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6133 5722 5354 5036 4756 4500 4296 4107 3933 3773 3628
6850 6377 5955 5599 5287 5000 4773 4563 4367 4188 4024
AIR
DIST
(NM)
PRESSURE ALTITUDE (1000 FT)
29 31 33 35 37
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
500 2.5 1:15 2.4 1:14 2.3 1:14 2.3 1:15 2.2 1:17
1000 4.9 2:31 4.7 2:28 4.6 2:26 4.4 2:26 4.3 2:27
1500 7.3 3:48 7.0 3:43 6.8 3:39 6.6 3:37 6.4 3:37
2000 9.6 5:05 9.3 4:58 9.0 4:52 8.7 4:49 8.4 4:48
2500 11.9 6:24 11.5 6:15 11.1 6:07 10.7 6:02 10.5 5:59
3000 14.1 7:45 13.6 7:33 13.2 7:23 12.8 7:16 12.4 7:11
3500 16.3 9:09 15.7 8:54 15.2 8:41 14.7 8:31 14.3 8:24
4000 18.4 10:35 17.7 10:17 17.1 10:01 16.6 9:49 16.1 9:39
REFERENCE FUEL REQUIRED
(1000 KG)
WEIGHT AT CHECK POINT (1000 KG)
30 40 45 50 60
5 -0.7 -0.3 0.0 0.4 1.6
6 -0.9 -0.3 0.0 0.4 1.8
7 -1.1 -0.4 0.0 0.5 2.0
8 -1.2 -0.4 0.0 0.6 2.3
9 -1.4 -0.5 0.0 0.6 2.5
10 -1.5 -0.5 0.0 0.7 2.7
11 -1.7 -0.6 0.0 0.8 2.9
12 -1.8 -0.6 0.0 0.8 3.1
13 -2.0 -0.7 0.0 0.9 3.3
14 -2.1 -0.7 0.0 1.0 3.5
15 -2.2 -0.8 0.0 1.0 3.7
16 -2.4 -0.9 0.0 1.1 3.9
17 -2.5 -0.9 0.0 1.2 4.0
18 -2.6 -1.0 0.0 1.2 4.2
19 -2.7 -1.0 0.0 1.3 4.3
June 7, 2002
737 Flight Crew Operations Manual
Performance Inflight -
All Engines
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.11.5
All Engines Long Range Cruise Wind-Altitude Trade
Descent
Based on .74/250 descent speed
PRESSURE
ALTITUDE
(1000 FT)
CRUISE WEIGHT (1000 KG)
62 60 58 56 54 52 50 48 46 44 42 40 38 36
37 14 8 1 0 0 0 0 0 0 0
35 9 5 2 0 0 2 6 8 10 12 13 14 14
33 2 1 0 1 3 7 12 17 20 23 26 27 29 30
31 1 3 4 9 14 19 25 31 35 38 41 43 44 45
29 8 12 17 22 28 33 39 45 50 54 57 59 60 61
27 17 25 30 35 41 48 55 61 66 69 71 74 75 77
25 34 39 44 51 57 63 70 78 82 86 89 92 94 96
23 48 53 59 65 72 79 86 94 99 103 106 109 112 113
The above wind factor tables are for calculation of wind required to maintain present range capability at new
pressure altitude, i.e., break-even wind.
Method:
1. Read wind factors for present and new altitudes from table.
2. Determine difference (new altitude wind factor minus present altitude wind factor); This difference may
be negative or positive.
3. Break-even wind at new altitude is present altitude wind plus difference from step 2.
PRESSURE ALT (1000 FT) 25 27 29 31 33 35 37
DISTANCE (NM) 79 86 92 98 105 111 116
TIME (MINUTES) 18 19 20 21 22 23 23
June 7, 2002
737 Flight Crew Operations Manual
Performance Inflight -
All Engines
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.11.6
All Engines Holding
Flaps Up
WEIGHT
(1000 KG)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000 20000 25000 30000 35000 37000
62
%N1 61.7 64.3 68.3 72.4 76.3 80.4 84.5 90.6
KIAS 247 248 250 253 255 257 256 249
FF/ENG 1430 1400 1360 1330 1310 1310 1310 1400
60
%N1 60.9 63.5 67.4 71.6 75.5 79.6 83.6 88.9
KIAS 243 244 246 248 251 253 252 246
FF/ENG 1390 1360 1320 1290 1270 1270 1270 1320
58
%N1 60.1 62.6 66.5 70.7 74.7 78.7 82.8 87.6
KIAS 239 240 241 244 246 248 248 243
FF/ENG 1360 1320 1280 1250 1230 1230 1220 1250
56
%N1 59.3 61.7 65.6 69.7 73.9 77.9 81.9 86.5 90.0
KIAS 235 235 237 239 242 244 245 241 237
FF/ENG 1320 1280 1240 1210 1190 1190 1180 1200 1260
54
%N1 58.4 60.8 64.7 68.7 73.0 77.0 81.0 85.4 88.2
KIAS 231 231 232 235 237 239 241 238 234
FF/ENG 1280 1240 1200 1170 1150 1150 1140 1150 1180
52
%N1 57.5 60.0 63.8 67.8 72.0 76.0 80.1 84.4 86.9
KIAS 228 227 228 230 232 235 236 234 231
FF/ENG 1240 1210 1160 1130 1110 1100 1090 1100 1120
50
%N1 56.6 59.1 62.7 66.8 71.0 75.0 79.1 83.3 85.6
KIAS 224 223 223 225 227 230 232 230 228
FF/ENG 1210 1170 1130 1090 1070 1060 1050 1060 1070
48
%N1 55.7 58.1 61.7 65.7 70.0 74.0 78.1 82.3 84.5
KIAS 220 219 219 220 223 225 227 226 225
FF/ENG 1170 1130 1090 1050 1030 1020 1010 1010 1020
46
%N1 54.8 57.1 60.6 64.6 68.8 73.0 77.1 81.2 83.4
KIAS 216 214 214 215 218 220 222 222 221
FF/ENG 1130 1100 1050 1020 990 980 970 970 980
44
%N1 53.9 56.1 59.6 63.5 67.6 72.0 76.0 80.1 82.2
KIAS 211 210 210 210 212 215 217 218 217
FF/ENG 1100 1060 1020 980 950 940 930 930 930
42
%N1 53.1 55.3 58.8 62.6 66.6 70.8 74.9 79.0 81.1
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