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Page Title: Table 1-5.—Pressure Altitude Values
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COMPUTATION OF AIRCRAFT PERFORMANCE INDICATORS FROM OBSERVED DATA
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Aerographers Mate, Module 01-Surface Weather Observations
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DENSITY  ALTITUDE

Table 1-5.—Pressure Altitude Values Hundredths ® 0.00 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 PRESSURE inches & PRESSURE ALTITUDE (FEET) ¯ tenths ¯ 28.0 1824 1814 1805 1795 1785 1776 1766 1756 1746 1737 28.1 1727 1717 1707 1698 1688 1678 1668 1659 1649 1639 28.2 1630 1620 1610 1601 1591 1581 1572 1562 1552 1542 28.3 1533 1523 1513 1504 1494 1484 1475 1465 1456 1446 28.4 1436 1427 1417 1407 1398 1388 1378 1369 1359 1350 28.5 1340 1330 1321 1311 1302 1292 1282 1273 1263 1254 28.6 1244 1234 1225 1215 1206 1196 1186 1177 1167 1138 28.7 1148 1139 1129 1120 1110 1100 1091 1081 1072 1062 28.8 1053 1043 1034 1024 1015 1005 995 986 976 967 28.9 957 948 938 929 919 910 900 891 881 872 29.0 863 853 844 834 825 815 806 796 787 777 29.1 768 758 749 739 730 721 711 702 692 683 29.2 673 664 655 645 636 626 617 607 598 589 29.3 579 570 560 551 542 532 523 514 504 495 29.4 485 476 467 457 448 439 429 420 410 401 29.5 392 382 373 364 354 345 336 326 318 308 29.6 298 289 280 270 261 252 242 233 224 215 29.7 205 196 187 177 168 159 149 140 131 122 29.8 112 103 94 85 75 66 57 47 38 29 29.9 20 10 +1 -8 -17 -26 -36 -45 -54 -63 30.0 -73 -82 -91 -100 -100 -119 -128 -137 -146 -156 30.1 -165 -174 -183 -192 -202 -211 -220 -229 -238 -248 30.2 -257 -266 -275 -284 -293 -303 -312 -321 -330 -339 30.3 -348 -358 -367 -376 -385 -394 -403 -412 -421 -431 30.4 -440 -449 -458 -467 -476 -485 -494 -504 -513 -522 30.5 -531 -540 -549 -558 -567 -576 -585 -594 -604 -613 30.6 -622 -631 -640 -649 -658 -667 -676 -685 -694 -703 30.7 -712 -721 -730 -740 -749 -758 -767 -776 -785 -794 30.8 -803 -812 -821 -830 -839 -848 -857 -866 -875 -884 30.9 -893 -902 -911 -920 -929 -938 -947 -956 -965 -974 31.0 -983 -992 -1001 -1010 -1019 -1028 -1037 -1046 -1055 -1064 INPUT STATION PRESSURE: READ  PRESSURE  ALTITUDE  DIRECTLY  FROM  TABLE. INPUT ALTIMETER SETTING:  READ VALUE FROM TABLE AND ADD STATION ELEVATION TO FIND  PRESSURE  ALTITUDE. 1-61

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