IL.XV.A.R11

From the FAA library

• Pilot's Handbook of Aeronautical Knowledgep. 5-38
  Chapter 5: Aerodynamics of Flight › Load Factors › Vg Diagram

  excessive flight loads. The limit airspeed (or redline speed) is a design reference point for the aircraft—this aircraft is limited to 225 mph. If flight is attempted beyond the limit airspeed, structural damage or structural failure may result from ... variety of phenomena. The aircraft in flight is limited to a regime of airspeeds and Gs that do not exceed the limit (or redline) speed, do not exceed the limit load factor, and cannot exceed the maximum lift capability…

• Pilot's Handbook of Aeronautical Knowledgep. 9-13
  Chapter 10: Weight and Balance

  such as ADs, provide pilots with ready access to pertinent information needed to safely fly a particular aircraft. By understanding the operations, limitations, and performance characteristics of the aircraft, the pilot can make educated flight decisions. By learning what preventive ... essential tools used to reach that goal. Chapter 10: Weight and Balance Compliance with the weight and balance limits of any aircraft is critical to flight safety. Operating above the maximum weight limitation compromises the structural integrity of an aircraft…

• Pilot's Handbook of Aeronautical Knowledgep. 5-37
  Chapter 5: Aerodynamics of Flight › Load Factors › Rough Air

  speed. Regardless of the speed held, there may be gusts that can produce loads that exceed the load limits. Each specific aircraft is designed with a specific G loading that ... imposed on the aircraft without causing structural damage. There are two types of load factors factored into aircraft design: limit load and ultimate load. The limit load is a force applied to an aircraft that causes a bending…

• Pilot's Handbook of Aeronautical Knowledgep. 10-3
  Chapter 10: Weight and Balance › Balance, Stability, and Center of Gravity › Stability

  those mentioned for an excess weight condition. It is vital to comply with weight and balance limits established for all aircraft. Operating above the maximum weight limitation compromises the structural integrity of the aircraft and can adversely affect performance. Stability ... fore and aft limits beyond which the CG should not be located for flight. These limits are published for each aircraft in the Type Certificate Data Sheet (TCDS), or aircraft specification and the AFM or pilot’s operating handbook…

• Aviation Instructor's Handbookp. 1-4
  Chapter 1: Risk Management and Single-Pilot Resource Management › Implementing the Risk Management Process › The Pave Checklist

  personal minimums for items in each risk category. These are limits unique to that individual pilot’s current level of experience and proficiency. For example, the aircraft may have a maximum crosswind component of 15 knots listed in the aircraft ... IMSAFE checklist (described later in this chapter) combined with proficiency, recency, and currency helps provide the answer. A = Aircraft What limitations will the aircraft impose upon the trip? Ask the following questions: ⦁ Is this the right aircraft for the flight…

• Pilot's Handbook of Aeronautical Knowledgep. 5-14
  Chapter 5: Aerodynamics of Flight › Aircraft Design Characteristics

  original flight path. It is primarily an aircraft design characteristic. The flight paths and attitudes an aircraft flies are limited by the aerodynamic characteristics of the aircraft, its propulsion system, and its structural strength. These limitations indicate the maximum performance ... utility, it must be safely controllable to the full extent of these limits without exceeding the pilot’s strength or requiring exceptional flying ability. If an aircraft is to fly straight and steady along any arbitrary flight path, the forces…