JPATS Weather - NETC
JPATS Weather - NETC
JPATS Weather - NETC
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<strong>JPATS</strong> AVIATION WEATHER BOOKLET<br />
When aircraft fly pressure altitudes, they are assigned a flight level (FL) of three digits, representing<br />
hundreds of feet above 29.92. As an example, an aircraft assigned FL250 (pronounced “flight level<br />
two five zero”) would be flying a pressure altitude, and the pilot would fly the aircraft so that the<br />
altimeter reads 25,000 feet with 29.92 in the Kollsman window. These above altitude definitions are<br />
illustrated in Figure 1-5.<br />
Figure 1-5 — Altitudes<br />
Density altitude (DA) is pressure altitude corrected for nonstandard temperature deviations. On a<br />
hot day, air molecules are farther apart, decreasing the air density and increasing the density<br />
altitude. In this situation, the DA of an airfield would be higher than both the published field<br />
elevation and the pressure altitude. The opposite is true on a colder day: Increased air density causes<br />
a decreased density altitude and a DA lower than the published field elevation and the pressure<br />
altitude.<br />
Density altitude is not a height reference; rather, it is an index to aircraft performance. It affects<br />
airfoil, engine, propeller, and rotor performance. Thrust is reduced because a jet engine has less<br />
mass (air) to compress. Lift is also reduced due to thinner air. Additionally, higher density<br />
altitudes result in longer takeoff and landing distances and a reduced rate of climb. Takeoff<br />
distances are longer since reduced thrust requires a longer distance to accelerate to takeoff speed.<br />
Landing distances are longer since a higher true airspeed is required to land at the same indicated<br />
airspeed. Climb rate is decreased because of reduced available thrust. At certain high density<br />
altitudes, takeoffs and/or single-engine flight (loss of one engine after becoming airborne) are not<br />
possible due to limitations of thrust, lift, and runway length. Table 1-1 summarizes the effects of<br />
temperature on aircraft performance. Moisture affects aircraft performance in the same manner<br />
as temperature, but to a much lesser degree.<br />
HIGH TEMPERATURE OR MOISTURE<br />
Lower Air Density<br />
LOW TEMPERATURE OR MOISTURE<br />
Higher Air Density<br />
1-7 Version 3.2/Dec 08