 1. The aircraft climbs (gains PE) using excess power above ... that required to maintain level flight, or 2. The aircraft climbs by converting airspeed (KE) to altitude (PE). As an example of factor 1 above, an aircraft with an engine capable of producing 200 horsepower (at a given altitude…

• Pilot's Handbook of Aeronautical Knowledgep. 11-8
  Chapter 11: Aircraft Performance › Performance › Climb Performance Factors

  Climb Performance Factors Since weight, altitude and configuration changes affect excess thrust and power, they also affect climb performance. Climb performance is directly dependent upon the ability to produce either excess thrust or excess power. Earlier in the book ... altitude, lowering the landing gear, or lowering the flaps all decrease both excess thrust and excess power for all aircraft. Therefore, maximum AOC and maximum ROC performance decreases under any of these conditions. Weight has a very pronounced effect…

• Pilot's Handbook of Aeronautical Knowledgep. 11-7
  Chapter 11: Aircraft Performance › Performance › Rate of Climb (ROC)

  Rate of Climb (ROC) ROC is a comparison of altitude gained relative to the time needed to reach that altitude. ROC is simply the vertical component of the aircraft’s flight path velocity vector. For maximum ROC performance, a pilot ... flies the aircraft at VY so as to achieve a maximum gain in altitude over a given period of time. Maximum ROC expedites a climb to an assigned altitude. This gains the greatest vertical distance over a period of time…

• Pilot's Handbook of Aeronautical Knowledgep. 5-24
  Chapter 5: Aerodynamics of Flight › Aerodynamic Forces in Flight Maneuvers › Forces in Descents

  Figure 5-36. Changes in lift during climb entry. The thrust required for a stabilized climb equals drag plus a percentage of weight dependent on the angle of climb. For example, a 10° climb would require thrust to equal drag ... plus 17 percent of weight. To climb straight up would require thrust to equal all of weight and drag. Therefore, the angle of climb for climb performance is dependent on the amount of excess thrust available to overcome a portion…

• Instrument Flying Handbookp. 9-29
  Chapter 9: Navigation Systems › Advanced Technologies › IFR Flight Using GPS

  NAVAIDs. Departure WP, DP, route, STAR, desired approach, IAF, and destination airport are entered into the GPS receiver according to the manufacturer’s instructions. During preflight, additional information may be entered for functions such as ETA, fuel planning, winds aloft ... aircraft. The GPS receiver provides navigational values such as track, bearing, groundspeed, and distance. These are computed from the aircraft’s present latitude and longitude to the location of the next WP. Course guidance is provided between…

• Small Unmanned Aircraft System (Small UAS)p. 7-1
  CHAPTER 7. SMALL UAS MAINTENANCE AND INSPECTION › 7.2 Maintenance

  perform checks of the small unmanned aircraft prior to each flight to determine whether the small UAS is in a condition for safe operation. This chapter provides guidance on how to inspect and maintain a small UAS. Additionally, Appendix ... necessary for flight. Whenever possible, the operator should maintain the small UAS and its components in accordance with manufacturer’s instructions. The aircraft manufacturer may provide the maintenance program, or, if one is not provided, the applicant may choose…