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Performance Inflight -
Text
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.16.12
For Maximum Climb and Go-Around thrust setting with both PMC’s Off,
use PMC On %N1.
Gear Down
This section contains performance for airplane operation with the landing
gear extended for all phases of flight. The data is based on engine bleeds
for normal air conditioning.
Note: The Flight Management Computer System (FMCS) does not contain
special provisions for operation with landing gear extended. As a result,
the FMCS will generate inaccurate enroute speed schedules, display nonconservative
predictions of fuel burn, estimated time of arrival (ETA),
maximum altitude, and compute overly shallow descent path. To obtain
accurate ETA predictions, gear down cruise speed and altitude should be
entered on the CLB and CRZ pages. Gear down cruise speed should also
be entered on the DES page. Use of VNAV during descent under these
circumstances is not recommended.
Tables for gear down performance in this section are identical in format
and used in the same manner as tables for the gear up configuration
previously described.
December 3, 2004
737 Flight Crew Operations Manual
Performance Inflight - Chapter PI
General Section 20
737-300/CFM56-3_22K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
PI.20.1
PI.20 Performance Inflight --General General Takeoff Speeds
160
113
C
4 &
B
A
D
111
118
125
116
139
121
128
136
103
135
113
122
131
117
125
121
130
112
125
132
146
153
122
129
168
101
126
134
106
124
133
120
129
100
125
133
123
131
127
139
119
145
152
118
125
132
139
146
153
130
137
168
99
108
116
124
132
140
148
105
114
122
131
140
148
156
109
118
127
164
115
123
131
129
125
160
120
126
132
139
145
152
119
126
146
153
160
138
145
153
160
168
98
106
122
146
103
112
129
154
107
116
125
134
144
153
162
121
129
KG
35
40
45
50
55
60
65
35
40
45
50
55
60
65
35
40
45
50
55
60
65
BELOW 10 20
40 60
& BELOW TEMPERATURE `F
80 100 120 140 160
TEMPERATURE `C
COLUMN REFERENCE
30 40 50 60 70
0
3
6
9
V1 VR V2 V1 VR V2 V1 VR V2
15
5
1
A B C D
1000 V1 VR V2
WT
1000 FT
PRESS ALT
* V 1 N O T T O E X C E E D VR
KG 0
1000
WEIGHT
S L O P E / W I N D V1 ADJUSTMENT*
-2 2
-2
-2
-2
0000
0000
-15 0
-3
-3
-3
-3 11
40
65
55
45
35
-2 3211
11
158
149
141
132
123
114
104
151
143
135
127
118
109
100
144
136
113
104
96
146
137
120
138
130
114
131
124
139
132
152
143
134
116
107
152
145
137
120
112
103
145
138
106
97
155
146
137
160
152
145
122
132
125
112
161
153
144
136
118
109
146
139
114
105
117
108
165
156
147
138
110
149
141
115
118
109
160
152
144
137
139
132
124
117
138
118
147
139
111
132
107
118
110
102
150
140
126
117
108
119
111
152
144
131
123
SLOPE %
DN UP
WIND KTS
TAIL HEAD
FLAPS
CHECK V1(MCG).
June 7, 2002
737 Flight Crew Operations Manual
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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