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FT 23400 –––– –––– –––– –––– –––– –––– –––– –––– –––– –––– –––– –––– –––– –––– –––– –––– –––– –––– ––––
51OM-00-01
WIND EFFECT ON DISTANCE - NM
(SUBTRACT FOR HEADWIND, ADD FOR TAILWIND)
TIME WIND
(MIN) 25KTS 50KTS 100KTS
10 4 8 16
20 8 16 33
30 12 25 50
40 16 33 66
50 20 41 83
60 25 50 100
CITATION MUSTANG OPERATING MANUAL
510OM-00 47
DESCENT
Performance for two types of descent is presented on the following pages. Time, distance and fuel
information are provided for a normal descent of 2000 feet per minute; and a high speed descent
of 3000 feet per minute for maximum speed.
This performance is based on controlling the fan speed to obtain the fuel flows, airspeed and rates
of descent presented with gear and flaps up, speed brakes retracted and anti-ice systems OFF or
ON.
The time, distance and fuel used from a given altitude are based on descending to sea level. If the
descent is to another altitude, the difference in time, distance and fuel used between the initial and
the final altitude must be determined.
Begin descent at MMO -10 KIAS, and maintain desired rate of descent when obtained. The data is
based on standard day temperature. However, temperature effects are minimal and the data can
be used for all conditions.
CITATION MUSTANG OPERATING MANUAL
48 510OM-00
NORMAL DESCENT
2000 FEET PER MINUTE RATE OF DESCENT
ANTI-ICE SYSTEMS OFF
SPEED BRAKES RETRACTED GEAR AND FLAPS UP
WEIGHT AT START OF DESCENT - LBS
PRESSURE 8000 7000 6000
ALTITUDE KIAS TIME DIST FUEL TIME DIST FUEL TIME DIST FUEL
FEET MIN NM LBS MIN NM LBS MIN NM LBS
41,000 172 20.6 108 148 20.5 108 158 20.5 108 167
39,000 181 19.5 102 144 19.5 102 153 19.5 102 163
37,000 190 18.5 96 139 18.5 96 149 18.5 96 158
35,000 200 17.5 90 134 17.5 90 143 17.5 90 153
33,000 209 16.5 84 128 16.5 84 137 16.5 84 146
31,000 220 15.5 78 122 15.5 78 130 15.5 78 139
29,000 230 14.5 73 114 14.5 73 122 14.5 73 131
27,000 240 13.5 66 105 13.5 66 113 13.5 66 121
25,000 240 12.5 61 97 12.5 61 105 12.5 61 113
23,000 240 11.5 55 89 11.5 55 96 11.5 55 104
21,000 240 10.5 49 81 10.5 49 88 10.5 49 95
19,000 240 9.5 44 74 9.5 44 80 9.5 44 86
17,000 240 8.5 39 66 8.5 39 72 8.5 39 77
15,000 240 7.5 34 58 7.5 34 63 7.5 34 68
10,000 240 5.0 22 40 5.0 22 43 5.0 22 46
5,000 240 2.5 10 20 2.5 10 22 2.5 10 24
51OM-00-01
NORMAL DESCENT
2000 FEET PER MINUTE RATE OF DESCENT
ANTI-ICE SYSTEMS ON
SPEED BRAKES RETRACTED GEAR AND FLAPS UP
WEIGHT AT START OF DESCENT - LBS
PRESSURE 8000 7000 6000
ALTITUDE KIAS TIME DIST FUEL TIME DIST FUEL TIME DIST FUEL
FEET MIN NM LBS MIN NM LBS MIN NM LBS
41,000 172 20.8 109 155 20.7 109 164 20.6 108 173
39,000 181 19.6 102 149 19.5 102 158 19.5 102 168
37,000 190 18.5 96 144 18.5 96 153 18.5 96 163
35,000 200 17.5 90 138 17.5 90 147 17.5 90 157
33,000 209 16.5 84 132 16.5 84 141 16.5 84 150
31,000 220 15.5 78 125 15.5 78 134 15.5 78 143
29,000 230 14.5 73 117 14.5 73 126 14.5 73 134
27,000 240 13.5 66 109 13.5 66 117 13.5 66 125
25,000 240 12.5 61 100 12.5 61 108 12.5 61 116
23,000 240 11.5 55 92 11.5 55 99 11.5 55 107
21,000 240 10.5 49 84 10.5 49 91 10.5 49 98
19,000 240 9.5 44 76 9.5 44 82 9.5 44 89
17,000 240 8.5 39 68 8.5 39 74 8.5 39 80
15,000 240 7.5 34 60 7.5 34 65 7.5 34 71
10,000 240 5.0 22 41 5.0 22 44 5.0 22 48
5,000 240 2.5 10 21 2.5 10 22 2.5 10 24
51OM-00-01
WIND EFFECT ON DESCENT DISTANCE - NM
(SUBTRACT FOR HEADWIND, ADD FOR TAILWIND)
TIME WIND
(MIN) 25KTS 50KTS 100KTS
5 2 4 8
10 4 8 16
15 6 12 25
20 8 16 33
25 10 20 41
30 12 25 50
CITATION MUSTANG OPERATING MANUAL
510OM-00 49
HIGH-SPEED DESCENT
3000 FEET PER MINUTE RATE OF DESCENT
ANTI-ICE SYSTEMS OFF
SPEED BRAKES RETRACTED GEAR AND FLAPS UP
WEIGHT AT START OF DESCENT - LBS
PRESSURE 8000 7000 6000
ALTITUDE KIAS TIME DIST FUEL TIME DIST FUEL TIME DIST FUEL
FEET MIN NM LBS MIN NM LBS MIN NM LBS
41,000 172 14.8 78 68 14.6 77 77 14.3 75 88
39,000 181 13.8 72 64 13.5 71 73 13.3 70 83
37,000 190 12.7 66 60 12.6 65 69 12.4 64 80
35,000 200 11.8 61 55 11.7 60 65 11.7 60 76
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Cessna塞斯纳公务机飞行手册(178)
