曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
12 14,000 49.5 NA NA NA NA NA NA NA
16 12,000 52.4 46.9 NA NA NA NA NA NA
20 10,000 58.6 52.3 46.5 NA NA NA NA NA
25 24 8,000 62.7 56.1 49.8 NA NA NA NA NA
28 6,000 66.9 60.1 53.3 48.1 NA NA NA NA
32 4,000 70.2 63.5 56.3 50.7 46.3 NA NA NA
36 2,000 73.8 67.0 59.5 53.6 48.9 NA NA NA
40 0 74.6 70.5 62.6 56.3 51.3 47.2 NA NA
15 15,000 46.3 NA NA NA NA NA NA NA
17 14,000 47.7 NA NA NA NA NA NA NA
21 12,000 50.4 45.4 NA NA NA NA NA NA
25 10,000 57.2 51.2 45.5 NA NA NA NA NA
30 29 8,000 60.9 54.7 48.6 NA NA NA NA NA
33 6,000 64.2 58.0 51.5 46.5 NA NA NA NA
37 4,000 67.4 61.2 54.4 49.1 NA NA NA NA
41 2,000 70.4 64.2 57.0 51.5 47.0 NA NA NA
45 0 73.3 67.1 59.6 53.7 49.0 45.0 NA NA
NOTES: 1. Maximum climb weights are limited by the design MAX TOGW of 74,600 lb for the GIV-SP and
73,200 for the GIV.
2. Increase MAX TOGW by 300 lb for each 10 knots of headwind up to a maximum of 40 knots.
Data not valid for tailwinds.
3. Cowl anti-ice bleeds are assumed ON for temperatures below 10° C; wing anti-ice bleeds
prohibited.
Quick Reference Handbook
NON-SP GIV PERFORMANCE REVISION 7
Page PA - 60 (NON-SP GIV AIRPLANES ONLY) May 30/02
Notes
Quick Reference Handbook
REVISION 7 NON-SP GIV PERFORMANCE
May 30/02 (NON-SP GIV AIRPLANES ONLY) Page PB - 1
Non-SP GIV Twin Engine Cruise Altitudes: Mach 0.77
CCM
GROSS WEIGHT - 1000 LB
74 70 66 62 58 54 50 46 42 38
ALT Δ ISA -20°C to 0°C +20°C
(FT) CEILING
45000 NM/LB **** **** **** **** .1721 .1857 .1982 .2101 .2218 .2326
TWIND **** **** **** **** 3 0 0 0 0 0
43000 NM/LB **** **** **** .1622 .1732 .1834 .1931 .2029 .2119 .2216
TWIND **** **** **** 0 0 6 12 16 21 22
41000 NM/LB **** .1439 .1534 .1621 .1704 .1781 .1864 .1938 .2019 .2089
TWIND **** 2 0 1 7 19 28 37 43 50
39000 NM/LB .1372 .1447 .1518 .1584 .1652 .1716 .1777 .1845 .1904 .1958
TWIND 0 0 5 11 21 36 51 61 73 83
37000 NM/LB .1365 .1421 .1478 .1532 .1584 .1634 .1691 .1740 .1784 .1821
TWIND 2 8 17 26 41 60 76 92 107 122
35000 NM/LB .1329 .1376 .1420 .1462 .1510 .1552 .1591 .1628 .1664 .1687
TWIND 14 23 36 49 65 87 109 129 148 168
33000 NM/LB .1276 .1311 .1351 .1385 .1418 .1450 .1486 .1510 .1529 ****
TWIND 34 41 61 77 99 126 150 175 202 ****
31000 NM/LB .1219 .1247 .1275 .1309 .1335 .1358 **** **** **** ****
TWIND 57 72 92 108 134 166 **** **** **** ****
29000 NM/LB .1162 .1185 .1208 .1234 .1253 **** **** **** **** ****
TWIND 82 101 123 143 174 **** **** **** **** ****
27000 NM/LB .1092 .1110 .1127 .1142 **** **** **** **** **** ****
TWIND 118 140 166 193 **** **** **** **** **** ****
25000 NM/LB .1030 .1043 **** **** **** **** **** **** **** ****
TWIND 154 179 **** **** **** **** **** **** **** ****
NOTES: 1. Values at optimum altitude are shaded.
2. Service Ceilings (100 FPM rate of climb) for selected temperature
conditions are represented on the table by bold lines.
3. Tailwind Factors (TWIND) are the difference in flight level wind
required to equal ground specific range at optimum altitude.
Quick Reference Handbook
NON-SP GIV PERFORMANCE REVISION 7
Page PB - 2 (NON-SP GIV AIRPLANES ONLY) May 30/02
Non-SP GIV Twin Engine Cruise Altitudes: Mach 0.80
CCM
GROSS WEIGHT - 1000 LB
74 70 66 62 58 54 50 46 42 38
ALT Δ ISA -20°C to 0°C +20°C
(FT) CEILING
45000 NM/LB **** **** **** **** .1694 .1816 .1919 .2023 .2126 .2212
TWIND **** **** **** **** 0 0 0 0 0 0
43000 NM/LB **** **** **** .1592 .1688 .1773 .1858 .1944 .2015 .2093
TWIND **** **** **** 0 2 11 15 19 25 26
41000 NM/LB **** .1415 .1498 .1572 .1644 .1711 .1783 .1841 .1907 .1962
TWIND **** 0 0 6 14 28 35 45 53 58
39000 NM/LB .1344 .1407 .1468 .1526 .1587 .1639 .1687 .1742 .1788 .1831
TWIND 0 3 9 20 31 50 63 74 87 95
37000 NM/LB .1321 .1370 .1422 .1467 .1509 .1549 .1595 .1633 .1668 .1697
TWIND 8 15 24 39 56 79 93 110 126 139
35000 NM/LB .1278 .1321 .1356 .1390 .1429 .1461 .1493 .1522 .1548 .1565
TWIND 24 33 48 67 85 112 132 152 172 191
33000 NM/LB .1220 .1249 .1281 .1309 .1336 .1362 .1388 **** **** ****
TWIND 47 62 79 101 125 155 178 **** **** ****
31000 NM/LB .1158 .1182 .1206 .1231 .1252 **** **** **** **** ****
TWIND 75 92 114 138 166 **** **** **** **** ****
29000 NM/LB .1097 .1116 .1134 .1154 **** **** **** **** **** ****
TWIND 107 127 152 180 **** **** **** **** **** ****
27000 NM/LB .1031 .1047 **** **** **** **** **** **** **** ****
TWIND 145 168 **** **** **** **** **** **** **** ****
25000 NM/LB .0971 **** **** **** **** **** **** **** **** ****
TWIND 185 **** **** **** **** **** **** **** **** ****
NOTES: 1. Values at optimum altitude are shaded.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:
湾流4快速检查单QRH GULFSTREAM IV QUICK REFERENCE HANDBOOK 2(42)