Boeing 737 - 600/700/800/900. Operations Manual (1997 year) - page 20
Performance Dispatch
Takeoff
FAA
Category G Brakes
Boeing 737 Operations Manual
Takeoff
Takeoff Field & Climb Limit Weights - Dry Runway
Flaps 5
8000 FT Pressure Altitude
FIELD LIMIT WEIGHT (1000 LB)
CORR'D FIELD
OAT (°C)
LENGTH (FT)
-40
0
11
14
18
22
26
30
35
40
50
4000
95.2
88.4
86.7
86.3
85.2
84.1
82.8
81.1
78.5
76.1
71.6
4200
98.1
91.1
89.4
89.0
87.9
86.7
85.4
83.6
81.1
78.6
73.9
4600
103.8
96.5
94.7
94.3
93.1
91.9
90.5
88.7
86.0
83.3
78.5
5000
109.2
101.6
99.7
99.2
98.0
96.8
95.3
93.4
90.6
87.8
82.7
5400
114.3
106.3
104.3
103.8
102.6
101.3
99.7
97.7
94.8
91.9
86.6
5800
119.1
110.8
108.7
108.2
106.9
105.5
103.9
101.8
98.8
95.8
90.3
6200
123.6
115.0
112.9
112.3
110.9
109.5
107.9
105.7
102.5
99.4
93.7
6600
128.0
119.0
116.8
116.2
114.8
113.4
111.6
109.4
106.1
102.8
96.9
7000
132.2
122.9
120.7
120.1
118.6
117.1
115.3
113.0
109.5
106.2
100.1
7400
136.3
126.7
124.4
123.8
122.3
120.7
118.9
116.4
112.9
109.5
103.1
7800
140.2
130.4
128.0
127.3
125.8
124.2
122.2
119.8
116.2
112.6
106.1
8200
144.0
134.0
131.5
130.8
129.2
127.6
125.6
123.1
119.4
115.7
109.1
8600
147.7
137.4
134.9
134.2
132.6
130.9
128.9
126.3
122.5
118.7
111.9
9000
151.0
140.5
137.9
137.2
135.5
133.8
131.8
129.1
125.2
121.4
114.4
9400
154.0
143.2
140.6
139.9
138.2
136.4
134.3
131.6
127.6
123.7
116.6
9800
156.7
145.8
143.1
142.4
140.6
138.8
136.7
133.9
129.9
125.9
118.6
10200
159.3
148.2
145.4
144.7
142.9
141.1
138.9
136.1
132.0
128.0
120.6
10600
161.8
150.4
147.7
146.9
145.1
143.3
141.1
138.2
134.0
129.9
122.4
CLIMB LIMIT
148.0
147.4
147.2
147.0
145.3
143.4
140.6
136.5
130.7
125.3
115.7
WT (1000 LB)
10000 FT Pressure Altitude
FIELD LIMIT WEIGHT (1000 LB)
CORR'D FIELD
OAT (°C)
LENGTH (FT)
-40
0
11
14
18
22
26
30
35
40
50
4000
88.6
82.3
80.7
79.9
78.8
77.8
76.5
74.8
72.4
69.9
65.2
4200
91.3
84.9
83.2
82.4
81.3
80.3
79.0
77.3
74.7
72.2
67.3
4600
96.7
90.0
88.2
87.4
86.3
85.1
83.8
82.0
79.3
76.7
71.6
5000
101.8
94.8
92.9
92.0
90.9
89.7
88.3
86.4
83.6
80.8
75.5
5400
106.5
99.2
97.2
96.3
95.1
93.8
92.4
90.4
87.5
84.6
79.0
5800
111.0
103.4
101.3
100.3
99.1
97.8
96.3
94.2
91.2
88.2
82.4
6200
115.2
107.3
105.2
104.2
102.8
101.5
100.0
97.8
94.6
91.5
85.5
6600
119.3
111.0
108.9
107.8
106.4
105.0
103.4
101.2
97.9
94.7
88.4
7000
123.2
114.7
112.4
111.3
109.9
108.5
106.8
104.5
101.1
97.8
91.3
7400
127.0
118.2
115.9
114.8
113.3
111.8
110.1
107.7
104.2
100.8
94.1
7800
130.6
121.6
119.2
118.0
116.5
115.0
113.3
110.8
107.2
103.7
96.8
8200
134.2
125.0
122.5
121.3
119.8
118.2
116.4
113.9
110.2
106.6
99.5
8600
137.7
128.2
125.7
124.5
122.9
121.3
119.4
116.8
113.1
109.3
102.1
9000
140.8
131.1
128.5
127.2
125.6
124.0
122.1
119.4
115.6
111.8
104.4
9400
143.5
133.6
131.0
129.7
128.0
126.4
124.4
121.7
117.8
113.9
106.3
9800
146.1
136.0
133.3
132.0
130.3
128.6
126.6
123.8
119.8
115.9
108.2
10200
148.5
138.2
135.5
134.1
132.4
130.7
128.7
125.9
121.8
117.8
109.9
10600
150.8
140.3
137.6
136.2
134.5
132.7
130.7
127.8
123.7
119.6
111.6
CLIMB LIMIT
138.8
137.9
137.2
136.0
134.3
132.4
129.7
125.8
120.3
115.1
104.9
WT (1000 LB)
With engine bleed for packs off, increase field limit weight by 800 lb and climb limit weight by 3100 lb.
With engine anti-ice on, decrease field limit weight by 500 lb and climb limit weight by 600 lb.
With engine and wing anti-ice on (optional system), decrease field limit weight by 1900 lb and climb limit
weight by 3200 lb.
