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airport/documents/Mesquite Master Plan Final.pdf - The City of ...

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Haul Length<br />

<strong>The</strong> FAA Computer Program also<br />

provides an estimation <strong>of</strong> runway<br />

lengths for general aviation aircraft<br />

weighing more than 60,000 pounds.<br />

This group includes the Gulfstream<br />

family <strong>of</strong> aircraft and some new longrange<br />

corporate jets. <strong>The</strong> estimate <strong>of</strong><br />

runway length requirements for the<br />

large corporate aircraft over 60,000<br />

pounds considers all airfield data, but<br />

also considers the typical haul distance.<br />

<strong>The</strong> origin/destination <strong>of</strong> many aircraft<br />

utilizing the <strong>airport</strong> was previously<br />

identified in Table 3C. <strong>The</strong> larger<br />

Gulfstream jets had haul lengths <strong>of</strong><br />

nearly 1,400 miles, to destinations such<br />

as Palm Springs, California, and Palm<br />

Beach, Florida. Other destinations<br />

included St. Paul, MN (1,000 mi.),<br />

Jackson Hole, WY (1,400 mi.),<br />

Kissimmee, FL (1,100 mi.), and Black<br />

Hills, SD (1,100 mi.). Since it is known<br />

that, when conditions allow, business<br />

jet operators are opting for longer haul<br />

lengths, consideration will be given to<br />

accommodate aircraft weighing more<br />

than 60,000 pounds with haul lengths<br />

<strong>of</strong> 1,400 miles. As indicated in Table<br />

3G, aircraft weighing more than 60,000<br />

pounds, with haul lengths <strong>of</strong> 1,400<br />

miles, require a runway length <strong>of</strong> 6,900<br />

feet.<br />

Specific Aircraft Requirements<br />

An additional consideration for runway<br />

length is to analyze the runway length<br />

requirements <strong>of</strong> specific aircraft<br />

currently utilizing or planned to utilize<br />

<strong>Mesquite</strong> Metro Airport in the future.<br />

Table 3J presents the runway length<br />

3-17<br />

needs for a wide variety <strong>of</strong> business jets,<br />

as obtained from the operations<br />

manuals for each aircraft. Figures in<br />

the table consider maximum take-<strong>of</strong>f<br />

and landing weights. It should be noted<br />

that landing length requirements<br />

during contaminated runway conditions<br />

(rainy, with 1/10-inch <strong>of</strong> water on the<br />

runway) increase significantly for<br />

aircraft with single landing gear<br />

configurations due to hydroplaning<br />

potential.<br />

In general, the data specific to each<br />

airplane presented in Table 3J is<br />

similar to the generalized output by the<br />

FAA computer program (presented in<br />

Table 3G). Obviously, <strong>airport</strong> planning<br />

cannot always conform to the worst case<br />

(maximum load) scenario. <strong>Plan</strong>ning<br />

should at least conform to providing a<br />

runway length capable <strong>of</strong> accommodating<br />

the majority <strong>of</strong> aircraft, the<br />

majority <strong>of</strong> the year. In other words,<br />

the runway should be capable <strong>of</strong><br />

handling business jets with typical<br />

weight loading during moderate heat<br />

conditions.<br />

Several aircraft which currently utilize<br />

the <strong>airport</strong> on an infrequent basis can<br />

require runway lengths longer than<br />

6,000 feet. <strong>The</strong> Lear 55, Gulfstream IV<br />

and V, Hawker 800, and Challenger<br />

require up to 7,000 feet. <strong>The</strong>se aircraft<br />

are capable <strong>of</strong> operating at the <strong>airport</strong>,<br />

but are weight-restricted during hot<br />

weather days. Weight restrictions can<br />

include taking less fuel and making an<br />

additional stop along the intended<br />

route, boarding fewer passengers, or<br />

taking less cargo. During cooler days,<br />

the weight restrictions could be minor<br />

or may be unnecessary.

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