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for runway 26 with 112,000 lbs. --- 46°C. (SEL TEMP entry)
4. Determine V Speeds from the appropriate V Speed page (this section of the
Flight Manual or the QRH). Enter the COLUMN REFERENCE chart with
actual temperature (or assumed temperature if used). Reference the A, B,
C, D, or E column to the appropriate flap setting chart and actual aircraft
gross weight to find the V Speeds.
In this case, using the gray > section in the QRH, enter the COLUMN
REFERENCE with 46°C --- Column B.
Proceeding down Column B for Flaps 5, interpolate to find V Speeds for
the actual weight of 108,000 lbs. --- 130, 131, 137.
5. Adjustments to weight limitations and/or V1 must be made if slope and/or
wind are a factor. Head wind corrections are not applied unless deemed
necessary by the Captain. Tail wind is always applied. Slope can be found
at the bottom of the Runway Analysis.
Sec. 5 Page 12 737
Rev. 11/15/02 #41 Continental Flight Manual
Bleed Configuration
Data presented in the Runway Analysis section of the flight papers is BLEEDS
OFF. Aircrews should attempt to use BLEEDS ON when possible.
ACCULOAD will calculate BLEEDS ON weight limits based on actual
departure runway and conditions. In the absence of ACCULOAD, crews can
determine legality for BLEEDS ON takeoff, by adding the following “worst
case” corrections to actual gross weight:
>>@ + 4,000 lbs.
B + 4,000 lbs.
C + 5,100 lbs.
D + 5,000 lbs.
This adjusted weight must be less than both the runway and climb limits for the
takeoff runway. This adjusted weight is also used in determining BLEEDS ON
Assumed Temperature. The above corrections are not runway specific and
represent the most conservative conditions. ACCULOAD calculates BLEEDS
ON corrections for a specific runway and conditions, which may provide a
lesser weight reduction. Use ACCULOAD data if available.
737 Sec. 5 Page 13
Flight Manual Continental Rev. 11/15/02 #41
>> Takeoff V Speeds
40 60 80 100 120 140 160
0
3
6
9
10 20 30 40 50 60 70
A
C
COLUMN REFERENCE
TEMPERATURE °C
TEMPERATURE °F
4 &
BELOW
& BELOW
P
R
ES
S
AL
T
10
00
FT
3737513
B
D
PMC ON
SLOPE/WIND V1 ADJUSTMENT*
WEIGHT
1000 SLOPE % WIND KTS
LB -2 0 2 -15 0 40
140 -2 0 3 -2 0 1
120 -2 0 1 -3 0 1
100 -2 0 0 -3 0 0
80 -2 0 1 -3 0 0
*V1 NOT TO EXCEED Vr
FLAPS
WT
1000
A B C D
LB V1 Vr V2 V1 Vr V2 V1 Vr V2 V1 Vr V2
140 158 160 165 159 162 165
F 130 151 153 158 152 154 158 154 156 158
L 120 143 145 152 144 147 151 146 148 151
A 110 136 137 145 137 139 144 139 140 144
P 100 128 128 138 129 130 137 131 132 137 133 134 137
S 90 119 120 131 121 122 131 122 123 130 125 125 130
1
80 111 111 124 112 113 124 114 114 123 116 116 122
75 107 107 121 108 109 120 110 110 120 112 112 119
140 151 153 157 152 154 157
F 130 144 146 151 145 147 151 146 149 152
L 120 137 138 145 138 140 144 139 142 146
A 110 130 131 139 131 132 138 132 134 139 135 136 139
P 100 122 123 133 123 125 132 125 126 132 127 128 132
S 90 114 115 126 116 117 126 117 118 125 119 120 125
5
80 106 106 120 108 108 120 109 110 118 111 111 118
75 102 102 117 103 104 117 103 106 115 107 107 114
140 144 145 150 146 146 149
F 130 137 138 144 139 140 143
L 120 130 131 138 133 133 137 135 135 138
A 110 123 124 132 125 126 131 127 128 131
P 100 116 117 126 118 119 126 120 120 125 121 122 126
S 90 108 110 120 110 111 120 112 112 119 113 114 119
15
80 100 102 114 102 103 114 104 104 113 105 106 112
75 96 98 111 98 99 111 100 100 110 101 102 109
CHECK MINIMUM V1(mcg) AND/OR VrMIN IN BOXED AREA.
MINIMUM V1(mcg) KIAS
PRESS ACTUAL OAT °C
ALT -50 50 15 20 25 30 35 40 45 50 55
0 112 111 111 111 111 110 109 107 104 102 100
2000 110 109 109 109 109 108 106 104 102 100 97
4000 110 109 109 108 108 108 106 103 101 98
6000 107 106 106 106 105 103 101 99 96 93
8000 103 102 102 101 100 97 95 94
9000 101 100 100 99 95 93 90
For Bleeds OFF Increase V1(mcg) By 2 Knots
Sec. 5 Page 14 737
Rev. 11/15/02 #41 Continental Flight Manual
@ Takeoff V Speeds
PMC ON
SLOPE/WIND V1 ADJUSTMENT*
WEIGHT SLOPE % WIND KTS
1000 DN UP TAIL HEAD
LB -2 0 2 -15 0 40
140 -2 0 2 -2 0 1
120 -2 0 1 -3 0 1
100 -2 0 1 -3 0 1
80 -2 0 2 -4 0 2
*V1 NOT TO EXCEED Vr
FLAP
WT
1000
A B C D E
LB V1 Vr V2 V1 Vr V2 V1 Vr V2 V1 Vr V2 V1 Vr V2
　
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