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2. Consider the situation where an airport with elevation 2500 ft AMSL and mean daily maximum temperature of the hottest month of 100, is planning

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2. Consider the situation where an airport with elevation 2500 ft AMSL and mean daily maximum temperature of the hottest month of 100, is planning for a new runway to be designed for the T- 39 aircraft at 60 percent useful load. CANT # Engines 2 Aircraft Mustang Eclipse 500 Hondajet Manufacturer Cessna Edipse Honda Avg. # Seats 5 5 5 Runway Required 3.100 2,400 3.100 2 2 2 Very Light Jet Aircraft Wingspan Length MSTOW (15) 43'2" 40"7" 8,645 33'6" 33'6 5,995 39'10" 418 9.200 Business Jet Aircraft 46'11" 427" 10,800 56'4" 52'6" 36,400 47'9" 576" 21.500 43'9" 58'6" 23,500 5404" 51'02" 28.000 77'10" 88'04" 73,200 93'06" 96'05" 85,100 5 2 10 9 Citation CJ1 Citation X Lear 45 XR Lear 60 XR Hawker 850 XP G-IV G-550 2 Cessna Cessna Bombardier Bombardier Beechcraft Gulfstream Gulfstream 2 9 3,300 3.560 5.040 3,400 5,200 5,000 5,150 2 2 2 8 19 19 "Runway lengths are takeoff runway length estimates based on sea level elevation, temperature 20C at maximum takeoff weight. It should be noted that required runway length varies considerably based on aircraft weight and local atmospheric conditions TABLE 22 Characteristics of General Aviation Aircraft (Continued) Menu Model Arse B01 C 125-700 Recht 400A Hecht Puma tech 2000 Madel 10 De en 20 Falcon SO/10 DX D 00/000 urel Arorat It Commander stres 1121 Wend 112/11 20 S Challenge 100 500 C 101 Citatione Citation / 52SA C C:21 350 Cena Ce 31/1NIA ER 35/36/ Manufacturer Bae Bombardier Bombardier Bombardier Bombardier Cesta Cessna Cessna Dassault Dassualt Israel Aircraft Industries (IAI IAI Learjet Learjet Learjet Raytheon/wer Raytheon/wer Raytheon/Hawker Sabriner Model Corporate 800/1000 600 Challenger 601/601-3A/3ER Challenger 604 Challenger BD 100 Continental 5550 Citation / 650 Citation / 750 Citation X Falcon 9000/900EX Falicon 2000/2000EX Astra 1125 Galaxy 1126 45 XR 55/55B/55C 60 Horvo 800/800 XP 1000 65/75 40/45 55 C SIC / M300 D 300 m Haytheon How 400/400 Ce Hathon Gen Saber 40/60 560 Encore 56D/ CE se Citation V U 650 CV Cews TSA Geen 50 S. TARE 6-6 Aircraft that including those in Table 6-1) Make Up 100 AAACH5 9.000 9.000 EXAMPLE TEMP OF AIRPORT ELEV SL RUNWAY LENGTH 4.0 B000 CLIMB LIMITATION B.BOY 8,500 8.500 6.000 8,000 8,000 CLIMA LIMITATION 7.700 7,500 7.500 3.000 7,000 AIRPORT ELEVATION SERTA 7,000 RUNWAY LENGTHS (FEET) 6,500 . 6,500 2.000 6.000 4000 6.000 AIRPORT ELEVATION FEET) 5,500 5,500 5.000 5,000 4,500 80 EXAMPLE TEMP 100" 4,500 AIRPORT ELEV- 1.000 4,000 RUNWAY LENGTH7550 40 50 60 70 80 90 100 110 40 50 60 70 4,000 90 100 110 Mean Daily Maximum Temperature of Hottest Month of the Year in Degrees Fahrenheit 75 percent of feet at 60 percent 75 percent of feet at 90 percent useful load useful load FIGURE 6-14 Seventy-five percent of fleet at 60 or 90 percent useful load. RUNWAY LENGTH (FEET) VRTION ET CLIMS LIMITATION 11.000 11,000 GLIME LIMITATION 11.000 11,000 10.500 10,500 10,000 10,000 9,500 9,500 9,000 9,000 8,500 8,500 8,000 8.000 7,500 7,500 7,000 7.000 6.500 6.500 6,000 6.000 5.500 5,500 5.000 5,000 EXAMPLE EXAMPLE TEM TEMPT 4,500 ELEV.2.000 ELEVATION 4,000 IRWAY LENGTI 5.00 RIWAYLENETO 40 50 60 70 80 90 100 110 40 50 60 70 80 Moan Daily Maximum Temperature of Hottest Month of the Year in Degrees Fahrenheit 100 percent of foot at 60 percent 100 percent