PD.40.4
Performance Dispatch
FAA
Takeoff
Category G Brakes
Boeing 737 Operations Manual
Takeoff
Takeoff Field Corrections - Wet Runway
Slope Corrections
FIELD LENGTH
SLOPE CORRECTED FIELD LENGTH (FT)
AVAILABLE
RUNWAY SLOPE (%)
(FT)
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
4200
4330
4300
4260
4230
4200
4160
4110
4070
4020
4600
4770
4730
4690
4640
4600
4540
4480
4420
4360
5000
5210
5160
5110
5050
5000
4930
4850
4780
4700
5400
5660
5590
5530
5460
5400
5310
5220
5130
5040
5800
6100
6030
5950
5880
5800
5700
5590
5490
5380
6200
6540
6460
6370
6290
6200
6080
5960
5840
5720
6600
6990
6890
6790
6700
6600
6470
6330
6200
6060
7000
7430
7320
7210
7110
7000
6850
6700
6550
6400
7400
7870
7750
7640
7520
7400
7240
7070
6910
6740
7800
8310
8190
8060
7930
7800
7620
7440
7260
7080
8200
8760
8620
8480
8340
8200
8010
7810
7620
7420
8600
9200
9050
8900
8750
8600
8390
8180
7970
7760
9000
9640
9480
9320
9160
9000
8780
8550
8330
8100
9400
10090
9910
9740
9570
9400
9160
8920
8680
8440
9800
10530
10350
10160
9980
9800
9550
9290
9040
8780
10200
11000
10800
10600
10400
10200
9930
9660
9390
9120
10600
11500
11270
11050
10820
10600
10320
10030
9750
9460
11000
11990
11740
11500
11250
11000
10700
10400
10100
9800
11400
12490
12220
11940
11670
11400
11090
10770
10460
10140
11800
12990
12690
12390
12100
11800
11470
11140
10810
10480
Wind Corrections
SLOPE CORR’D
SLOPE & WIND CORRECTED FIELD LENGTH (FT)
FIELD LENGTH
WIND COMPONENT (KTS)
(FT)
-15
-10
-5
0
10
20
30
40
4200
3050
3430
3820
4200
4460
4730
5000
5280
4600
3390
3790
4200
4600
4870
5160
5440
5740
5000
3730
4150
4580
5000
5290
5580
5890
6190
5400
4070
4520
4960
5400
5700
6010
6330
6650
5800
4410
4880
5340
5800
6120
6440
6770
7110
6200
4750
5240
5720
6200
6530
6870
7220
7570
6600
5100
5600
6100
6600
6940
7300
7660
8030
7000
5440
5960
6480
7000
7360
7730
8100
8490
7400
5780
6320
6860
7400
7770
8150
8550
8950
7800
6120
6680
7240
7800
8190
8580
8990
9410
8200
6460
7040
7620
8200
8600
9010
9430
9870
8600
6800
7400
8000
8600
9010
9440
9880
10320
9000
7140
7760
8380
9000
9430
9870
10320
10780
9400
7480
8120
8760
9400
9840
10300
10760
11240
9800
7820
8480
9140
9800
10260
10720
11210
11700
10200
8160
8840
9520
10200
10670
11150
11650
12160
10600
8500
9200
9900
10600
11080
11580
12090
12620
11000
8840
9560
10280
11000
11500
12010
12540
13080
11400
9180
9920
10660
11400
11910
12440
12980
13540
11800
9520
10280
11040
11800
12330
12870
13420
14000
PD.40.5
Performance Dispatch
Takeoff
FAA
Category G Brakes
Boeing 737 Operations Manual
Takeoff
Takeoff Field & Climb Limit Weights - Wet Runway
Flaps 5
Sea Level Pressure Altitude
FIELD LIMIT WEIGHT (1000 LB)
CORR'D FIELD
OAT (°C)
LENGTH (FT)
-40
0
11
14
18
22
26
30
35
40
50
4000
124.0
115.5
113.2
112.6
111.8
111.0
110.2
109.4
106.1
103.0
96.8
4200
127.6
118.8
116.4
115.8
114.9
114.1
113.3
112.5
109.2
105.9
99.5
4600
134.6
125.3
122.8
122.1
121.2
120.3
119.5
118.6
115.1
111.6
104.8
5000
141.2
131.4
128.8
128.1
127.1
126.2
125.3
124.4
120.7
117.0
109.9
5400
147.5
137.2
134.5
133.7
132.7
131.8
130.8
129.9
126.0
122.2
114.7
5800
153.5
142.8
139.9
139.1
138.1
137.1
136.1
135.1
131.1
127.1
119.3
6200
159.1
148.0
145.0
144.2
143.2
142.1
141.1
140.1
135.9
131.7
123.6
6600
164.6
153.1
150.0
149.1
148.0
147.0
145.9
144.8
140.5
136.2
127.8
7000
169.9
157.9
154.7
153.9
152.8
151.6
150.6
149.4
144.9
140.5
131.8
7400
175.0
162.7
159.4
158.5
157.3
156.2
155.1
153.9
149.3
144.7
135.8
7800
179.9
167.3
163.9
163.0
161.8
160.6
159.4
158.2
153.4
148.7
139.5
8200
184.8
171.7
168.2
167.3
166.1
164.9
163.7
162.4
157.5
152.7
143.2
8600
189.4
176.0
172.4
171.5
170.2
169.0
167.7
166.5
161.4
156.5
146.7
9000
189.9
180.0
176.3
175.3
174.0
172.8
171.5
170.2
165.0
160.0
150.0
9400
189.9
183.7
180.0
179.0
177.6
176.3
175.0
173.7
168.4
163.2
153.0
9800
189.9
187.4
183.5
182.5
181.1
179.8
178.5
177.2
171.7
166.4
156.0
10200
189.9
189.9
187.0
185.9
184.5
183.2
181.8
180.5
174.9
169.5
158.8
10600
189.9
189.9
189.9
189.2
187.8
186.4
185.1
183.7
178.0
172.4
161.6
CLIMB LIMIT
188.1
187.4
186.8
186.6
186.4
186.1
185.8
185.4
177.7
170.3
155.9
WT (1000 LB)
2000 FT Pressure Altitude
FIELD LIMIT WEIGHT (1000 LB)
CORR'D FIELD
OAT (°C)
LENGTH (FT)
-40
0
11
14
18
22
26
30
35
40
50
4000
117.0
108.6
106.5
105.9
105.2
104.4
103.7
101.8
98.9
96.0
90.3
4200
120.4
111.7
109.5
108.9
108.1
107.4
106.6
104.7
101.7
98.7
92.8
4600
127.0
117.8
115.4
114.8
114.0
113.2
112.4
110.4
107.2
104.0
97.7
5000
133.2
123.5
121.1
120.4
119.6
118.7
117.9
115.7
112.4
109.0
102.5
5400
139.1
128.9
126.4
125.7
124.8
123.9
123.1
120.8
117.3
113.8
106.9
5800
144.7
134.1
131.5
130.8
129.8
128.9
128.0
125.7
122.0
118.3
111.2
6200
150.0
139.1
136.3
135.6
134.6
133.6
132.7
130.2
126.5
122.6
115.2
6600
155.1
143.8
140.9
140.1
139.1
138.2
137.2
134.6
130.7
126.7
119.1
7000
160.1
148.4
145.4
144.6
143.6
142.5
141.5
138.9
134.9
130.7
122.8
7400
164.9
152.8
149.7
148.9
147.9
146.8
145.8
143.1
138.9
134.6
126.5
7800
169.6
157.1
153.9
153.1
152.0
150.9
149.8
147.1
142.8
138.4
130.0
8200
174.1
161.3
158.0
157.2
156.0
154.9
153.8
151.0
146.5
142.0
133.4
8600
178.4
165.3
161.9
161.1
159.9
158.8
157.6
154.7
150.2
145.5
136.6
9000
182.5
169.0
165.6
164.7
163.5
162.3
161.2
158.1
153.5
148.8
139.7
9400
186.3
172.5
169.0
168.0
166.8
165.6
164.5
161.4
156.6
151.8
142.4
9800
189.9
175.9
172.3
171.3
170.1
168.9
167.7
164.5
159.6
154.7
145.1
10200
189.9
179.1
175.5
174.5
173.2
172.0
170.8
167.5
162.6
157.5
147.8
10600
189.9
182.3
178.6
177.6
176.3
175.0
173.8
170.5
165.4
160.2
150.3
CLIMB LIMIT
179.3
178.6
178.1
178.0
177.8
177.6
177.3
173.1
166.2
159.2
145.8
WT (1000 LB)
With engine bleed for packs off, increase field limit weight by 800 lb and climb limit weight by 3100 lb.
With engine anti-ice on, decrease field limit weight by 400 lb and climb limit weight by 600 lb.
With engine and wing anti-ice on (optional system), decrease field limit weight by 1700 lb and climb limit
weight by 3200 lb.
