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6 -0.4 -0.2 0.0 0.3 1.1
8 -0.5 -0.2 0.0 0.3 1.4
10 -0.6 -0.3 0.0 0.4 1.6
12 -0.7 -0.3 0.0 0.5 1.9
14 -0.8 -0.3 0.0 0.5 2.1
Based on 220 KIAS cruise and descent.
PRESSURE ALT (1000 FT) 5 10 15 17 19 21 23 25 27 29 31 33
DISTANCE (NM) 17 26 35 39 42 46 49 53 57 60 64 68
TIME (MINUTES) 6 8 10 11 11 12 13 14 14 15 16 16
December 1, 2000
737 Flight Crew Operations Manual
Performance Inflight -
Gear Down
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.15.4
GEAR DOWN
Gear Down Holding
Flaps Up
WEIGHT
(1000 KG)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000 20000 25000 30000
64
%N1 72.8 75.6 79.7 83.7 88.1
KIAS 230 230 230 230 230
FF/ENG 2030 2000 1980 1980 2000
60
%N1 70.7 73.4 77.5 81.6 85.9 91.4
KIAS 220 220 220 220 220 220
FF/ENG 1890 1860 1830 1830 1840 1900
56
%N1 69.7 72.4 76.4 80.5 84.6 89.7
KIAS 220 220 220 220 220 220
FF/ENG 1830 1800 1770 1750 1760 1790
52
%N1 67.5 70.1 74.1 78.3 82.3 86.9
KIAS 210 210 210 210 210 210
FF/ENG 1700 1660 1620 1610 1600 1620
48
%N1 66.4 69.0 73.1 77.1 81.2 85.5 91.5
KIAS 210 210 210 210 210 210 210
FF/ENG 1640 1600 1560 1540 1540 1540 1600
44
%N1 65.5 68.1 72.1 76.1 80.1 84.4 89.8
KIAS 210 210 210 210 210 210 210
FF/ENG 1590 1550 1510 1490 1480 1480 1520
40
%N1 64.6 67.2 71.1 75.1 79.2 83.4 88.5
KIAS 210 210 210 210 210 210 210
FF/ENG 1550 1510 1470 1440 1430 1430 1450
36
%N1 63.8 66.3 70.3 74.3 78.4 82.5 87.4
KIAS 210 210 210 210 210 210 210
FF/ENG 1510 1470 1430 1400 1380 1380 1390
32
%N1 63.1 65.6 69.5 73.6 77.7 81.7 86.4
KIAS 210 210 210 210 210 210 210
FF/ENG 1470 1430 1390 1360 1350 1340 1350
This table includes 5% additional fuel for holding in a racetrack pattern.
Based on 230 KIAS for weights above 62823 kg.
December 1, 2000
737 Flight Crew Operations Manual
Performance Inflight - Chapter PI
Text Section 16
737-300/CFM56-3_20K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
PI.16.1
PI.16 Performance Inflight --Text
Text
Introduction
This chapter contains information to supplement performance data from
the Flight Management Computer (FMC). In addition, sufficient inflight
data is provided to complete a flight with the FMC inoperative. In the event
of conflict between data presented in this chapter and that contained in the
Approved Flight Manual, the Flight Manual shall always take precedence.
General
Takeoff Speeds
The speeds presented in the Takeoff Speeds table, as well as FMC
computed takeoff speeds, can be used for all performance conditions
provided adjustments are made to V1 for clearway, stopway, brake
deactivation, improved climb, contaminated runway situations, brake
energy limits or obstacle clearance with unbalanced V1. These speeds may
be used for weights less than or equal to the performance limited weight.
Normal takeoff speeds, V1, VR, and V2, with anti-skid on, are read from
the table by entering with takeoff flap setting, brake release weight, and
appropriate column. The appropriate column is obtained by entering the
Column Reference chart with the airport pressure altitude and the actual
temperature. If an Altitude Adjustment chart is provided, adjust the takeoff
speeds appropriately. Slope and wind adjustments to V1 are obtained by
entering the Slope and Wind V1 Adjustment table.
V1(MCG)
Regulations prohibit scheduling takeoff with a V1 less than minimum V1
for control on the ground, V1(MCG). Therefore compare the adjusted V1
to the V1(MCG). To find V1(MCG) enter the V1(MCG) table with the
airport pressure altitude and actual OAT. If applicable, add the
adjustments shown below the table. If the adjusted V1 is less than
V1(MCG), set V1 equal to V1(MCG). If VR is less than V1(MCG), set VR
equal to V1(MCG), and determine a new V2 by adding the difference
between the normal VR and V1(MCG) to the normal V2.
If it is necessary to increase V1 to V1(MCG), then provided the actual field
length exceeds the minimum field length of 4000 ft no takeoff weight
adjustment is necessary.
December 3, 2004
737 Flight Crew Operations Manual
Performance Inflight -
Text
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.16.2
Clearway and Stopway V1 Adjustments
Takeoff speed corrections are to be applied to V1 speed when using takeoff
weights based on the use of clearway and stopway.
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