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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. 2000 11 72 675 3 0.6 3 3000 9 72 630 4 0.9 5 4000 7 71 580 6 1.2 8 5000 5 71 535 8 1.6 10 6000 3 70 485 10 1.9 12 7000 1 69 440 12 2.3 15 8000 -1 69 390 15 2.7 19 9000 -3 68 345 17 3.2 22 10,000 -5 68 295 21 3.7 27 11,000 -7 67 250 24 4.2 32 12,000 -9 67 200 29 4.9 38 Figure 5-6. Time, Fuel, and Distance to Climb CRUISE PERFORMANCE CONDITIONS: 2300 Pounds Recommended Lean Mixture PRESSURE ALTITUDE FT RPM 20°C STANDARD BELOW TEMP STANDARD TEMPERATURE 20°C ABOVE STANDARD TEMP BHP BHP KTAS GPH % BHP KTAS GPH % BHP KTAS GPH 2000 2500 - - - - - - - - - 75 116 8.4 71 115 7.9 2400 72 111 8.0 67 111 7.5 63 110 7.1 2300 64 106 7.1 60 105 6.7 56 105 6.3 2200 56 101 6.3 53 100 6.1 50 99 5.8 2100. 5D 95 5.8 47 94 5.6 45 93 5.4 4000 2550 - - - - - - - - - 75 118 8.4 71 118 7.9 2500 76 116 8.5 71 115 8.0 67 115 7.5 2400 68 111 7.6 64 110 7.1 60 109 6.7 2300 60 105 6.8 57 105 6.4 54 104 6.1 中国通航网 www.ga.cn 通航翻译 www.aviation.cn 本文链接地址：塞斯纳172飞行员操作手册 Cessna 172 PILOT'S OPERATING HANDBOOK(49) |