PD.40.6
Performance Dispatch
FAA
Takeoff
Category G Brakes
Boeing 737 Operations Manual
Takeoff
Takeoff Field & Climb Limit Weights - Wet Runway
Flaps 5
4000 FT Pressure Altitude
FIELD LIMIT WEIGHT (1000 LB)
CORR'D FIELD
OAT (°C)
LENGTH (FT)
-40
0
11
14
18
22
26
30
35
40
50
4000
109.3
101.4
99.4
98.9
98.2
97.6
96.2
94.6
92.1
89.4
84.4
4200
112.4
104.3
102.2
101.7
101.0
100.3
98.9
97.3
94.7
91.9
86.8
4600
118.5
109.9
107.7
107.2
106.4
105.7
104.2
102.5
99.8
96.8
91.4
5000
124.3
115.2
113.0
112.4
111.6
110.8
109.3
107.5
104.6
101.5
95.7
5400
129.8
120.3
117.9
117.3
116.5
115.7
114.1
112.2
109.2
105.9
99.9
5800
135.0
125.1
122.7
122.0
121.1
120.3
118.6
116.6
113.5
110.1
103.9
6200
140.0
129.7
127.1
126.5
125.6
124.7
122.9
120.9
117.6
114.1
107.6
6600
144.7
134.1
131.4
130.7
129.8
128.9
127.1
124.9
121.6
117.9
111.2
7000
149.3
138.3
135.6
134.8
133.9
133.0
131.1
128.9
125.4
121.6
114.7
7400
153.8
142.5
139.6
138.9
137.9
136.9
135.0
132.7
129.1
125.2
118.0
7800
158.1
146.4
143.5
142.7
141.7
140.7
138.7
136.4
132.7
128.7
121.3
8200
162.4
150.3
147.3
146.5
145.5
144.5
142.4
140.0
136.2
132.1
124.5
8600
166.4
154.0
150.9
150.1
149.1
148.0
145.9
143.5
139.6
135.3
127.5
9000
170.1
157.5
154.3
153.5
152.4
151.3
149.2
146.6
142.6
138.3
130.3
9400
173.6
160.7
157.4
156.6
155.5
154.4
152.2
149.6
145.5
141.0
132.9
9800
177.0
163.8
160.5
159.6
158.5
157.3
155.1
152.4
148.3
143.7
135.4
10200
180.3
166.8
163.4
162.5
161.4
160.2
157.9
155.2
150.9
146.3
137.8
10600
183.5
169.7
166.3
165.4
164.2
163.0
160.7
157.9
153.5
148.8
140.1
CLIMB LIMIT
168.6
167.9
167.5
167.4
167.2
167.0
164.5
161.0
155.2
148.5
136.5
WT (1000 LB)
6000 FT Pressure Altitude
FIELD LIMIT WEIGHT (1000 LB)
CORR'D FIELD
OAT (°C)
LENGTH (FT)
-40
0
11
14
18
22
26
30
35
40
50
4000
101.9
94.6
92.8
92.3
91.7
90.5
89.3
87.9
85.6
83.1
78.6
4200
104.8
97.2
95.4
94.9
94.2
93.0
91.8
90.3
88.0
85.4
80.8
4600
110.4
102.4
100.4
99.9
99.2
98.0
96.7
95.1
92.6
89.9
85.0
5000
115.8
107.4
105.3
104.8
104.0
102.7
101.3
99.7
97.1
94.2
89.1
5400
120.9
112.1
109.9
109.3
108.6
107.2
105.8
104.0
101.3
98.3
92.9
5800
125.7
116.6
114.3
113.7
112.9
111.5
110.0
108.2
105.3
102.2
96.6
6200
130.3
120.8
118.4
117.8
117.0
115.5
114.0
112.1
109.1
105.9
100.0
6600
134.7
124.9
122.4
121.8
120.9
119.4
117.8
115.8
112.8
109.4
103.3
7000
139.0
128.8
126.3
125.6
124.7
123.1
121.5
119.5
116.3
112.8
106.5
7400
143.2
132.6
130.0
129.3
128.4
126.8
125.1
123.0
119.7
116.1
109.7
7800
147.2
136.3
133.6
132.9
132.0
130.3
128.5
126.4
123.0
119.3
112.7
8200
151.1
139.9
137.2
136.4
135.5
133.7
131.9
129.7
126.3
122.5
115.6
8600
154.8
143.4
140.5
139.8
138.8
137.0
135.1
132.9
129.4
125.4
118.4
9000
158.3
146.5
143.6
142.9
141.8
140.0
138.1
135.8
132.2
128.2
121.0
9400
161.5
149.5
146.5
145.7
144.7
142.8
140.9
138.5
134.8
130.7
123.3
9800
164.6
152.4
149.3
148.5
147.4
145.5
143.5
141.1
137.3
133.1
125.6
10200
167.6
155.1
152.0
151.2
150.1
148.1
146.1
143.6
139.8
135.5
127.8
10600
170.6
157.8
154.6
153.8
152.7
150.7
148.6
146.1
142.2
137.8
129.9
CLIMB LIMIT
158.1
157.5
157.2
157.1
156.9
154.8
152.5
149.3
143.6
137.3
126.7
WT (1000 LB)
With engine bleed for packs off, increase field limit weight by 800 lb and climb limit weight by 3100 lb.
With engine anti-ice on, decrease field limit weight by 400 lb and climb limit weight by 600 lb.
With engine and wing anti-ice on (optional system), decrease field limit weight by 1700 lb and climb limit
weight by 3200 lb.
PD.40.7
Performance Dispatch
Takeoff
FAA
Category G Brakes
Boeing 737 Operations Manual
Takeoff
Takeoff Field & Climb Limit Weights - Wet Runway
Flaps 5
8000 FT Pressure Altitude
FIELD LIMIT WEIGHT (1000 LB)
CORR'D FIELD
OAT (°C)
LENGTH (FT)
-40
0
11
14
18
22
26
30
35
40
50
4000
95.0
88.3
86.6
86.2
85.2
84.1
82.8
81.2
78.8
76.6
72.5
4200
97.7
90.7
89.0
88.6
87.5
86.4
85.1
83.4
81.0
78.7
74.5
4600
102.9
95.5
93.7
93.3
92.1
91.0
89.6
87.8
85.2
82.8
78.3
5000
107.9
100.1
98.2
97.7
96.6
95.3
93.9
92.0
89.3
86.7
82.0
5400
112.6
104.5
102.5
102.0
100.8
99.5
97.9
96.0
93.1
90.5
85.6
5800
117.1
108.7
106.6
106.1
104.8
103.4
101.8
99.8
96.8
94.0
88.9
6200
121.3
112.6
110.5
109.9
108.5
107.2
105.5
103.4
100.3
97.4
92.1
6600
125.4
116.3
114.1
113.5
112.2
110.7
109.0
106.8
103.6
100.6
95.1
7000
129.4
120.0
117.7
117.1
115.7
114.2
112.4
110.1
106.8
103.7
98.0
7400
133.2
123.6
121.2
120.6
119.1
117.6
115.7
113.4
110.0
106.8
100.9
7800
136.9
127.0
124.5
123.9
122.4
120.8
118.9
116.5
113.0
109.7
103.7
8200
140.6
130.3
127.8
127.1
125.6
124.0
122.0
119.5
115.9
112.6
106.4
8600
144.0
133.5
130.9
130.3
128.6
127.0
125.0
122.5
118.8
115.3
108.9
9000
147.2
136.4
133.8
133.1
131.4
129.7
127.7
125.1
121.3
117.8
111.2
9400
150.2
139.1
136.4
135.7
134.0
132.3
130.2
127.5
123.7
120.0
113.3
9800
153.0
141.8
139.0
138.3
136.6
134.8
132.6
129.9
125.9
122.2
115.4
10200
155.8
144.3
141.5
140.8
139.0
137.2
135.0
132.2
128.1
124.3
117.4
10600
158.5
146.8
143.9
143.1
141.3
139.5
137.3
134.4
130.3
126.4
119.3
CLIMB LIMIT
148.0
147.4
147.2
147.0
145.3
143.4
140.6
136.5
130.7
125.3
115.7
WT (1000 LB)
10000 FT Pressure Altitude
FIELD LIMIT WEIGHT (1000 LB)
CORR'D FIELD
OAT (°C)
LENGTH (FT)
-40
0
11
14
18
22
26
30
35
40
50
4000
88.7
82.4
80.8
80.0
79.0
78.0
76.8
75.2
73.0
70.8
66.5
4200
91.2
84.7
83.0
82.2
81.2
80.1
78.9
77.3
75.0
72.7
68.3
4600
96.0
89.1
87.4
86.5
85.4
84.3
83.0
81.3
78.9
76.5
71.8
5000
100.7
93.4
91.5
90.6
89.5
88.3
87.0
85.1
82.6
80.1
75.1
5400
105.0
97.5
95.5
94.6
93.4
92.1
90.7
88.8
86.1
83.5
78.3
5800
109.2
101.3
99.3
98.3
97.1
95.8
94.3
92.3
89.5
86.8
81.4
6200
113.2
105.0
102.8
101.8
100.5
99.2
97.7
95.6
92.7
89.9
84.3
6600
117.0
108.4
106.2
105.2
103.9
102.5
100.9
98.8
95.8
92.8
87.0
7000
120.6
111.8
109.6
108.5
107.1
105.7
104.0
101.8
98.7
95.6
89.7
7400
124.2
115.1
112.8
111.7
110.2
108.8
107.1
104.8
101.6
98.4
92.3
7800
127.6
118.3
115.9
114.7
113.3
111.8
110.0
107.7
104.4
101.1
94.8
8200
131.0
121.4
118.9
117.7
116.2
114.7
112.9
110.5
107.1
103.7
97.2
8600
134.2
124.3
121.8
120.6
119.0
117.5
115.6
113.1
109.6
106.2
99.5
9000
137.2
127.0
124.4
123.2
121.6
120.0
118.1
115.5
112.0
108.5
101.6
9400
139.9
129.5
126.9
125.6
124.0
122.3
120.4
117.8
114.1
110.5
103.5
9800
142.5
131.9
129.2
127.9
126.3
124.6
122.6
119.9
116.2
112.5
105.3
10200
145.1
134.3
131.5
130.2
128.5
126.7
124.7
122.0
118.2
114.4
107.1
10600
147.6
136.5
133.7
132.3
130.6
128.8
126.8
124.0
120.1
116.3
108.8
CLIMB LIMIT
138.8
137.9
137.2
136.0
134.3
132.4
129.7
125.8
120.3
115.1
104.9
WT (1000 LB)
With engine bleed for packs off, increase field limit weight by 800 lb and climb limit weight by 3100 lb.