of feet at 90 percent useful load useful load RUNWAY LENGTH (FEET) BURVIRON 4.500 90 100 118.000 2. Consider the situation where an airport with elevation 2500 ft AMSL and mean daily maximum temperature of the hottest month of 100, is planning for a new runway to be designed for the T- 39 aircraft at 60 percent useful load. CANT # Engines 2 Aircraft Mustang Eclipse 500 Hondajet Manufacturer Cessna Edipse Honda Avg. # Seats 5 5 5 Runway Required 3.100 2,400 3.100 2 2 2 Very Light Jet Aircraft Wingspan Length MSTOW (15) 43'2" 40"7" 8,645 33'6" 33'6 5,995 39'10" 418 9.200 Business Jet Aircraft 46'11" 427" 10,800 56'4" 52'6" 36,400 47'9" 576" 21.500 43'9" 58'6" 23,500 5404" 51'02" 28.000 77'10" 88'04" 73,200 93'06" 96'05" 85,100 5 2 10 9 Citation CJ1 Citation X Lear 45 XR Lear 60 XR Hawker 850 XP G-IV G-550 2 Cessna Cessna Bombardier Bombardier Beechcraft Gulfstream Gulfstream 2 9 3,300 3.560 5.040 3,400 5,200 5,000 5,150 2 2 2 8 19 19 "Runway lengths are takeoff runway length estimates based on sea level elevation, temperature 20C at maximum takeoff weight. It should be noted that required runway length varies considerably based on aircraft weight and local atmospheric conditions TABLE 22 Characteristics of General Aviation Aircraft (Continued) Menu Model Arse B01 C 125-700 Recht 400A Hecht Puma tech 2000 Madel 10 De en 20 Falcon SO/10 DX D 00/000 urel Arorat It Commander stres 1121 Wend 112/11 20 S Challenge 100 500 C 101 Citatione Citation / 52SA C C:21 350 Cena Ce 31/1NIA ER 35/36/ Manufacturer Bae Bombardier Bombardier Bombardier Bombardier Cesta Cessna Cessna Dassault Dassualt Israel Aircraft Industries (IAI IAI Learjet Learjet Learjet Raytheon/wer Raytheon/wer Raytheon/Hawker Sabriner Model Corporate 800/1000 600 Challenger 601/601-3A/3ER Challenger 604 Challenger BD 100 Continental 5550 Citation / 650 Citation / 750 Citation X Falcon 9000/900EX Falicon 2000/2000EX Astra 1125 Galaxy 1126 45 XR 55/55B/55C 60 Horvo 800/800 XP 1000 65/75 40/45 55 C SIC / M300 D 300 m Haytheon How 400/400 Ce Hathon Gen Saber 40/60 560 Encore 56D/ CE se Citation V U 650 CV Cews TSA Geen 50 S. TARE 6-6 Aircraft that including those in Table 6-1) Make Up 100 AAACH5 9.000 9.000 EXAMPLE TEMP OF AIRPORT ELEV SL RUNWAY LENGTH 4.0 B000 CLIMB LIMITATION B.BOY 8,500 8.500 6.000 8,000 8,000 CLIMA LIMITATION 7.700 7,500 7.500 3.000 7,000 AIRPORT ELEVATION SERTA 7,000 RUNWAY LENGTHS (FEET) 6,500 . 6,500 2.000 6.000 4000 6.000 AIRPORT ELEVATION FEET) 5,500 5,500 5.000 5,000 4,500 80 EXAMPLE TEMP 100" 4,500 AIRPORT ELEV- 1.000 4,000 RUNWAY LENGTH7550 40 50 60 70 80 90 100 110 40 50 60 70 4,000 90 100 110 Mean Daily Maximum Temperature of Hottest Month of the Year in Degrees Fahrenheit 75 percent of feet at 60 percent 75 percent of feet at 90 percent useful load useful load FIGURE 6-14 Seventy-five percent of fleet at 60 or 90 percent useful load. RUNWAY LENGTH (FEET) VRTION ET CLIMS LIMITATION 11.000 11,000 GLIME LIMITATION 11.000 11,000 10.500 10,500 10,000 10,000 9,500 9,500 9,000 9,000 8,500 8,500 8,000 8.000 7,500 7,500 7,000 7.000 6.500 6.500 6,000 6.000 5.500 5,500 5.000 5,000 EXAMPLE EXAMPLE TEM TEMPT 4,500 ELEV.2.000 ELEVATION 4,000 IRWAY LENGTI 5.00 RIWAYLENETO 40 50 60 70 80 90 100 110 40 50 60 70 80 Moan Daily Maximum Temperature of Hottest Month of the Year in Degrees Fahrenheit 100 percent of foot at 60 percent 100 percent of feet at 90 percent useful load useful load RUNWAY LENGTH (FEET) BURVIRON 4.500 90 100 118.000

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