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For aircraft greater than 60,000 lb MGTOW, runway lengths are estimated based on the specific performance specifications of the critical aircraft These performance specifications may be found in the published aircraft airport planning manuals These manuals may be found on the Internet sites of the major aircraft manufacturers Within the aircraft airport planning manuals are performance charts that are used to determine the aircraft s required runway lengths for both takeoff and landing, based on the aircraft s operating configuration, its estimated weights during takeoff and landing, as well as the airport elevation and average high temperature during the hottest month Example Problem 6-2 illustrates the procedure for estimating runway length using these charts
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Example Problem 6-2 Consider the situation where an airport with elevation 1000 ft AMSL and mean daily maximum temperature of the hottest month of 84 F, is planning for a new runway to be designed for the Boeing 737-900 aircraft, equipped with Pratt & Whitney CFM56-7B27 engines At the airport a runway gradient of 20 ft is projected According to the performance specification chart, illustrated in Fig 6-16, found in the Boeing 737-900 airport planning manual, the maximum design landing weight for the aircraft is 146,300 lb and the maximum design takeoff weight is 174,200 lb First, estimation of required runway length for landing is performed using the landing runway length performance chart for the aircraft As with most landing performance charts, runway length requirements found landing may be found under both dry and wet runway conditions For airport planning purposes, design runway length for landing is estimated by considering wet runway conditions If a landing runway length performance chart does not include wet runway conditions, the design runway length is estimated as the runway length found under dry runway conditions, plus 15 percent Figure 6-17 illustrates this example Applying the case example, a vertical line is drawn from the base of the horizontal axis at the location of the maximum design landing weight (146,300 lb), up to an interpolated point between the sea level and 2000 ft (to represent the example airport s 1000 ft elevation) wetrunway curves, and then a horizontal line is drawn to the vertical axis, where the estimated required runway length may be found In this example, the estimated runway length for landing is approximately 6600 ft
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CHARACTERISTICS MAX DESIGN TAXI WEIGHT MAX DESIGN TAKEOFF WEIGHT MAX DESIGN LANDING WEIGHT MAX DESIGN ZERO FUEL WEIGHT OPERATING EMPTY WEIGHT (1) MAX STRUCTURAL PAYLOAD SEATING CAPACITY (1)
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UNITS POUNDS KILOGRAMS POUNDS KILOGRAMS POUNDS KILOGRAMS POUNDS KILOGRAMS POUNDS KILOGRAMS POUNDS KILOGRAMS TWO-CLASS ALL-ECONOMY Landing Weight Takeoff Weight
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737 900 164,500 74,616 164,000 174,700 79,243 174,200 79,016 146,300 66,361 138,300 140,300 63,639 94,580 42,901 43,720 19,831 177 189 1,835 520 6875 26,022 46,063 20,894 45,720 20,738 177 189 1,835 520 6875 26,022 46,063 20,894
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NOTE: (1) OPERATING EMPTY WEIGHT FOR BASELINE MIXED CLASS CONFIGURATION CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS
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FIGURE 6-16 Boeing 737 900 general airplane characteristics (Boeing Corp document #D6-58325-3 and FAA AC 150/5325-4B)
These charts are designed for level runways An adjustment for runway gradient must be made by adding 10 ft of runway length for every foot of runway gradient In this example, an additional 200 ft of runway length is added, resulting in an adjusted runway length for landing of 6800 ft Second, estimation of required runway length for takeoff is performed using the takeoff runway length performance chart for the aircraft Oftentimes, an aircraft will have multiple takeoff performance charts, typically for different average high temperatures The chart associated with the temperature nearest the airport s average high during the hottest month is used