With engine anti-ice on, decrease field limit weight by 400 lb and climb limit weight by 600 lb.
With engine and wing anti-ice on (optional system), decrease field limit weight by 1700 lb and climb limit
weight by 3200 lb.
PD.40.8
Performance Dispatch
FAA
Takeoff
Category G Brakes
Boeing 737 Operations Manual
Takeoff
Takeoff Obstacle Limit Weight
Flaps 5
Sea Level 30°C & Below, Zero Wind
Based on engine bleed for packs on and anti-ice off
Reference Obstacle Limit Weight (1000 LB)
OBSTACLE
DISTANCE FROM BRAKE RELEASE (1000 FT)
HEIGHT (FT)
8
10
12
14
16
18
20
22
24
10
157.5
175.5
188.6
50
147.5
163.9
176.8
186.3
100
138.4
153.9
166.1
175.5
182.9
187.9
150
131.4
146.1
158.0
167.3
174.7
180.7
185.3
188.6
200
125.4
139.7
151.3
160.6
168.1
174.2
179.2
183.2
186.5
250
120.2
134.2
145.5
154.8
162.4
168.6
173.8
178.1
181.7
300
115.6
129.3
140.4
149.6
157.3
163.6
168.9
173.4
177.2
350
111.4
124.9
135.8
145.0
152.7
159.1
164.6
169.2
173.1
400
107.5
120.8
131.7
140.8
148.5
155.0
160.5
165.3
169.3
450
103.9
117.2
127.9
136.9
144.6
151.2
156.8
161.6
165.8
500
100.6
113.7
124.4
133.4
141.0
147.6
153.3
158.2
162.5
550
97.5
110.6
121.2
130.1
137.7
144.3
150.0
155.0
159.3
600
94.6
107.6
118.1
127.0
134.6
141.1
146.9
151.9
156.3
650
91.9
104.7
115.2
124.1
131.6
138.2
144.0
149.0
153.5
700
102.1
112.5
121.3
128.9
135.4
141.2
146.3
150.8
750
99.5
109.9
118.7
126.2
132.8
138.6
143.7
148.3
800
97.2
107.5
116.2
123.7
130.3
136.1
141.2
145.8
850
94.9
105.2
113.9
121.3
127.9
133.7
138.8
143.4
900
92.7
102.9
111.6
119.1
125.6
131.4
136.6
141.2
950
90.7
100.8
109.4
116.9
123.4
129.2
134.4
139.0
1000
98.8
107.4
114.8
121.3
127.1
132.3
136.9
Obstacle height must be calculated from lowest point of the runway to conservatively account for runway
slope.
OAT Adjustments
REFERENCE OBSTACLE LIMIT WEIGHT (1000 LB)
OAT (°C)
90
110
130
150
170
190
30 & BELOW
0
0
0
0
0
0
32
-1.3
-1.7
-2.0
-2.3
-2.7
-3.0
34
-2.6
-3.3
-4.0
-4.7
-5.4
-6.0
36
-4.0
-5.0
-6.0
-7.0
-8.0
-9.1
38
-5.3
-6.6
-8.0
-9.4
-10.7
-12.1
40
-6.5
-8.2
-9.9
-11.6
-13.3
-14.9
42
-7.7
-9.8
-11.8
-13.8
-15.8
-17.8
44
-9.0
-11.3
-13.6
-16.0
-18.3
-20.7
46
-10.2
-12.9
-15.5
-18.2
-20.8
-23.5
48
-11.4
-14.4
-17.4
-20.4
-23.4
-26.3
50
-12.7
-16.0
-19.3
-22.6
-25.9
-29.2
PD.40.9
Performance Dispatch
Takeoff
FAA
Category G Brakes
Boeing 737 Operations Manual
Takeoff
Takeoff Obstacle Limit Weight
Flaps 5
Sea Level 30°C & Below, Zero Wind
Based on engine bleed for packs on and anti-ice off
Pressure Altitude Adjustments
OAT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 LB)
ALT (FT)
90
110
130
150
170
190
S.L.& BELOW
0
0
0
0
0
0
1000
-3.3
-4.0
-4.6
-5.3
-6.0
-6.7
2000
-6.5
-7.9
-9.3
-10.6
-12.0
-13.4
3000
-9.6
-11.6
-13.7
-15.7
-17.8
-19.8
4000
-12.6
-15.3
-18.1
-20.8
-23.5
-26.2
5000
-15.5
-18.8
-22.2
-25.6
-29.0
-32.3
6000
-18.3
-22.4
-26.4
-30.4
-34.4
-38.4
7000
-20.9
-25.6
-30.3
-35.1
-39.8
-44.5
8000
-23.4
-28.9
-34.3
-39.8
-45.2
-50.6
9000
-26.0
-32.0
-38.0
-44.0
-50.1
-56.1
10000
-28.5
-35.1
-41.7
-48.3
-54.9
-61.5
Wind Adjustments
OAT & ALT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 LB)
WIND (KTS)
90
110
130
150
170
190
15 TW
-19.2
-18.8
-18.3
-17.9
-17.4
-16.9
10 TW
-12.8
-12.5
-12.2
-11.9
-11.6
-11.3
5 TW
-6.4
-6.3
-6.1
-6.0
-5.8
-5.6
0
0
0
0
0
0
0
10 HW
2.3
2.1
1.9
1.7
1.5
1.3
20 HW
4.5
4.1
3.8
3.4
3.0
2.6
30 HW
7.0
6.5
5.9
5.3
4.7
4.1
40 HW
9.5
8.8
8.0
7.2
6.4
5.6
With engine bleed for packs off, increase weight by 1400 lb.
With engine anti-ice on, decrease weight by 700 lb.
With engine and wing anti-ice on, decrease weight by 3300 lb (optional system).
