曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
73.4
247
0.597
2052
359
72.3
241
0.583
1966
351
71.1
235
0.569
1878
343
Max TAT not shown where N1 can be set in ISA + 30°C conditions.
Increase/decrease avg. N1 required by 1% per 5°C above/below STD TAT.
Increase/decrease fuel flow 1% per 5°C above/below STD TAT.
Increase/decrease TAS by 1 Kt. per 1°C above/below STD TAT.
Interpolate if necessary.
(Continued)
737 Sec. 5 Page 61
Flight Manual Continental Rev. 11/15/02 #41
B Turbulent Air Penetration
TARGET PRESS GROSS WEIGHT 1000 LB
SPEED ALT 160 150 140 130 120 110 100 90
IASMACH 1000 FT APPROXIMATE POWER SETTING
IN %N1 RPM
41 93.1 89.2 86.7 85.1 83.7
40 90.3 87.6 85.7 84.3 83.0
35 89.0 87.1 85.7 84.5 83.5 82.5 81.6 81.0
280/.76 30 84.9 84.1 83.2 82.5 81.8 81.2 80.7 80.3
25 81.2 80.3 79.5 78.8 78.1 77.6 77.1 76.7
20 77.2 76.4 75.7 75.0 74.4 73.9 73.5 73.1
15 73.4 72.6 72.0 71.3 70.7 70.2 69.7 69.2
10 69.5 68.8 68.2 67.6 67.1 66.7 66.3 65.9
B Max Cruise Percent N1
MAX CRUISE PERCENT N1
PRESS
ALT TAT DEG C
1000
FT -60 -55 -50 -45 -40 -35 -30 -25 -20 -15 -10 -5 0 5
41
39
37
87.4
87.6
87.8
88.3
88.5
88.7
89.3
89.5
89.7
90.2
90.4
90.6
91.1
91.3
91.5
92.0
92.2
92.4
92.9
93.1
93.3
93.7
94.0
94.2
94.6
94.7
94.4
94.3
94.1
93.8
93.4
93.4
93.1
92.7
92.7
92.4
91.9
92.0
91.6
91.1
91.3
90.8
35
33
31
87.2
86.0
85.4
88.2
87.0
86.3
89.1
88.0
87.3
90.1
88.9
88.2
91.0
89.9
89.2
91.9
90.8
90.1
92.8
91.7
91.0
93.6
92.6
91.9
94.5
93.6
92.8
94.2
94.5
93.7
93.4
94.2
94.6
92.7
93.4
94.0
91.8
92.5
93.1
91.0
91.6
92.2
MAX CRUISE PERCENT N1
PRESS
ALT TAT DEG C
1000
FT -50 -45 -40 -35 -30 -25 -20 -15 -10 -5 0 5 10 15
29
27
25
86.2
85.5
85.0
87.2
86.5
85.9
88.1
87.4
86.8
89.0
88.3
87.7
90.0
89.2
88.6
90.9
90.1
89.5
91.8
91.0
90.4
92.6
91.9
91.3
93.5
92.8
92.2
94.3
93.6
93.0
93.6
93.8
93.9
92.8
93.0
93.2
92.0
92.2
92.5
91.1
91.3
91.6
Sec. 5 Page 62 737
Rev. 11/15/02 #41 Continental Flight Manual
C Two Engine Long Range Cruise
LONG RANGE CRUISE
ALL ENGINES A/C AUTO
MAX CRUISE THRUST
LIMITS
ISA Average %N1 Required
Max TAT for Thrust Rating
IAS Knots
Mach Number
ISA Fuel Flow LB/HR/ENG
ISA TAS Kts.
PRESSURE ALTITUDE 41000 FT TO 25000 FT
Press
Alt
1000
GROSS WEIGHT (1,000 POUNDS)
Feet
(Std
TAT)
175 170 165 160 155 150 145 140 135 130 125 120 115 110
41
(-29)
91.6
-13
235
0.795
2458
456
90.2
-9
235
0.794
2344
455
88.9
-6
234
0.791
2239
454
87.8
-3
232
0.786
2142
451
39
(-30)
92.1
-13
246
0.795
2725
456
90.6
-10
246
0.795
2606
456
89.4
-6
246
0.793
2498
455
88.3
-3
244
0.789
2397
453
87.4
0
243
0.785
2304
450
86.5
2
241
0.78
2216
447
85.7
239
0.774
2139
444
37
(-30)
92
-13
258
0.794
2982
456
90.6
-9
258
0.795
2858
456
89.5
-6
258
0.794
2750
455
88.5
-3
256
0.791
2648
454
87.6
0
255
0.787
2553
452
86.8
2
254
0.783
2463
449
86
252
0.778
2380
446
85.3
250
0.773
2304
443
84.6
248
0.766
2225
439
83.7
244
0.756
2137
434
35
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737 FLIGHT MANUAL 737飞行手册2(126)
