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者

;vref for flaps 40
vref=40
77200 109
82700 113
88200 116
93700 120
99200 124
104700 127
110200 130
115800 134
121300 137
126800 140
132300 143
137800 146
143300 149
148800 152
154300 155
vrefend
The stick shaker speeds can be set as well... using the same system as the other speeds.
;stick shaker speeds for flaps up
vss=0
90000 137
100000 144
Project Magenta Revision: 26-May-07
109
110000 152
120000 157
130000 165
132500 167
vssend
vss=1
vss30 1.12
vssend
N1 Takeoff Table
The following is a table for the takeoff thrust N1% limit. The table goes from the highest to the lowest
temperature in the first column, then the various N1 settings are listed in columns according to the airport's
pressure altitude (OAT).
n1totable
C -2000 0 1000 2000 3000 4000 5000 6000 7000 8000 9000
60 84.0 84.7 86.1 87.3 88.1 89.1 89.3 89.5 88.8 88.2 87.9
55 84.8 85.8 87.0 88.1 89.0 90.0 90.1 90.3 89.6 88.8 88.1
50 85.8 86.8 87.9 88.9 89.8 90.8 90.9 91.0 90.3 89.6 88.7
45 86.8 87.7 88.8 89.7 90.7 91.7 91.7 91.7 91.1 90.4 89.5
40 87.7 88.6 89.7 90.6 91.6 92.5 92.4 92.4 91.8 91.2 90.3
35 88.4 89.5 90.6 91.5 92.4 93.4 93.3 93.2 92.6 91.9 91.0
30 88.2 90.1 91.1 92.1 93.0 94.0 94.0 94.0 93.4 92.7 91.8
25 87.5 89.7 90.7 91.8 92.7 93.7 94.2 94.3 94.1 93.5 92.6
20 86.8 89.0 90.0 91.1 91.9 93.0 93.4 93.9 94.5 94.2 93.4
15 86.0 88.3 89.3 90.3 91.2 92.2 92.6 93.1 93.7 94.2 94.0
10 85.3 87.5 88.5 89.6 90.4 91.4 91.9 92.3 92.9 93.4 93.7
5 84.6 86.8 87.7 88.8 89.6 90.7 91.1 91.6 92.1 92.6 92.9
0 83.8 86.0 87.0 88.0 88.9 89.9 90.3 90.8 91.3 91.8 92.1
-5 83.1 85.2 86.2 87.2 88.1 89.1 89.5 90.0 90.5 91.0 91.3
-10 82.3 84.5 85.4 86.4 87.3 88.3 88.7 89.2 89.7 90.2 90.5
-15 81.6 83.7 84.6 85.6 86.5 87.5 87.9 88.3 88.9 89.3 89.7
-20 80.8 82.9 83.8 84.8 85.7 86.7 87.0 87.5 88.1 88.5 88.8
-25 80.0 82.1 83.0 84.0 84.8 85.8 86.2 86.7 87.2 87.7 88.0
-30 79.2 81.3 82.2 83.2 84.0 85.0 85.4 85.8 86.4 86.8 87.2
-35 78.4 80.5 81.4 82.4 83.2 84.1 84.5 85.0 85.6 86.0 86.3
-40 77.6 79.6 80.5 81.5 82.3 83.3 83.7 84.1 84.7 85.1 85.4
-45 76.8 78.8 79.7 80.7 81.5 82.4 82.8 83.3 83.8 84.2 84.5
-50 76.0 78.0 78.9 79.8 80.6 81.5 81.9 82.4 82.9 83.3 83.7
-55 75.2 77.1 78.0 79.0 79.8 80.7 81.1 81.5 82.1 82.5 82.8
end
N1 Climb Table
Similarly, a table for N1 Climb values, again, it has to be from the highest to the lowest temperature:
n1clbtable
C 0 5000 10000 15000 20000 25000 30000 35000 37000 41000
60 83.7 83.8 83.7 83.7 86.9 91.3 92.9 94.3 94.4 92.7
55 84.7 84.6 84.6 87.3 90.6 92.3 93.6 93.7 92.0 84.5
50 85.2 85.5 85.5 85.5 88.2 90.7 91.6 92.9 93.0 91.3
45 86.0 86.3 86.3 86.3 89.1 91.6 91.6 92.2 92.3 90.6
Project Magenta Revision: 26-May-07
110
40 86.9 87.0 87.1 87.1 89.9 92.4 92.4 91.5 91.6 89.9
35 87.8 87.9 87.9 90.7 93.2 93.2 92.3 91.6 90.0 87.5
30 86.8 88.5 88.6 88.7 91.5 94.0 93.9 93.1 92.5 91.0
25 86.1 88.6 89.4 89.4 92.3 94.8 94.6 93.9 93.3 92.0
20 85.4 87.9 90.2 90.1 93.0 95.5 95.3 94.6 94.1 92.9
15 84.7 87.1 89.6 90.9 93.8 96.2 96.0 95.4 94.9 93.9
10 84.0 86.4 88.8 91.1 94.6 96.9 96.6 96.1 95.7 94.8
5 83.2 85.7 88.1 90.3 95.5 97.8 97.3 96.9 96.5 95.7
0 82.5 84.9 87.3 89.5 94.8 98.9 98.3 97.8 97.4 96.6
-5 81.8 84.1 86.5 88.7 94.0 98.8 99.3 98.5 98.2 97.7
-10 81.0 83.4 85.7 87.9 93.2 98.0 99.6 99.4 99.1 98.6
-15 80.3 82.6 85.0 87.1 92.4 97.3 98.8 100.4 100.1 99.6
-20 79.5 81.8 84.2 86.3 91.5 96.5 98.0 100.1 100.6 100.2
-25 78.7 81.0 83.3 85.5 90.7 95.7 97.2 99.2 99.8 99.4
-30 78.0 80.2 82.5 84.7 89.9 94.9 96.4 98.4 98.9 98.6
-35 77.2 79.4 81.7 83.8 89.0 94.0 95.5 97.6 98.1 97.7
-40 76.4 78.6 80.9 83.0 88.2 93.2 94.7 96.7 97.2 96.9
end
Climb 1 and 2 thrust reduction sequence E.g.: reducing by 3% N1 until 10000 ft, gradually increasing to full
climb N1 until 15000 ft:
clb1-reduction
3, 10000, 15000
clb2-reduction
6, 5000, 15000
For Take-Off thrust reduction use the following:
to1-reduction
10, 10000, 15000
to2-reduction
15, 10000, 15000
Note: The reduction entries should be made after the tables.
Cost Index Data (Experimental)
costindex
0 271/.72 270/.71 330/.78 3.2
20 283/.74 282/.74 266/.73 2.7
200 335/.78 320/.78 330/.78 2.1
end
Example: 20 is cost index clbias/clbmach crzias/crzmach desias/desmach (descent angle in degrees)
(Note: Descent, IAS first, then MACH, normally it is spoken/written as mach/ias, (high cost index should
have a higher descent angle for path descent)
Project Magenta Revision: 26-May-07
　
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