PD.40.10
Performance Dispatch
FAA
Takeoff
Category G Brakes
Boeing 737 Operations Manual
Takeoff
Tire Speed Limit Weight
Flaps 5 Limit Weight (1000 LB)
AIRPORT PRESSURE ALTITUDE (FT)
OAT (°C)
0
2000
4000
6000
8000
10000
54
190.0
187.8
173.3
159.8
147.2
52
190.0
189.0
174.5
160.9
148.2
50
190.0
190.0
175.7
162.0
149.2
137.6
48
190.0
190.0
176.9
163.1
150.3
138.5
46
190.0
190.0
178.2
164.3
151.3
139.4
44
190.0
190.0
179.4
165.4
152.4
140.3
42
190.0
190.0
180.7
166.6
153.4
141.3
40
190.0
190.0
182.0
167.7
154.5
142.2
38
190.0
190.0
183.3
169.0
155.6
143.2
36
190.0
190.0
184.6
170.2
156.7
144.3
34
190.0
190.0
186.0
171.4
157.8
145.3
32
190.0
190.0
187.3
172.7
159.0
146.3
30
190.0
190.0
188.7
173.9
160.1
147.4
28
190.0
190.0
190.0
175.2
161.3
148.5
26
190.0
190.0
190.0
176.5
162.5
149.6
24
190.0
190.0
190.0
177.8
163.7
150.7
22
190.0
190.0
190.0
179.1
164.9
151.8
20
190.0
190.0
190.0
180.4
166.1
152.9
18
190.0
190.0
190.0
181.8
167.4
154.0
16
190.0
190.0
190.0
183.1
168.6
155.2
14
190.0
190.0
190.0
184.5
169.9
156.3
12
190.0
190.0
190.0
185.9
171.2
157.5
10
190.0
190.0
190.0
187.3
172.5
158.7
-40
190.0
190.0
190.0
190.0
190.0
190.0
Increase tire speed limit weight by 1200 lb per knot headwind.
Decrease tire speed limit weight by 2500 lb per knot tailwind.
PD.40.11
Performance Dispatch
Takeoff
FAA
Category G Brakes
Boeing 737 Operations Manual
Takeoff
Brake Energy Limits VMBE
Maximum Brake Energy Speed
REFERENCE VMBE (KIAS)
OAT (°C)
PRESSURE ALTITUDE (FT)
TO BE SUPPLIED
Weight Adjusted VMBE
WEIGHT
REFERENCE VMBE (KIAS)
(1000 LB)
TO BE SUPPLIED
PD.40.12
FAA
Category G Brakes
Boeing 737 Operations Manual
Performance Dispatch
Chapter PD
Enroute
Section 41
Enroute
Long Range Cruise Maximum Operating Altitude
Max Cruise Thrust
ISA + 10°C and Below
WEIGHT
OPTIMUM
TAT
MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
(1000 LB)
ALT (FT)
(°C)
1.20 (33°)
1.25 (36°)
1.30 (39°)
1.40 (44°)
1.50 (48°)
190
30000
-5
31900*
31900*
31900*
31500
30100
180
31200
-7
33500*
33500*
33500*
32600
31300
170
32400
-10
35000*
35000*
35000*
33900
32500
160
33700
-13
36300*
36300*
36300*
35100
33800
150
35100
-16
37600*
37600*
37600*
36500
35100
140
36500
-18
38900*
38900*
38900*
37900
36600
130
38100
-18
40300*
40300*
40300*
39500
38100
120
39700
-18
41000
41000
41000
41000
39800
110
41000
-18
41000
41000
41000
41000
41000
100
41000
-18
41000
41000
41000
41000
41000
90
41000
-18
41000
41000
41000
41000
41000
ISA + 15°C
WEIGHT
OPTIMUM
TAT
MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
(1000 LB)
ALT (FT)
(°C)
1.20 (33°)
1.25 (36°)
1.30 (39°)
1.40 (44°)
1.50 (48°)
190
30000
1
29300*
29300*
29300*
29300*
29300*
180
31200
-2
31500*
31500*
31500*
31500*
31300
170
32400
-4
33600*
33600*
33600*
33600*
32500
160
33700
-7
35300*
35300*
35300*
35100
33800
150
35100
-10
36700*
36700*
36700*
36500
35100
140
36500
-13
38000*
38000*
38000*
37900
36600
130
38100
-13
39300*
39300*
39300*
39300*
38100
120
39700
-13
40700*
40700*
40700*
40700*
39800
110
41000
-13
41000
41000
41000
41000
41000
100
41000
-13
41000
41000
41000
41000
41000
90
41000
-13
41000
41000
41000
41000
41000
ISA + 20°C
WEIGHT
OPTIMUM
TAT
MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
(1000 LB)
ALT (FT)
(°C)
1.20 (33°)
1.25 (36°)
1.30 (39°)
1.40 (44°)
1.50 (48°)
190
30000
7
26000*
26000*
26000*
26000*
26000*
180
31200
4
28200*
28200*
28200*
28200*
28200*
170
32400
1
30600*
30600*
30600*
30600*
30600*
160
33700
-2
33200*
33200*
33200*
33200*
33200*
150
35100
-5
35200*
35200*
35200*
35200*
35100
140
36500
-7
36600*
36600*
36600*
36600*
36600
130
38100
-7
38000*
38000*
38000*
38000*
38000*
120
39700
-7
39400*
39400*
39400*
39400*
39400*
110
41000
-7
40900*
40900*
40900*
40900*
40900*
100
41000
-7
41000
41000
41000
41000
41000
90
41000
-7
41000
41000
41000
41000
41000
*Denotes altitude thrust limited in level flight, 100 fpm residual rate of climb.
