Figure 1-20. Airport/runway analysis example.  1-21  Sample Aircraft  Engine Type  Flaps 0  KAPA/APA  Denver - Centennial  Runway Conditions: Dry  Elevation = 5883 ft  OAT  F  C  N1  A/1  ON  SEC.  SEG.  CLIMB  10  17L  17R  28  35L  35R  Max Structural Takeoff Weight Limit = 28000  Runways - lbs  50  52  54  55  57  59  61  63  10  11  12  13  14  15  16  17  98.91  98.73  98.56  98.47  98.29  98.11  97.95  97.80  97.11  21880 R  21750 R  21620 R  21550 R  21420 R  21290 R  21160 R  21020 R  29380 C  29340 C  29190 C  29100 C  28950 O  28790 O  28620 O  28450 O  25250 R  25070 R  24900 R  24820 R  24650 R  24490 R  24320 R  24160 R  26690 R  26500 R  26310 R  26210 R  26020 R  25830 R  25650 R  25460 R  29460 C  29460 C  29460 C  29460 C  29460 C  29460 C  29360 C  29210 C  21210 R  21090 R  20950 R  20890 R  20750 R  20620 R  20490 R  20360 R  29000  29000  29000  29000  29000  29000  29000  29000  64  66  68  70  18  19  20  21  97.72  97.56  97.40  97.20  20960 R  20820 R  20670 R  20530 R  28360 O  28170 O  27980 O  27720 O  24080 R  23930 R  23770 R  23610 R  25370 R  25180 R  25000 R  24810 R  29120 C  28870 R  28630 R  28380 R  20300 R  20170 R  20030 R  19880 R  29000  29000  28930  28630  72  73  75  77  22  23  24  25  97.00  96.90  96.70  96.50  20380 R  20310 R  20170 R  20020 R  27460 O  27370 R  27110 R  26860 R  23420 O  23340 O  23170 O  22990 O  24630 R  24530 R  24350 R  24150 R  28110 R  27970 R  27690 R  27390 R  19740 R  19670 R  19530 R  19390 R  28330  28180  27870  27570  79  81  82  84  26  27  28  29  96.24  95.97  95.84  95.58  19880 R  19710 R  19630 R  19460 R  26590 R  26330 R  26190 R  25920 R  22810 O  22630 O  22540 O  22320 O  23960 R  23760 R  23660 R  23460 R  27100 R  26800 R  26650 R  26350 R  19240 R  19070 R  18990 R  18820 R  27230  26890  26720  26380  86  88  90  91  30  31  32  33  95.31  95.04  94.77  94.64  19290 R  19130 R  18980 R  18900 R  25610 R  25300 R  24990 R  24840 R  22120 O  21930 O  21730 O  21630 O  23260 R  23070 R  22870 R  22770 R  26050 C  25740 C  25440 C  25290 C  18650 R  18490 R  0 R  0 R  26040  25690  25350  25180  93  95  34  35  94.37  94.10  18740 R  18590 R  24530 R  24220 R  21440 O  21240 O  22570 R  22380 R  24990 C  24690 C  0 R  0 R  24830  24490  RUNWAY DIM  Length = ft  Slope = %  4800  –0.62  10002  0.9  7000  0.93  7000  –0.93  10002  –0.9  4800  0.62  --- --- LVLOFF ALT  ft  7383  7383  7383  7383  7383 7383  --- WIND CORR  lbs/kt hw  lbs/kt tw  67  N/A  5  –254  31  –227  42  –223  4  –131  62  N/A  --- --- QNH  lbs/.1"Hg > 29.92  lbs/.1"Hg < 29.92  75  –87  10  –127  85  –99  88  –113  5  –114  0  –86  0  –123  ANTI-ICE  lbs  –1210  –1400  –1480  –1690  –830 –1180  –70  LIMIT CODES  R = RUNWAY LIMIT  O = OBSTACLE LIMIT  B = BRAKE LIMIT  C = CLIMB LIMIT  DATE: 07/01/2011  FOR SAMPLE USE ONLY 