IL.X.A.R4
Risk managementAirframe and airspeed limitations.
From the FAA library
- Chapter 9: Flight Manuals and Other Documents › General (Section 1)
also be included. Limitations (Section 2) The Limitations section contains only those limitations required by regulation or that are necessary for the safe operation of the aircraft, powerplant, systems, and equipment. It includes operating limitations, instrument markings, color-coding ... basic placards. Some of the limitation areas are airspeed, powerplant, weight and loading distribution, and flight…
- Glossary › Pilot’s Operating Handbook/Airplane Flight Manual
surface, brought on by exceeding the critical angle of attack. A stall can occur at any pitch attitude or airspeed. Standard atmosphere. At sea level, the standard atmosphere consists of a barometric pressure of 29.92 inches of mercury ... Standard empty weight (GAMA). This weight consists of the airframe, engines, and all items of operating equipment that have fixed locations and are permanently installed in the airplane including fixed ballast, hydraulic fluid, unusable fuel, and full engine oil. Standard…
- Glossary › Domestic Reduced Vertical Separation Minimum
extended for takeoffs and landings to increase the amount of aerodynamic lift that is produced at any given airspeed. Leans, the. A physical sensation caused by an abrupt correction of a banked attitude entered too slowly to stimulate the motion ... create the illusion of banking in the opposite direction. Licensed empty weight. The empty weight that consists of the airframe, engine(s), unusable fuel, and undrainable oil plus standard and optional equipment as specified in the equipment list. Some manufacturers…
- 14 CFR Part 135 — Operating Requirements: Commuter and on Demand Operations and Rules Governing Persons on Board Such AircraftOpen14 CFR Part 135, Appendix A to Part 135—Additional Airworthiness Standards for 10 or More Passenger Airplanes
airplane. (f) Airspeeds, as indicated airspeeds, corresponding to those determined for takeoff under section 5(b). 21. Maximum operating altitudes. The maximum operating altitude to which operation is allowed, as limited by flight, structural, powerplant, functional, or equipment characteristics, must ... restarting turbine engines in flight (including the effects of altitude) must be set forth in the Airplane Flight Manual. Airframe Requirements Flight Loads 24. Engine torque. (a) Each turbopropeller engine mount and its supporting structure must be designed…
- Chapter 3: Basic Flight Maneuvers › Effect and Use of Flight Controls › Feel of the Airplane
instrumentation is often called “feeling the airplane.” Examples of this “feel” may be sounds of the airflow across the airframe, vibrations felt through the controls, engine and propeller sounds and vibrations at various flight attitudes, and the sensations felt ... provide the pilot with critical information about changes in the airplane’s direction and speed; however, there are limits in kinesthetic sense when relied upon solely without visual information, as when flying in instrument meteorological conditions (IMC). Sole reliance…
- Chapter 10: Aircraft Systems › Pitot-Static Pressure-Sensing Flight Instruments › Airspeed Indicators
artificial horizon display. Refer to Figure 10-4 showing T configuration. Complications continue when considering airspeed indications and operating limitations. It is very important to keep high-speed aircraft from traveling faster than the speed of sound if they ... designed to do so. Even as an aircraft approaches the speed of sound, certain parts on the airframe may experience airflows that exceed it. The problem with this is that near the speed of sound, shock waves can develop that…