IL.II.I.K4

From the FAA library

• 14 CFR Part 91 — General Operating and Flight RulesOpen
  14 CFR § 91.611 Authorization for ferry flight with one engine inoperative.

  operator, if applicable) and with all other engines operating at not more than the power selected for type certification as set forth in § 25.101 of this chapter. (2) The minimum takeoff field length must be the horizontal distance required ... more than the power selected for type certification as set forth in § 25.101 of this chapter. (3) The takeoff, flight, and landing procedures such as the approximate trim setting, method of power application, maximum power, and speed must be established…

• Pilot's Handbook of Aeronautical Knowledgep. G-26
  Glossary › Pilot’s Operating Handbook/Airplane Flight Manual

  radio aids to navigation, airports, controlled airspace, restricted areas, obstructions and related data. SDF. See simplified directional facility. Selective availability (SA). A satellite technology permitting the Department of Defense (DOD) to create, in the interest of national security, a significant ... set to any desired level. Service ceiling. The maximum density altitude where the best rate-of-climb airspeed will produce a 100-feet-per-minute climb at maximum weight while in a clean configuration with maximum continuous power. Servo…

• Pilot's Handbook of Aeronautical Knowledgep. 7-6
  Chapter 7: Aircraft Systems › Adjustable-Pitch Propeller

  pitch settings: low and high. Today, most adjustable-pitch propeller systems are capable of a range of pitch settings. A constant-speed propeller is a controllable-pitch propeller whose pitch is automatically varied in flight by a governor maintaining constant ... propellers because it allows selection of the most efficient engine rpm for the given conditions. An aircraft with a constant-speed propeller has two controls: the throttle and the propeller control. The throttle controls power output, and the propeller control…

• Pilot's Handbook of Aeronautical Knowledgep. 7-15
  Chapter 7: Aircraft Systems › Ignition System

  whenever the crankshaft is rotating. Most standard certificated aircraft incorporate a dual ignition system with two individual magnetos, separate sets of wires, and spark plugs to increase reliability of the ignition system. Each magneto operates independently to fire ... mixture and results in a slightly higher power output. If one of the magnetos fails, the other is unaffected. The engine continues to operate normally, although a slight decrease in engine power can be expected. The same is true…

• Instrument Flying Handbookp. 7-14
  Chapter 7, Section I: Airplane Basic Flight Maneuvers › Straight Climbs and Descents › Entry

  ensure the proper climb power setting is being maintained. If the climb attitude is correct for the power setting selected, the airspeed will stabilize at the desired speed. If the airspeed is low or high, make an appropriately small pitch ... level flight. The climb entry is then identical to entry from cruising airspeed, except that power must be increased simultaneously to the climb setting as the pitch attitude is increased. Climb entries on partial panel are more easily and accurately…

• Instrument Flying Handbookp. 7-17
  Chapter 7, Section I: Airplane Basic Flight Maneuvers › Straight Climbs and Descents › Leveling Off

  level off at an airspeed higher than descending speed. At the lead point, add power to the appropriate level flight cruise setting. [Figure 7-31] Since the nose tends to rise as the airspeed increases, hold forward elevator pressure ... attitude for the airspeed selected. To level off from a descent at descent airspeed, lead the desired altitude by approximately 50 feet, simultaneously adjusting the pitch attitude to level flight and adding power to a setting that holds the airspeed…