FAA HANDBOOK — EDUCATIONAL REFERENCE

Altitude and Flight

FAA-H-8083-25C — Chapter 12. Weather Theory

Official text — PHAK Chapter 12

FAA HANDBOOK — EDUCATIONAL REFERENCE

Altitude affects every aspect of flight from aircraft performance to human performance. At higher altitudes, with a decreased atmospheric pressure, takeoff and landing distances are increased, while climb rates decrease. When an aircraft takes off, lift is created by the flow of air around the wings. If the air is thin, more speed is required to obtain enough lift for takeoff; therefore, the ground run Pressure Altitude: Sea level 745 feet Pressure Altitude: 8,000 feet 1,590 feet Atmosphere Station Pressure New Orleans 29.92 "Hg New Orleans 29.92 "Hg el pressure. is longer. An aircraft that requires 745 feet of ground run at sea level requires more than double that at a pressure altitude of 8,000 feet. [Figure 12-9]. It is also true that at higher altitudes, due to the decreased density of the air, aircraft engines and propellers are less efficient. This leads to reduced rates of climb and a greater ground run for obstacle clearance.

Reproduced from the FAA Pilot’s Handbook of Aeronautical Knowledge (FAA-H-8083-25C). The PHAK is an educational reference, not regulation. Figures and tables from the original are not reproduced here — consult the official PDF for those.

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