曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

299
.743
3094
444
83.5
297
.739
3004
441
82.8
295
.734
2912
438
82.1
292
.727
2817
434
81.3
288
.718
2722
429
80.5
284
.709
2622
423
79.6
279
.697
2517
416
78.6
274
.685
2413
409
77.6
269
.673
2311
402
76.5
263
.660
2210
394
75.4
257
.646
2109
386
74.1
251
.631
2007
377
72.8
244
.615
1906
367
71.3
237
.598
1804
357
25
(-13)
83.8
309
.738
3252
444
83.2
307
.732
3158
441
82.5
304
.725
3062
437
81.8
300
.717
2965
432
81.1
296
.708
2864
426
80.2
292
.698
2759
420
79.3
287
.687
2655
414
78.4
282
.676
2553
407
77.4
277
.664
2451
400
76.4
271
.652
2350
392
75.2
265
.638
2248
384
74.0
259
.624
2146
376
72.7
252
.609
2045
367
71.4
246
.594
1944
357
69.9
238
.577
1842
347
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.
737 Sec. 5 Page 59
Flight Manual Continental Rev. 11/15/02 #41
@ Turbulent Air Penetration
TARGET PRESS GROSS WEIGHT 1000 LB
SPEED ALT 70 80 90 100 110 120 130 N1 BLEED ADJUSTMENTS
IAS/MACH 1000 FT
APPROXIMATE POWER SETTING
IN %N1 RPM
BLEED
CONFIGURATION
N1
ADJUSTMENT
%
37 78 79 81 83 85 88 A/C OFF +0.8
35 77 78 80 81 83 85 88 A/C HIGH -0.6
30 77 78 79 80 81 82 83 ENG TAI -1.0
280/.73 25 75 76 77 78 79 80 81 WING TAI
20 72 72 73 74 75 76 77 NORMAL -2.0
15 68 69 69 70 71 72 73 HIGH -2.0
10 64 65 66 67 67 68 69
@ 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
37
36
35
85.9
85.9
84.5
87.0
86.5
85.5
87.9
87.5
86.5
88.9
88.4
87.4
89.9
89.4
88.4
90.8
90.3
89.3
91.7
91.2
90.2
92.6
92.2
91.1
93.0
93.1
92.0
92.7
92.8
92.8
92.4
92.6
92.6
92.2
92.2
92.2
91.9
91.9
92.0
91.8
91.6
91.7
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
31
29
27
85.6
84.6
83.8
86.5
85.6
84.7
87.5
86.5
85.6
88.4
87.4
86.5
89.3
88.4
87.4
90.2
89.3
88.3
91.1
90.1
89.2
91.9
91.0
90.1
92.5
91.8
90.9
92.2
92.0
91.7
91.8
91.7
91.6
91.5
91.4
91.3
91.3
91.1
91.0
91.0
90.8
90.7
MAX CRUISE PERCENT N1
PRESS
ALT TAT DEG C
1000
FT -40 -35 -30 -25 -20 -15 -10 -5 0 5 10 15 20 25
25 84.9 85.8 86.7 87.5 88.4 89.3 90.1 90.9 91.5 91.2 90.9 90.6 90.2 89.8
Sec. 5 Page 60 737
Rev. 11/15/02 #41 Continental Flight Manual
B 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)
160 155 150 145 140 135 130 125 120 115 110 105 100 95
41
(-30)
93.7
-18
233
0.789
2593
452
91.6
-13
234
0.79
2439
453
90
-9
233
0.79
2312
453
88.6
-5
232
0.786
2195
451
87.4
-2
　
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