Aircraft Performance | Aeronautical Knowledge

Aircraft Performance

Aeronautical Knowledge, Flying Training

The performance or operational information section of the Aircraft Flight Manual/Pilot’s Operating Handbook (AFM/ POH) contains the operating data for the aircraft; that is, the data pertaining to takeoff, climb, range, endurance, descent, and landing. The use of this data in flying operations is mandatory for safe and efficient operation. Considerable knowledge and familiarity of […]

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Aircraft Performance Charts

Aeronautical Knowledge, Flying Training

Performance charts allow a pilot to predict the takeoff, climb, cruise, and landing performance of an aircraft. These charts, provided by the manufacturer, are included in the AFM/POH. Information the manufacturer provides on these charts has been gathered from test flights conducted in a new aircraft, under normal operating conditions while using average piloting skills,

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Performance Speeds of the Aircraft

Aeronautical Knowledge, Flying Training

True airspeed (TAS)—the speed of the aircraft in relation to the air mass in which it is flying. Indicated airspeed (IAS)—the speed of the aircraft as observed on the ASI. It is the airspeed without correction for indicator, position (or installation), or compressibility errors. Calibrated airspeed (CAS)—the ASI reading corrected for position (or installation) and

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Aircraft Takeoff and Landing Performance

Aeronautical Knowledge, Flying Training

The majority of pilot-caused aircraft accidents occur during the takeoff and landing phase of flight. Because of this fact, the pilot must be familiar with all the variables that influence the takeoff and landing performance of an aircraft and must strive for exacting, professional procedures of operation during these phases of flight. Takeoff and landing

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Pressure Altitude and Density Altitude

Aeronautical Knowledge, Flying Training

Pressure Altitude Pressure altitude is the height above the standard datum plane (SDP). The aircraft altimeter is essentially a sensitive barometer calibrated to indicate altitude in the standard atmosphere. If the altimeter is set for 29.92 “Hg SDP, the altitude indicated is the pressure altitude—the altitude in the standard atmosphere corresponding to the sensed pressure.

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