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AUTOBRAKES 2 4690 520/-430 140 -230 840 40 -50 140 -130 530 10 60
AUTOBRAKES 1 5390 610/-530 180 -290 1020 160 -150 160 -150 470 420 510
MAX MANUAL 3550 280/-270 90 -150 570 80 -70 80 -80 280 170 610
MAX AUTO 3550 280/-270 90 -150 570 80 -70 80 -80 280 170 610
AUTOBRAKES 3 4000 350/-320 110 -180 640 50 -40 110 -100 410 40 240
AUTOBRAKES 2 5190 500/-480 150 -250 890 70 -70 150 -140 500 80 80
AUTOBRAKES 1 5740 600/-560 180 -300 1060 170 -160 160 -150 470 550 670
MAX MANUAL 4690 420/-400 130 -240 920 190 -150 120 -110 350 460 1950
MAX AUTO 4690 420/-400 130 -240 920 190 -150 120 -110 350 460 1950
AUTOBRAKES 3 4780 420/-400 130 -250 930 160 -110 120 -120 440 360 1850
AUTOBRAKES 2 5560 530/-510 160 -280 1040 150 -140 150 -140 480 210 1200
AUTOBRAKES 1 5930 610/-580 190 -310 1110 230 -180 170 -160 460 620 1390
MAX MANUAL 5890 580/-550 180 -350 1400 420 -280 150 -140 400 910 5480
MAX AUTO 5890 580/-550 180 -350 1400 420 -280 150 -140 400 920 5480
AUTOBRAKES 3 5890 580/-550 180 -350 1400 420 -270 150 -140 420 920 5480
AUTOBRAKES 2 6240 610/-590 190 -370 1450 380 -270 160 -160 460 680 5120
AUTOBRAKES 1 6440 670/-630 200 -380 1480 430 -300 170 -170 460 910 5030
Reference distance is for sea level, standard day, no wind or slope, VREF30 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.12.3
ADVISORY INFORMATION
Advisory Information Normal Configuration Landing Distance
Flaps 40
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
VREF40
1
REV
NO
REV
MAX MANUAL 2600 300/-160 70 -90 320 30 -20 50 -40 200 40 120
MAX AUTO 2640 280/-180 60 -90 350 20 -10 60 -50 240 20 40
AUTOBRAKES 3 3180 410/-260 90 -140 540 30 -30 90 -80 360 30 60
AUTOBRAKES 2 4510 620/-500 130 -230 820 40 -40 130 -130 520 10 60
AUTOBRAKES 1 5150 620/-500 170 -280 1000 150 -140 150 -140 460 390 490
MAX MANUAL 3450 300/-260 80 -150 560 80 -60 80 -70 280 160 570
MAX AUTO 3450 300/-260 80 -150 560 80 -60 80 -70 280 160 570
AUTOBRAKES 3 3850 360/-310 100 -170 630 50 -30 100 -90 400 40 230
AUTOBRAKES 2 4970 510/-460 140 -240 870 70 -70 140 -130 470 70 70
AUTOBRAKES 1 5460 600/-520 170 -290 1030 160 -150 150 -150 440 490 640
MAX MANUAL 4510 430/-380 130 -240 900 190 -140 110 -100 340 410 1770
MAX AUTO 4510 430/-380 130 -240 900 190 -140 110 -100 340 410 1770
AUTOBRAKES 3 4580 450/-380 130 -240 910 160 -110 120 -110 420 340 1700
AUTOBRAKES 2 5290 530/-490 150 -270 1010 140 -140 140 -140 440 200 1100
AUTOBRAKES 1 5620 610/-550 180 -300 1080 210 -170 160 -150 430 540 1300
MAX MANUAL 5630 590/-520 170 -350 1370 410 -270 140 -130 390 810 4900
MAX AUTO 5630 590/-520 170 -350 1370 410 -270 140 -130 390 810 4900
AUTOBRAKES 3 5610 590/-510 170 -350 1370 410 -260 140 -130 400 810 4900
AUTOBRAKES 2 5950 620/-560 180 -360 1420 370 -260 150 -150 430 620 4580
AUTOBRAKES 1 6120 670/-600 190 -370 1450 410 -290 160 -160 430 800 4530
Reference distance is for sea level, standard day, no wind or slope, VREF40 approach speed and 2 engine
detent reverse thrust.
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold (1000 ft 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.12.4
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Dry Runway
LANDING DISTANCE AND ADJUSTMENTS (FT)
REFERENCE
DISTANCE
FOR 48000 KG
LANDING
WEIGHT
WT ADJ
PER 2000
KG
ABOVE/
BELOW
48000 KG
ALTITUDE
ADJ PER
1000 FT
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