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153.6
152.1
150.6
148.5
145.9
N/A
N/A
162.4
160.5
158.8
157.0
155.4
153.7
152.1
150.6
148.3
145.7
143.6
142.2
N/A
N/A
159.2
157.3
155.6
153.9
152.3
150.7
148.3
145.6
143.4
142.0
140.6
N/A
N/A
N/A
156.0
154.2
152.5
150.8
148.5
145.7
143.4
141.9
140.5
139.1
137.8
N/A
N/A
N/A
D
MAXIMUM QUICK TURN AROUND WEIGHT LIMITS
FLAPS 40 LBS. X 1000
PRESSURE ALTITUDE – FEET
°F 0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000
-10
0
10
20
30
40
50
60
70
80
90
100
110
120
190.0
190.0
190.0
190.0
190.0
190.0
190.0
188.7
186.7
184.9
183.2
181.5
179.7
178.1
190.0
190.0
190.0
190.0
190.0
189.0
187.0
185.1
183.3
181.5
179.8
178.1
176.4
174.8
190.0
190.0
190.0
189.4
187.3
185.4
183.5
181.7
179.9
178.1
176.5
174.8
173.2
171.6
190.0
190.0
187.8
185.7
183.8
181.9
180.0
178.2
176.5
174.7
173.1
171.5
169.9
N/A
188.5
186.2
184.2
182.2
180.3
178.4
176.6
174.8
173.1
171.4
169.8
168.2
166.6
N/A
184.8
182.7
180.7
178.8
176.9
175.0
173.2
171.5
169.8
168.1
166.5
165.0
163.5
N/A
181.3
179.2
177.2
175.3
173.4
171.6
169.9
168.1
166.5
164.9
163.3
161.8
N/A
N/A
177.7
175.7
173.8
171.9
170.1
168.3
166.5
164.9
163.2
161.7
160.1
158.6
N/A
N/A
174.3
172.3
170.4
168.5
166.7
165.0
163.3
161.6
160.0
158.5
157.0
155.5
N/A
N/A
170.8
168.9
167.0
165.2
163.4
161.7
160.0
158.4
156.9
155.3
153.8
N/A
N/A
N/A
167.4
165.5
163.7
161.9
160.1
158.5
156.8
155.3
153.7
152.2
150.8
N/A
N/A
N/A
Slope - Add 1500 lbs./1% uphill slope
Subtract 2700 lbs./1% downhill slope
Wind - Add 350 lbs./knot headwind
Subtract 1800 lbs./knot tailwind
Time - If landing weight exceeds chart value, wait at
least 67 min. Then check wheel thermal plugs
before making a subsequent takeoff.
Sec. 5 Page 140 737
Rev. 11/15/02 #41 Continental Flight Manual
Overweight Landing
In an emergency situation requiring a return after takeoff or a landing short of
destination, a Captain may land at a weight in excess of the limitations and
performance of this manual.
Aircraft certification under FAR’s requires a demonstration that the aircraft can
withstand a landing impact of ten feet per second at normal maximum landing
weight. In addition, it must be capable of withstanding a landing impact of six
feet per second at maximum takeoff weight. A normal landing sink rate
averages one to two feet per second; therefore, a normal landing at maximum
gross takeoff weight will not result in a structural problem.
Note: When a landing is made over the normal maximum landing weight, an
entry is required in the aircraft logbook, and a hard landing
maintenance inspection is mandatory.
737 Sec. 5 Page 141
Flight Manual Continental Rev. 11/15/02 #41
MISCELLANEOUS
>>@ Flight With Unreliable Airspeed
CONDITION WEIGHT (1000 LB)
120 110 100 90 80
CLIMB (280/.74). FLAPS UP, SET MAX CLIMB THRUST
CLIMB
30000
4.7
+1200
4.8
+1500
4.9
+1800
5.1
+2200
5.3
+2600
PITCH
V/S
CLIMB
20000
6.2
+1900
6.3
+2200
6.5
+2500
6.8
+2900
7.1
+3300
CLIMB
10000
8.2
+2800
8.5
+3200
8.8
+3500
8.9
+4100
10.1
+4600
CLIMB
SEA LEVEL
10.5
+3600
11.1
+4000
11.7
+4500
12.6
+5100
13.6
+5800
　
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