IL.VIII.H.S3
SkillEstablish a positive rate of climb and the appropriate airspeed ±10 knots.
From the FAA library
- Chapter 5: Aerodynamics of Flight › Aerodynamic Forces in Flight Maneuvers › Forces in Climbs
Figure 5-35. Normal, slipping, and skidding turns at a constant altitude. If the climb is entered with no change in power setting, the airspeed gradually diminishes because the thrust required to maintain a given airspeed in level flight ... insufficient to maintain the same airspeed in a climb. When the flight path is inclined upward, a component of the aircraft’s weight acts in the same direction as, and parallel to, the total drag of the aircraft, thereby increasing…
- 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…
- Appendix C: Certificates, Ratings, and Endorsements › Flight Instructor Endorsements
training and make logbook endorsements for pilots who are already certificated such as sport, recreational, private, commercial, and instrument rated pilots, as well as for other flight instructors. Typical endorsements include but are not limited to flight reviews, instrument proficiency ... additional training required for high performance, high altitude, and tail wheel aircraft, and types of glider launches. Additional rating applicants (e.g., multiengine add-on, seaplane add-on, glider add-on, helicopter add-on) are rated pilots and not considered student…
- Chapter 8: Flight Instruments › Airspeed Indicator Markings
never exceed speed. Operating above this speed is prohibited since it may result in damage or structural failure. Other Airspeed Limitations Some important airspeed limitations are not marked on the face of the ASI, but are found on placards ... These airspeeds include: Design maneuvering speed (VA)—the maximum speed at which the structural design’s limit load can be imposed (either by gusts or full deflection of the control surfaces) without causing structural damage. It is important to consider…
- Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Landing Performance
could be accepted. There is a light rain and the winds are out of the east at ten knots. The pilot accepts because he or she is approaching the extended centerline of runway 27. The turn is tight ... feet AGL, the pilot is already 1,000 feet down the 3,500 feet runway. The airspeed is still high by about ten percent (should be at 70 knots and is at about 80 knots). The wind of ten knots…
- 14 CFR Part 141, Appendix G to Part 141—Flight Instructor Instrument (For an Airplane, Helicopter, or Powered-Lift Instrument Instructor Rating, as Appropriate) Certification Course
Part 141, Appendix G to Part 141—Flight Instructor Instrument (For an Airplane, Helicopter, or Powered-Lift Instrument Instructor Rating, as Appropriate) Certification Course 1. Applicability. This appendix prescribes the minimum curriculum for a flight instructor instrument certification course required ... under this part, for the following ratings: (a) Flight Instructor Instrument—Airplane. (b) Flight Instructor Instrument—Helicopter. (c) Flight Instructor Instrument—Powered-lift aircraft. 2. Eligibility for enrollment. A person must hold the following prior to enrolling in the flight…