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Pressure Effective Landing Length – Feet *
Altitude 4000 5000 6000 7000 8000
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000
100200
97200
94300
91400
N/A
N/A
N/A
N/A
N/A
N/A
N/A
132200
129000
125900
122900
119800
116100
112500
109000
105500
102100
98800
165300
161300
157400
153500
148700
141500
137900
134500
131100
127800
124500
190000
188600
184800
180200
175600
171200
166900
162700
158500
154400
150400
190000
190000
190000
190000
190000
190000
189900
186500
181700
177000
172300
· * For dispatch to a wet or slippery runway, divide the Effective Runway
Landing Length by 1.15 and use that length to enter the chart.
· Subtract 11,900 lbs. from the Runway Landing Limit Weight when auto
speedbrakes not operative.
· Add 550 lb/kt for forecast headwind.
· Subtract 2700 lb/kt for forecast tailwinds.
· Interpolation may be used in the tables.
737 Sec. 5 Page 115
Flight Manual Continental Rev. 11/15/02 #41
D Runway Landing Limit Weight
RUNWAY LANDING LIMIT WEIGHT
15 FLAPS ZERO WIND
ANTI-SKID OPERATIVE
AUTO GROUND SPOILER OPERATIVE
Pressure Effective Landing Length – Feet *
Altitude 5000 6000 7000 8000
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000
110900
108300
105700
102800
99600
96600
93600
90600
N/A
N/A
N/A
134500
131200
128100
124900
121800
118900
115900
113100
110200
107400
104700
163000
159100
155200
151300
143100
139500
136000
132500
129200
125900
122700
179600
176500
173400
170300
167300
164400
160900
156800
152800
145500
140600
· * For dispatch to a wet or slippery runway, divide the Effective Runway
Landing Length by 1.15 and use that length to enter the chart.
· Subtract 12,200 lbs. from the Runway Landing Limit Weight when auto
speedbrakes not operative.
· Add 500 lb/kt for forecast headwind.
· Subtract 2600 lb/kt for forecast tailwinds.
· Interpolation may be used in the tables.
Sec. 5 Page 116 737
Rev. 11/15/02 #41 Continental Flight Manual
Example Landing Problem – Pre-Departure (>)
The following example illustrates the manual (ACCULOAD unavailable)
method to obtain the maximum allowable dispatch landing weight at a particular
airport for the forecast landing conditions, ambient temperature, wind, terrain,
etc.
Note: Examples for the non-normal operations such as anti-skid inoperative
can be found in the non-normal portion of this section.
Destination Airport ---------- AAA
Field Elevation ---------- 4,000 ft.
Runway Length ---------- 7,000 ft.
Flap Setting ---------- 30
Anti-Skid ---------- Normal
Auto Ground Spoilers ---------- Normal
Forecast Temperature ---------- 27°C
Forecast Wind Dir./Vel. ---------- 070/10
Forecast Rwy Condition ---------- Dry
Approach Climb Limit Calculation (-300):
From the Approach Climb Limit Weight chart for landing flap 30, the maximum
approach climb limit weight at 4,000 ft. pressure altitude and 27°C is 129,600
lbs.
Runway Limit Calculation:
From the Runway Limit chart for flaps 30 degree landing, the zero wind
maximum weight at 4,000 ft. pressure altitude and 7,000 ft. runway length is
134,000 lbs. The headwind correction for flaps 30 is 370 lbs./knot. For 10
knots headwind, the correction is 10 x 370 or 3,700 lbs. The maximum runway
limit landing weight is then 134,000 + 3,700 = 137,700 lbs.
Answer:
The approach climb and runway limit weight are both well above the maximum
structural weight. Therefore, the maximum structural landing weight of
114,000 lbs. is the landing weight limit.
737 Sec. 5 Page 117
Flight Manual Continental Rev. 11/15/02 #41
>> V(REF) Speeds
WEIGHT FLAPS
1000 LB 15 30 40
135
132
128
124
120
116
112
108
104
100
96
92
88
84
82
160
158
155
153
151
148
145
　
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