CP.IX.B.R3

From the FAA library

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

  same manner as 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 ... undesirable characteristic. This makes it easy for the pilot to inadvertently overstress an aircraft. Stability and Center of Gravity Limits for the location of the CG are established by the manufacturer. These are the fore and aft limits beyond which…

• Pilot's Handbook of Aeronautical Knowledgep. 5-45
  Chapter 5: Aerodynamics of Flight › High Speed Flight › Speed Ranges

  VMO/MMO is defined as the maximum operating limit speed. VMO is expressed in knots calibrated airspeed (KCAS), while MMO is expressed in Mach number. The VMO limit is usually associated with operations at lower altitudes and deals with structural loads ... flutter. The MMO limit is associated with operations at higher altitudes and is usually more concerned with compressibility effects and flutter. At lower altitudes, structural loads and flutter are of concern; at higher altitudes, compressibility effects and flutter…

• Pilot's Handbook of Aeronautical Knowledgep. 1-16
  Chapter 1: Introduction To Flying › Pilot Certifications

  depending on the type of certificates sought. [Figure 1-20] Each type of pilot’s certificate has privileges and limitations that are inherent within the certificate itself. However, other privileges and limitations may be applicable based on the aircraft type ... operation being conducted, and the type of certificate. For example, a certain certificate may have privileges and limitations under 14 CFR part 61 and part 91. Figure 1-20. Front side (top) and back side (bottom) of an airman certificate…

• Pilot's Handbook of Aeronautical Knowledgep. 8-18
  Chapter 8: Flight Instruments › Instrument Check › Attitude Indicator

  spins in the horizontal plane and resists deflection of the rotational path. Since the gyro relies on rigidity in space, the aircraft actually rotates around the spinning gyro. Figure 8-23. Attitude indicator. An adjustment knob is provided with which ... wings overlap the horizon bar when the aircraft is in straight-and-level cruising flight. The pitch and bank limits of an attitude indicator depend upon the make and model of the instrument. Some attitude indicators have limits…

• Pilot's Handbook of Aeronautical Knowledgep. 9-3
  Chapter 9: Flight Manuals and Other Documents › Weight and Loading Distribution

  weight and balance section of the AFM/POH. Figure 9-4. Manifold pressure gauge (top) and tachometer (bottom). Flight Limits Flight Limits list authorized maneuvers with appropriate entry speeds, flight load factor limits, and types of operation limits. It also indicates ... those maneuvers that are prohibited, such as spins or acrobatic flight, as well as operational limitations such as flight into known icing conditions. Placards Most aircraft display one or more placards that contain information having a direct bearing…

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

  less than this does not provide negative lift capability sufficient to damage the aircraft from excessive flight loads. The limit airspeed (or redline speed) is a design reference point for the aircraft—this aircraft is limited ... flight is attempted beyond the limit airspeed, structural damage or structural failure may result from a variety of phenomena. The aircraft in flight is limited to a regime of airspeeds and Gs that do not exceed the limit (or redline…