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June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight -
General
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.20.10
ADVISORY INFORMATION
Slippery Runway Takeoff
No Reverse Thrust
V1 Adjustment (KIAS)
WEIGHT
(1000 KG)
REPORTED BRAKING ACTION
GOOD MEDIUM POOR
PRESS ALT (FT) PRESS ALT (FT) PRESS ALT (FT)
S.L. 4000 8000 S.L. 4000 8000 S.L. 4000 8000
64 -8 -6 -4 -21 -19 -17 -41 -39 -37
60 -9 -7 -5 -23 -21 -19 -44 -42 -40
56 -11 -9 -7 -26 -24 -22 -47 -45 -43
52 -13 -11 -9 -29 -27 -25 -50 -48 -46
48 -15 -13 -11 -31 -29 -27 -53 -51 -49
44 -16 -14 -12 -33 -31 -29 -55 -53 -51
40 -17 -15 -13 -35 -33 -31 -56 -54 -52
36 -18 -16 -14 -36 -34 -32 -56 -54 -52
1. Obtain V1, VR and V2 for the actual weight.
2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment Table with the
actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG).
June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight -
General
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
 PI.20.11
Takeoff %N1
Based on engine bleed to packs on (Auto) and anti-ice on or off
%N1 Adjustments for Engine Bleeds
AIRPORT
OAT AIRPORT PRESSURE ALTITUDE (FT)
°C °F -1000 0 1000 2000 3000 4000 5000 6000 7000 8000
55 131 93.2 93.8 93.8 93.8
50 122 93.8 94.3 94.3 94.3 93.9 93.6
45 113 94.2 94.7 94.7 94.6 94.6 94.6 94.7 94.4 94.2
40 104 94.6 95.2 95.2 95.1 95.0 95.1 95.1 95.2 95.1 94.9
35 95 95.2 95.6 95.6 95.6 95.5 95.7 95.7 95.7 95.6 95.5
30 86 95.2 96.1 96.1 96.0 96.0 96.3 96.2 96.1 96.0 96.0
25 77 94.4 95.3 95.8 96.2 96.5 96.7 96.6 96.6 96.5 96.4
20 68 93.6 94.5 95.0 95.4 95.9 96.6 97.1 97.1 97.0 96.9
15 59 92.8 93.7 94.2 94.6 95.1 95.8 96.3 96.8 97.2 97.5
10 50 92.0 92.9 93.4 93.8 94.2 95.0 95.4 95.9 96.4 96.8
5 41 91.2 92.1 92.5 92.9 93.4 94.1 94.6 95.1 95.5 96.0
0 32 90.3 91.2 91.7 92.1 92.6 93.3 93.7 94.2 94.7 95.1
-10 14 88.7 89.6 90.0 90.4 90.8 91.5 92.0 92.5 92.9 93.4
-20 -4 87.0 87.8 88.3 88.7 89.1 89.8 90.2 90.7 91.1 91.6
-30 -22 85.2 86.0 86.5 86.9 87.3 88.0 88.4 88.9 89.3 89.7
-40 -40 83.5 84.3 84.7 85.1 85.5 86.2 86.6 87.1 87.4 87.9
-50 -58 81.7 82.5 82.9 83.2 83.7 84.3 84.7 85.2 85.6 86.0
BLEED
CONFIGURATION
AIRPORT PRESSURE ALTITUDE (FT)
-2000 9000
ENGINE BLEED
TO PACKS OFF 1.0 1.0
June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight -
General
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.20.12
Assumed Temperature Reduced Thrust
Maximum Assumed Temperature (Table 1)
Based on 25% Takeoff Thrust Reduction
%N1 Adjustment For Temperature Difference (Table 3)
OAT
(°C)
PRESS ALT (1000 FT) OAT
(°F)
PRESS ALT (1000 FT)
-1 0 1 2 3 4 5 6 7 8 -1 0 1 2 3 4 5 6 7 8
55 74 71 71 130 165 159 159
50 71 69 68 68 69 70 120 160 155 154 154 155 157
45 69 67 66 66 67 67 67 68 70 110 155 151 149 149 150 151 151 152 155
40 67 65 64 64 64 64 64 64 66 68 100 151 148 145 145 145 145 147 145 149 151
35 65 63 62 62 62 61 61 62 63 64 90 146 143 141 141 140 140 140 140 143 144
30 63 61 60 60 59 59 59 59 60 61 80 146 142 139 138 136 135 135 135 137 138
25 63 61 59 58 57 56 56 56 57 58 70 146 142 138 136 135 131 129 129 130 132
20 63 61 59 58 57 55 53 54 54 55 60 146 142 138 136 135 131 127 127 126 126
15 &
BELOW 63 61 59 58 57 55 53 53 52 52 50 &
BELOW 146 142 138 136 135 131 127 127 126 126
ASSUMED TEMP
MINUS OAT OUTSIDE AIR TEMPERATURE
°C °F °C -40 -20 0 5 10 15 20 25 30 35 40 45 50 55
°F -40 -4 32 41 50 59 68 77 86 95 104 113 122 131
10 18 1.6 1.6 1.6 1.5 1.5 1.5 1.5 1.4 1.4
20 36 3.3 3.2 3.2 3.1 3.0 3.0 2.9 2.8 2.8 2.7 2.5 2.3
30 54 4.8 4.8 4.6 4.5 4.4 4.3 4.0 3.8 3.6 3.6 3.6 3.6
40 72 6.0 6.2 6.1 6.0 5.8 5.7 5.2 5.0 5.0
50 90 8.2 7.5 7.3 7.2 6.6 6.5
60 108 10.4 9.5 8.7 8.1 7.9
70 126 11.8 10.7 9.3
80 144 13.0 11.8 10.1
90 162 14.0 12.4
100 180 15.0 12.8
110 198 15.4
1. Determine Maximum Assumed Temperature allowed from Table 1.
2. Find Maximum %N1 from Table 2 using the desired assumed temperature (no greater than temperature
from Table 1).
3. Use the difference between assumed temperature and OAT to determine the %N1 adjustment from
Table 3.
4. Subtract %N1 adjustment from Maximum %N1 in Table 2.
June 3, 2005
737 Flight Crew Operations Manual
Performance Inflight -
　
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