曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

Altimeter Position Correction - Feet, Pilot/Copilot Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-22
Altimeter Position Correction - Feet, Standby System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-23
Stall Speeds - KCAS (Stall Warning-NORMAL) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-24
Stall Speeds - KCAS (Stall Warning-HIGH). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-25
Takeoff Thrust . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-26
Maximum Continuous Thrust . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-29
Buffet Onset / Airspeed - KIAS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-34
Crosswind Component . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-35/4-36
510FM-05 AA 4-15/4-16

MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
ISA TEMPERATURE DEVIATION CORRECTION
NO CORRECTION REQUIRED
Figure 4-2*
Figure 4-3
510FM-06 AH 4-17
SECTION IV - PERFORMANCE MODEL 510
STANDARD CHARTS
FAA APPROVED
U.S. Configuration
TEMPERATURE CONVERSION
CELSIUS TO FAHRENHEIT
Figure 4-4
PRESSURE CONVERSION
INCHES OF MERCURY TO MILLIBARS
Figure 4-5
°C °F °C °F °C °F °C °F °C °F
-54
-53
-52
-65
-63
-62
-32
-31
-30
-26
-24
-22
-10
-9
-8
14
16
18
12
13
14
54
55
57
34
35
36
93
95
97
-51
-50
-49
-60
-58
-56
-29
-28
-27
-20
-18
-17
-7
-6
-5
19
21
23
15
16
17
59
61
63
37
38
39
99
100
102
-48
-47
-46
-54
-53
-51
-26
-25
-24
-15
-13
-11
-4
-3
-2
25
27
28
18
19
20
64
66
68
40
41
42
104
106
108
-45
-44
-43
-49
-47
-45
-23
-22
-21
-9
-8
-6
-1
01
30
32
34
21
22
23
70
72
73
43
44
45
109
111
113
-42
-41
-40
-44
-42
-40
-20
-19
-18
-4
-2
0
234
36
37
39
24
25
26
75
77
79
46
47
48
115
117
118
-39
-38
-37
-38
-36
-35
-17
-16
-15
135
567
41
43
45
27
28
29
81
82
84
49
50
51
120
122
124
-36
-35
-34
-33
-31
-29
-14
-13
-12
79
10
89
10
46
48
50
30
31
32
86
88
90
52
53
54
126
127
129
-33 -27 -11 12 12 52 33 91
INCHES OF MERCURY 28.0 28.1 28.2 28.3 28.4 28.5 28.6 28.7 28.8 28.9 29.0
MILLIBARS 948 951 955 958 962 965 968 972 975 979 982
INCHES OF MERCURY 29.1 29.2 29.3 29.4 29.5 29.6 29.7 29.8 29.9 30.0
MILLIBARS 985 989 992 995 999 1002 1006 1009 1012 1016
INCHES OF MERCURY 30.1 30.2 30.3 30.4 30.5 30.6 30.7 30.8 30.9 31.0
MILLIBARS 1019 1023 1026 1029 1033 1036 1040 1043 1046 1050
4-18 AA 510FM-00
MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
ISA TEMPERATURE DEVIATION CORRECTION
Figure 4-2
Figure 4-3
INDICATED AIRSPEED 80 100 120 140 160 180 200 220 240 250
TEMPERATURE
CORRECTION -4 -3 -3 -3 -2 -3 -3 -4 -4 -5
510FM-06 AI 4-17.1
SECTION IV - PERFORMANCE MODEL 510
STANDARD CHARTS
FAA APPROVED
U.S. Configuration
TEMPERATURE CONVERSION
CELSIUS TO FAHRENHEIT
Figure 4-4
PRESSURE CONVERSION
INCHES OF MERCURY TO MILLIBARS
Figure 4-5
°C °F °C °F °C °F °C °F °C °F
-54
-53
-52
-65
-63
-62
-32
-31
-30
-26
　
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本文鏈接地址：Citation Mustang airplane flight manual 1(127)