PD.41.1
Performance Dispatch
Enroute
FAA
Category G Brakes
Boeing 737 Operations Manual
Enroute
Long Range Cruise Trip Fuel and Time
Ground to Air Miles Conversion
AIR DISTANCE (NM)
GROUND
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
DISTANCE
TAILWIND COMPONENT (KTS)
100
80
60
40
20
(NM)
20
40
60
80
100
276
257
240
225
212
200
190
181
173
165
158
544
508
475
447
423
400
381
364
348
333
320
810
758
711
670
633
600
572
547
523
502
482
1077
1008
946
892
844
800
763
730
699
670
645
1342
1258
1181
1114
1054
1000
955
913
874
839
807
1606
1506
1416
1336
1265
1200
1146
1096
1050
1008
969
1870
1754
1650
1557
1475
1400
1337
1279
1225
1176
1132
2133
2002
1883
1779
1685
1600
1528
1462
1401
1345
1295
2395
2249
2117
2000
1895
1800
1720
1645
1577
1514
1458
2657
2496
2350
2221
2105
2000
1911
1829
1753
1684
1621
2917
2741
2582
2441
2315
2200
2103
2012
1929
1853
1784
3177
2987
2814
2661
2525
2400
2294
2196
2106
2023
1948
3437
3232
3046
2882
2735
2600
2486
2380
2282
2193
2111
3696
3477
3278
3102
2944
2800
2677
2563
2458
2362
2275
3955
3721
3509
3322
3154
3000
2869
2747
2635
2532
2439
4213
3966
3741
3542
3363
3200
3061
2931
2812
2703
2603
4471
4210
3972
3762
3573
3400
3252
3115
2989
2873
2767
4729
4454
4203
3981
3782
3600
3444
3299
3166
3043
2931
4986
4697
4434
4201
3992
3800
3636
3483
3343
3213
3096
5243
4940
4665
4420
4201
4000
3828
3668
3520
3384
3260
5500
5183
4895
4640
4410
4200
4019
3852
3696
3554
3424
5756
5426
5126
4859
4620
4400
4211
4036
3873
3724
3589
6011
5669
5356
5079
4829
4600
4403
4220
4050
3895
3753
6267
5911
5586
5298
5038
4800
4595
4404
4227
4065
3918
6522
6153
5816
5517
5247
5000
4786
4588
4404
4236
4082
PD.41.2
Performance Dispatch
FAA
Enroute
Category G Brakes
Boeing 737 Operations Manual
Enroute
Long Range Cruise Trip Fuel and Time
Reference Fuel and Time Required
PRESSURE ALTITUDE (1000 FT)
AIR
29
31
33
35
37
DIST
(NM)
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
(1000 LB)(HR:MIN)(1000 LB)(HR:MIN)(1000 LB)(HR:MIN)(1000 LB)(HR:MIN)(1000 LB)(HR:MIN)
200
3.7
0:38
3.7
0:38
3.7
0:37
3.7
0:38
3.7
0:38
400
6.3
1:06
6.2
1:05
6.2
1:05
6.1
1:04
6.1
1:04
600
8.8
1:35
8.7
1:33
8.6
1:32
8.5
1:31
8.4
1:31
800
11.4
2:03
11.2
2:01
11.0
1:59
10.9
1:58
10.8
1:57
1000
14.1
2:31
13.8
2:28
13.5
2:26
13.3
2:25
13.2
2:24
1200
16.8
2:59
16.4
2:55
16.1
2:53
15.8
2:51
15.7
2:50
1400
19.5
3:26
19.1
3:22
18.6
3:20
18.3
3:18
18.3
3:17
1600
22.2
3:54
21.7
3:50
21.2
3:47
20.8
3:44
20.8
3:43
1800
24.9
4:21
24.3
4:17
23.8
4:13
23.3
4:11
23.3
4:09
2000
27.6
4:49
27.0
4:44
26.3
4:40
25.8
4:38
25.8
4:36
2200
30.5
5:15
29.7
5:10
29.0
5:06
28.5
5:04
2400
33.3
5:42
32.5
5:37
31.8
5:33
31.3
5:30
2600
36.2
6:09
35.3
6:03
34.5
5:59
34.0
5:57
2800
39.0
6:36
38.1
6:30
37.2
6:25
36.7
6:23
3000
41.9
7:03
40.9
6:56
39.9
6:52
39.4
6:49
3200
44.9
7:29
43.8
7:23
42.9
7:18
3400
47.9
7:56
46.8
7:49
45.8
7:44
3600
51.0
8:22
49.7
8:15
48.7
8:10
3800
54.0
8:48
52.7
8:41
51.7
8:36
4000
57.0
9:15
55.6
9:07
54.6
9:02
4200
60.2
9:40
58.8
9:33
4400
63.4
10:06
62.0
9:59
4600
66.6
10:32
65.2
10:25
4800
69.8
10:58
68.3
10:51
5000
73.1
11:24
71.5
11:17
Fuel Required Adjustments (1000 LB)
REFERENCE FUEL REQUIRED
LANDING WEIGHT (1000 LB)
(1000 LB)
90
110
130
150
170
5
-0.8
-0.4
0.0
0.5
1.0
10
-1.6
-0.8
0.0
0.9
2.1
15
-2.4
-1.3
0.0
1.4
3.3
20
-3.2
-1.7
0.0
2.0
4.6
25
-4.0
-2.1
0.0
2.6
5.9
30
-4.8
-2.5
0.0
3.2
7.4
35
-5.6
-2.9
0.0
3.8
9.0
40
-6.4
-3.3
0.0
4.6
10.7
45
-7.2
-3.7
0.0
5.3
12.4
50
-8.0
-4.1
0.0
6.1
14.3
55
-8.8
-4.5
0.0
7.0
16.3
60
-9.6
-4.9
0.0
7.9
18.3
65
-10.4
-5.3
0.0
8.8
20.5
70
-11.2
-5.7
0.0
9.8
22.8
75
-12.0
-6.1
0.0
10.8
25.1
80
-12.8
-6.5
0.0
11.9
27.6
Based on 280/.78 climb, Long Range Cruise and .78/280/250 descent.
PD.41.3
Performance Dispatch
Enroute
FAA
Category G Brakes
Boeing 737 Operations Manual
Enroute
Long Range Cruise Step Climb
Ground to Air Miles Conversion
AIR DISTANCE (NM)
GROUND
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
DISTANCE
TAILWIND COMPONENT (KTS)
100
80
60
40
20
(NM)
20
40
60
80
100
1317
1239
1169
1107
1051
1000
954
912
874
838
806
1832
1725
1631
1546
1469
1400
1337
1279
1227
1178
1133
2346
2212
2092
1985
1888
1800
1720
1647
1580
1518
1460
2859
2698
2553
2424
2306
2200
2103
2014
1933
1857
1788
3372
3183
3014
2862
2725
2600
2486
2382
2286
2197
2115
3885
3669
3475
3301
3143
3000
2869
2749
2639
2538
2443
4397
4154
3936
3739
3562
3400
3252
3117
2993
2878
2771
4909
4638
4396
4178
3980
3800
3636
3485
3346
3218
3100
5421
5123
4856
4616
4398
4200
4019
3853
3700
3559
3428
5932
5607
5316
5054
4816
4600
4402
4221
4054
3900
3757
6443
6091
5776
5492
5234
5000
4786
4589
4408
4240
4085
Trip Fuel and Time Required
TRIP FUEL (1000 LB)
AIR DIST
TIME
LANDING WEIGHT (1000 LB)
(NM)
(HRS:MIN)
90
100
110
120
130
140
150
1000
10.4
11.0
11.7
12.4
13.3
14.0
14.8
2:25
1400
14.2
15.0
15.9
17.1
18.2
19.2
20.4
3:18
1800
18.0
19.1
20.3
21.8
23.3
24.6
26.1
4:11
2200
22.0
23.3
24.9
26.7
28.5
30.2
32.1
5:04
2600
26.0
27.6
29.6
31.7
33.9
35.9
38.2
5:57
3000
30.1
32.1
34.4
36.9
39.4
41.9
44.5
6:50
3400
34.4
36.7
39.4
42.2
45.2
48.0
50.9
7:43
3800
38.7
41.5
44.5
47.7
51.1
54.3
57.6
8:35
4200
43.2
46.4
49.7
53.4
57.1
60.7
64.5
9:28
4600
47.9
51.4
55.2
59.3
63.4
67.4
71.6
10:20
5000
52.7
56.5
60.8
65.3
69.8
74.3
78.9
11:12
Based on 280/.78 climb, Long Range Cruise, and .78/280/250 descent.
Valid for all pressure altitudes with 4000 ft step climb to 2000 ft above optimum altitude.
PD.41.4
Performance Dispatch
FAA
Enroute
Category G Brakes
Boeing 737 Operations Manual
Enroute
Short Trip Fuel and Time
Ground to Air Miles Conversion
AIR DISTANCE (NM)
GROUND
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
DISTANCE
TAILWIND COMPONENT (KTS)
100
80
60
40
20
(NM)
20
40
60
80
100
94
80
69
61
55
50
46
42
39
36
34
160
143
129
118
108
100
93
87
82
77
73
226
205
188
173
161
150
141
132
125
118
112
291
267
246
229
213
200
188
178
168
160
152
354
327
304
283
266
250
236
224
213
202
193
417
387
361
338
318
300
284
270
257
245
234
480
447
418
392
370
350
332
316
301
288
276
543
507
475
447
422
400
380
362
345
330
317
607
567
533
502
475
450
428
408
390
373
358
673
629
591
557
527
500
476
453
433
415
398
Trip Fuel and Time Required
AIR DIST
LANDING WEIGHT (1000 LB)
TIME
(NM)
90
110
130
150
170
(HRS:MIN)
FUEL (1000 LB)
1.2
1.3
1.5
1.6
1.7
50
0:14
ALT (FT)
12000
11000
9000
8000
7000
FUEL (1000 LB)
1.9
2.1
2.3
2.5
2.7
100
0:23
ALT (FT)
19000
17000
17000
16000
15000
FUEL (1000 LB)
2.5
2.7
3.0
3.3
3.5
150
0:30
ALT (FT)
25000
24000
23000
22000
20000
FUEL (1000 LB)
3.0
3.3
3.7
4.0
4.3
200
0:37
ALT (FT)
31000
27000
26000
26000
24000
FUEL (1000 LB)
3.5
3.9
4.3
4.7
5.1
250
0:44
ALT (FT)
39000
35000
31000
31000
27000
FUEL (1000 LB)
3.9
4.4
4.9
5.4
5.8
300
0:50
ALT (FT)
41000
39000
35000
33000
29000
FUEL (1000 LB)
4.4
4.9
5.5
6.0
6.6
350
0:57
ALT (FT)
41000
39000
37000
33000
31000
FUEL (1000 LB)
4.8
5.4
6.0
6.7
7.3
400
1:03
ALT (FT)
41000
39000
37000
33000
31000
FUEL (1000 LB)
5.3
5.9
6.6
7.3
8.1
450
1:10
ALT (FT)
41000
41000
37000
35000
31000
FUEL (1000 LB)
5.7
6.4
7.2
8.0
8.8
500
1:17
ALT (FT)
41000
41000
37000
35000
31000
Based on 280/.78 climb, Long Range Cruise, and .78/280/250 descent.
