Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 2-200
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 2
PREFLIGHT
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
HOLDING FUEL FLOW
ALTITUDE ft
1500 5000 10,000 15,000 20,000 25,000 30,000 35,000
16,000 165
1038 1010 971 938 899 867 850 849
17,000 170
1086 1057 1017 981 940 909 891 879
18,000 175
1135 1105 1060 1023 982 951 934 922
19,000 180
1185 1154 1107 1066 1025 995 978 967
20,000 185
1236 1204 1153 1111 1068 1038 1022 1011
21,000 190
1288 1250 1197 1154 1111 1080 1065 1054
22,000 194
1339 1297 1243 1197 1156 1125 1109 1098
23,000 198
1387 1343 1287 1240 1199 1169 1150 1139
24,000 202
1433 1388 1332 1283 1242 1213 1193 1181
25,000 206
1481 1434 1378 1328 1286 1258 1236 1222
26,000 210
1527 1481 1425 1375 1333 1303 1279 1264
8XC098
ENGINE ANTICE OFF
WEIGHT lb
KIAS
TOTAL FUEL FLOW lb/hr
NOTE: Total fuel flow is increased by approximately 50 lb/hr for every 10° C above ISA and
decreased by approximately 50 lb/hr for every 10° C below ISA.