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KIAS 210 210 210 210 210 210 212 213 212
FF/ENG 1070 1030 990 950 920 900 890 890 890
40
%N1 52.3 54.5 58.0 61.7 65.7 69.8 73.8 77.9 79.9
KIAS 210 210 210 210 210 210 210 210 210
FF/ENG 1040 1010 960 930 890 870 850 850 850
38
%N1 51.5 53.8 57.2 60.8 64.8 69.0 72.9 76.9 79.0
KIAS 210 210 210 210 210 210 210 210 210
FF/ENG 1010 980 940 900 870 840 830 820 820
36
%N1 50.7 53.1 56.4 60.0 63.9 68.0 72.0 76.0 78.0
KIAS 210 210 210 210 210 210 210 210 210
FF/ENG 990 960 920 880 850 820 800 790 790
This table includes 5% additional fuel for holding in a racetrack pattern.
June 7, 2002
737 Flight Crew Operations Manual
Performance Inflight - Chapter PI
Advisory Information Section 12
737-300/CFM56-3_20K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
PI.12.1
PI.12 Performance Inflight --AAdvDisVorIyS InOfoRrmYa tIioNnFORMATION
Advisory Information Normal Configuration Landing Distance
Flaps 15
Dry Runway
Good Reported Braking Action
Medium Reported Braking Action
Poor Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (FT)
REF
DIST
WT
ADJ
ALT
ADJ
WIND ADJ
PER 10 KTS
SLOPE ADJ
PER 1%
TEMP ADJ
PER 10°C
VREF
ADJ
REVERSE
THRUST
ADJ
BRAKING
CONFIGURATION
48000 KG
LANDING
WEIGHT
PER
5000 KG
ABOVE/
BELOW
48000
KG
PER
1000 FT
ABOVE
SEA
LEVEL
HEAD
WIND
TAIL
WIND
DOWN
HILL
UP
HILL
ABV
ISA
BLW
ISA
PER 10
KTS
ABOVE
VREF15
1
REV
NO
REV
MAX MANUAL 2750 400/-180 60 -90 340 30 -20 60 -50 210 50 150
MAX AUTO 2910 370/-210 70 -100 370 20 -10 70 -60 250 20 50
AUTOBRAKES 3 3570 500/-310 100 -160 580 40 -30 110 -100 380 30 70
AUTOBRAKES 2 5200 660/-510 160 -250 890 60 -60 160 -150 540 30 90
AUTOBRAKES 1 5950 740/-610 200 -300 1080 180 -170 180 -170 490 550 680
MAX MANUAL 3800 310/-290 100 -160 590 90 -70 90 -80 280 200 690
MAX AUTO 3800 310/-290 100 -160 590 90 -70 90 -80 280 200 690
AUTOBRAKES 3 4390 400/-380 120 -190 680 60 -40 120 -120 430 50 250
AUTOBRAKES 2 5760 580/-560 170 -270 950 90 -90 170 -160 520 140 140
AUTOBRAKES 1 6350 690/-640 210 -320 1120 200 -190 180 -180 480 710 880
MAX MANUAL 5070 480/-450 150 -250 950 200 -160 130 -120 360 540 2240
MAX AUTO 5070 480/-450 150 -250 950 200 -160 130 -120 360 540 2240
AUTOBRAKES 3 5250 490/-460 150 -260 970 160 -110 140 -130 470 370 2060
AUTOBRAKES 2 6170 610/-590 190 -300 1100 170 -160 170 -160 490 300 1360
AUTOBRAKES 1 6570 710/-670 220 -330 1170 250 -210 190 -180 480 790 1670
MAX MANUAL 6410 660/-610 200 -370 1450 450 -300 170 -160 420 1090 6370
MAX AUTO 6410 660/-610 200 -370 1450 450 -300 170 -160 420 1090 6370
AUTOBRAKES 3 6430 660/-610 200 -370 1450 440 -280 170 -160 460 1080 6360
AUTOBRAKES 2 6880 700/-680 210 -390 1510 410 -290 180 -180 480 840 5910
AUTOBRAKES 1 7100 770/-720 230 -400 1550 460 -330 190 -190 480 1100 5830
Reference distance is for sea level, standard day, no wind or slope, VREF15 approach speed and 2 engine
detent reverse thrust
Actual (unfactored) distances are shown
Includes distance from 50 ft above threshold (1000 feet of air distance)
June 4, 2004
737 Flight Crew Operations Manual
Performance Inflight -
Advisory Information
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.12.2
ADVISORY INFORMATION
Advisory Information Normal Configuration Landing Distance
Flaps 30
Dry Runway
Good Reported Braking Action
Medium Reported Braking Action
Poor Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (FT)
REF
DIST
WT
ADJ
ALT
ADJ
WIND ADJ
PER 10 KTS
SLOPE ADJ
PER 1%
TEMP ADJ
PER 10°C
VREF
ADJ
REVERSE
THRUST
ADJ
BRAKING
CONFIGURATION
48000 KG
LANDING
WEIGHT
PER
5000 KG
ABOVE/
BELOW
48000
KG
PER
1000 FT
ABOVE
SEA
LEVEL
HEAD
WIND
TAIL
WIND
DOWN
HILL
UP
HILL
ABV
ISA
BLW
ISA
PER 10
KTS
ABOVE
VREF30
ONE
REV
NO
REV
MAX MANUAL 2590 310/-160 50 -90 330 30 -20 50 -50 200 40 130
MAX AUTO 2710 280/-180 60 -100 350 20 -10 60 -50 240 20 40
AUTOBRAKES 3 3270 400/-270 90 -150 550 40 -30 90 -80 360 30 60
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