PD.41.5
Performance Dispatch
Enroute
FAA
Category G Brakes
Boeing 737 Operations Manual
Enroute
Holding Planning
Flaps Up
TOTAL FUEL FLOW (LB/HR)
WEIGHT
PRESSURE ALTITUDE (FT)
(1000 LB)
1500
5000
10000
15000
20000
25000
30000
35000
41000
190
6890
6790
6760
6720
6690
6750
7040
180
6560
6460
6400
6370
6300
6360
6570
170
6240
6130
6060
6030
5930
5970
6140
6640
160
5910
5800
5720
5680
5580
5590
5740
6040
150
5590
5480
5400
5330
5240
5200
5340
5540
140
5260
5150
5070
4990
4910
4830
4950
5080
130
4940
4830
4740
4660
4580
4470
4570
4670
5360
120
4620
4510
4420
4330
4250
4140
4190
4270
4690
110
4310
4190
4090
4000
3920
3830
3880
3940
4220
100
4010
3880
3770
3750
3660
3590
3540
3570
3770
90
3800
3670
3540
3440
3350
3280
3240
3210
3360
This table includes 5% additional fuel for holding in a racetrack pattern.
Crew Oxygen Requirements
Required Pressure (PSI) for 76 Cubic FT Cylinder
BOTTLE
NUMBER OF CREW USING OXYGEN
TEMPERATURE
°C
°F
2
3
4
50
122
735
1055
1360
45
113
725
1040
1340
40
104
715
1020
1320
35
92
700
1005
1300
30
86
690
990
1280
25
77
680
975
1255
20
68
670
960
1240
15
59
655
940
1215
10
50
645
925
1195
5
41
635
910
1175
0
32
620
890
1150
-5
23
610
875
1130
-10
14
600
860
1110
Required Pressure (PSI) for 114/115 Cubic FT Cylinder
BOTTLE
NUMBER OF CREW USING OXYGEN
TEMPERATURE
°C
°F
2
3
4
50
122
530
735
945
45
113
520
725
930
40
104
510
715
915
35
92
505
700
900
30
86
495
690
885
25
77
485
680
870
20
68
480
670
860
15
59
470
655
840
10
50
460
645
830
5
41
455
635
815
0
32
445
620
800
-5
23
440
610
785
-10
14
430
600
770
PD.41.6
Performance Dispatch
FAA
Enroute
Category G Brakes
Boeing 737 Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Net Level Off Weight
PRESSURE ALTITUDE
LEVEL OFF WEIGHT (1000 LB)
(1000 FT)
ISA + 10°C & BELOW
ISA + 15°C
ISA + 20°C
30
92.5
28
100.7
97.7
94.6
26
109.5
106.1
102.9
24
119.0
115.2
111.6
22
129.2
124.9
120.8
20
140.0
135.3
130.7
18
151.0
145.6
140.1
16
161.6
156.2
151.0
14
170.0
166.2
161.9
12
181.5
176.5
170.2
Anti-Ice Adjustments
LEVEL OFF WEIGHT ADJUSTMENT (1000 LB)
ANTI-ICE
PRESSURE ALTITUDE (1000 FT)
CONFIGURATION
12
14
16
18
20
22
24
26
28
30
ENGINE ONLY
-3.9
-3.7
-3.7
-3.7
-3.3
-3.2
-3.0
-2.7
-2.5
-1.7
ENGINE & WING
-15.4
-14.7
-14.2
-14.4
-13.3
-12.1
-11.0
-10.2
-9.3
PD.41.7
Performance Dispatch
Enroute
FAA
Category G Brakes
Boeing 737 Operations Manual
ALL ENGINES
Long Range Cruise Critical Fuel Reserves
Ground to Air Miles Conversion
AIR DISTANCE (NM)
GROUND
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
DISTANCE
TAILWIND COMPONENT (KTS)
100
80
60
40
20
(NM)
20
40
60
80
100
287
264
244
228
213
200
189
178
169
161
154
582
533
492
457
427
400
376
356
337
320
305
877
803
740
687
640
600
564
533
504
479
456
1172
1072
988
916
854
800
752
710
672
638
607
1467
1341
1236
1146
1068
1000
940
887
840
797
759
1762
1611
1484
1375
1282
1200
1128
1064
1007
956
910
2057
1880
1732
1605
1496
1400
1316
1241
1175
1115
1061
2352
2150
1980
1835
1709
1600
1504
1419
1343
1274
1212
2647
2419
2228
2064
1923
1800
1692
1596
1510
1433
1364
Critical Fuel (1000 LB)
AIR
WEIGHT AT CRITICAL POINT (1000 LB)
DIST
(NM)
100
110
120
130
140
150
160
170
180
190
200
4.2
4.4
4.5
4.7
4.8
5.0
5.1
5.3
5.4
5.6
300
5.9
6.1
6.3
6.5
6.7
6.9
7.1
7.3
7.5
7.7
400
7.7
7.9
8.1
8.4
8.6
8.9
9.2
9.4
9.7
9.9
500
9.4
9.6
9.9
10.2
10.5
10.9
11.2
11.5
11.8
12.1
600
11.1
11.4
11.8
12.1
12.5
12.8
13.2
13.6
13.9
14.3
700
12.8
13.1
13.5
13.9
14.3
14.7
15.2
15.6
16.0
16.5
800
14.5
14.8
15.3
15.7
16.2
16.7
17.1
17.6
18.1
18.6
900
16.2
16.5
17.0
17.5
18.0
18.6
19.1
19.7
20.2
20.7
1000
17.9
18.2
18.8
19.3
19.9
20.5
21.1
21.7
22.3
22.9
1100
19.6
20.0
20.6
21.2
21.8
22.4
23.0
23.7
24.3
25.0
1200
21.3
21.7
22.3
22.9
23.6
24.3
25.0
25.7
26.4
27.1
1300
23.0
23.4
24.0
24.7
25.4
26.1
26.9
27.6
28.4
29.1
1400
24.7
25.1
25.7
26.5
27.2
28.0
28.8
29.6
30.4
31.2
1500
26.4
26.8
27.4
28.2
29.0
29.8
30.7
31.6
32.5
33.3
1600
28.1
28.5
29.1
30.0
30.8
31.7
32.6
33.5
34.4
35.3
1700
29.8
30.2
30.8
31.7
32.6
33.5
34.5
35.4
36.4
37.4
1800
31.5
31.9
32.5
33.4
34.4
35.3
36.3
37.3
38.4
39.4
Based on: Emergency descent to 10000 ft. Level cruise at 10000 ft. 250 KIAS descent to 1500 ft. 15 minute
hold at 1500 ft. One missed approach; approach and land. 5% allowance for wind errors.
Increase fuel required by 0.5% per 10°C above ISA.
If icing conditions exist, increase fuel by 14% to account for engine and wing anti-ice on (7%) and ice accu-
mulation on unheated surfaces (7%).
Allowance for performance deterioration not included.
Compare the fuel required for all engine and engine inoperative critical fuel reserves and use the higher of
the two.
PD.41.8
Performance Dispatch
FAA
Enroute
Category G Brakes
Boeing 737 Operations Manual
ENGINE INOP
Long Range Cruise Critical Fuel Reserves
Ground to Air Miles Conversion
AIR DISTANCE (NM)
GROUND
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
DISTANCE
TAILWIND COMPONENT (KTS)
100
80
60
40
20
(NM)
20
40
60
80
100
291
267
246
229
213
200
188
178
168
160
152
591
539
496
459
428
400
376
354
335
318
302
890
812
746
690
642
600
563
531
502
476
452
1190
1085
996
921
856
800
751
707
668
634
602
1490
1357
1246
1152
1070
1000
938
884
835
792
752
1790
1630
1496
1382
1285
1200
1126
1060
1002
950
902
2090
1903
1746
1613
1499
1400
1313
1237
1169
1107
1052
2390
2175
1996
1844
1713
1600
1501
1413
1335
1265
1203
2690
2448
2246
2075
1928
1800
1688
1590
1502
1423
1353
Critical Fuel (1000 LB)
AIR
WEIGHT AT CRITICAL POINT (1000 LB)
DIST
(NM)
100
110
120
130
140
150
160
170
180
190
200
3.7
3.9
4.1
4.2
4.4
4.5
4.7
4.8
5.0
5.2
300
5.3
5.5
5.7
5.9
6.1
6.4
6.6
6.8
7.0
7.2
400
6.8
7.1
7.3
7.6
7.9
8.2
8.5
8.8
9.0
9.3
500
8.3
8.6
9.0
9.3
9.7
10.0
10.4
10.7
11.1
11.4
600
9.8
10.2
10.6
11.0
11.5
11.9
12.3
12.7
13.1
13.5
700
11.3
11.8
12.3
12.7
13.2
13.6
14.1
14.6
15.0
15.5
800
12.9
13.3
13.9
14.4
14.9
15.4
15.9
16.5
17.0
17.5
900
14.4
14.9
15.4
16.0
16.6
17.2
17.8
18.4
18.9
19.5
1000
15.9
16.4
17.0
17.7
18.3
19.0
19.6
20.3
20.9
21.6
1100
17.4
17.9
18.6
19.3
20.0
20.7
21.4
22.1
22.8
23.5
1200
19.0
19.4
20.2
21.0
21.7
22.5
23.2
24.0
24.7
25.5
1300
20.5
20.9
21.8
22.6
23.4
24.2
25.0
25.8
26.6
27.5
1400
22.0
22.5
23.3
24.2
25.0
25.9
26.8
27.7
28.5
29.4
1500
23.5
24.0
24.8
25.7
26.7
27.6
28.6
29.5
30.4
31.4
1600
25.0
25.5
26.3
27.3
28.3
29.3
30.3
31.3
32.3
33.3
1700
26.6
27.0
27.9
28.9
30.0
31.0
32.1
33.1
34.2
35.2
1800
28.1
28.5
29.4
30.5
31.6
32.7
33.8
34.9
36.0
37.1
Based on: Emergency descent to 10000 ft. Level cruise at 10000 ft. 250 KIAS descent to 1500 ft. 15 minute
hold at 1500 ft. One missed approach; approach and land. 5% allowance for wind errors.
Increase fuel required by 0.5% per 10°C above ISA.
If icing conditions exist, increase fuel by 15% to account for engine and wing anti-ice on (6%) and ice accu-
mulation on unheated surfaces (9%).
Allowance for performance deterioration not included.
Compare the fuel required from this table with critical fuel reserves for all engines operative and use the
higher of the two.
PD.41.9
Performance Dispatch
Enroute
FAA
Category G Brakes
Boeing 737 Operations Manual
Intentionally
Blank
PD.41.10
FAA
Category G Brakes
Boeing 737 Operations Manual
Performance Dispatch
Chapter PD
Landing
Section 42
Landing
Landing Field Limit Weight
Flaps 40
Wind Corrected Field Length (FT)
FIELD LENGTH
WIND COMPONENT (KTS)
AVAILABLE
(FT)
-15
-10
-5
0
10
20
30
40
3000
2640
3000
3200
3420
3630
3860
3400
2650
3020
3400
3620
3840
4070
4310
3800
2660
3020
3400
3800
4030
4260
4500
4750
4200
3010
3380
3770
4200
4440
4680
4940
5200
4600
3370
3740
4150
4600
4850
5110
5380
5650
5000
3730
4100
4530
5000
5260
5530
5810
6100
5400
4090
4470
4910
5400
5670
5950
6250
6550
5800
4440
4830
5280
5800
6080
6380
6680
7000
6200
4800
5190
5660
6200
6500
6800
7120
7440
6600
5160
5560
6040
6600
6910
7220
7550
7890
7000
5510
5920
6410
7000
7320
7650
7990
8340
7400
5870
6280
6790
7400
7730
8070
8420
8790
7800
6230
6640
7170
7800
8140
8490
8860
9240
8200
6590
7010
7550
8200
8550
8920
9300
9690
8600
6940
7370
7920
8600
8960
9340
9730
10140
9000
7300
7730
8300
9000
9370
9760
10170
10580
9400
7660
8100
8680
9400
9790
10190
10600
11030
9800
8010
8460
9050
9800
10200
10610
11040
10200
8370
8820
9430
10200
10610
11030
10600
8730
9180
9810
10600
11020
Field Limit Weight (1000 LB)
WIND CORR'D
AIRPORT PRESSURE ALTITUDE (FT)
FIELD LENGTH
0
2000
4000
6000
8000
10000
(FT)
DRY
WET
DRY
WET
DRY
WET
DRY
WET
DRY
WET
DRY
WET
3800
93.3
87.8
4200
107.1
88.3
100.8
94.7
88.9
4600
121.0
100.2
114.0
94.3
107.1
88.6
100.6
94.3
88.3
5000
132.2
112.3
125.9
105.6
119.8
99.3
112.5
93.2
105.5
87.4
98.8
5400
143.5
123.7
136.5
117.2
130.0
110.1
123.7
103.5
116.8
97.0
109.4
90.8
5800
159.6
133.4
151.9
127.1
140.0
120.9
133.2
113.8
126.6
106.7
120.2
100.0
6200
171.1
143.2
162.9
136.3
154.9
129.7
142.7
123.5
135.6
116.6
128.8
109.2
6600
182.7
157.8
173.8
148.5
165.2
138.5
157.1
131.7
146.7
125.2
137.3
118.6
7000
191.9
167.9
184.8
159.8
175.6
151.8
166.9
140.0
158.5
133.0
150.4
126.4
7400
177.9
193.0
169.3
186.0
161.0
176.7
153.0
167.8
140.9
159.2
133.8
7800
187.5
178.8
193.3
170.0
186.5
161.6
177.1
153.5
168.0
141.1
8200
194.6
187.8
179.0
193.3
170.1
186.3
161.5
176.7
153.3
8600
194.5
187.5
178.6
190.7
169.6
183.1
160.9
9000
193.8
186.9
194.3
177.7
187.2
168.5
9400
192.9
185.7
191.3
176.1
9800
189.9
182.3
10200
193.1
185.9
10600
189.4
11000
192.9
Decrease field limit weight 13300 lb when using manual speedbrakes.
PD.42.1