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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_22K
Copyright © The Boeing Company. See title page for details.
PI.22.4
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
ABOVE S.L.
WIND
CORRECT
PER 10 KTS
HEAD
WIND
WIND
CORRECT
PER 10 KTS
TAIL
WIND
LANDING
CONFIGURATION VREF
ALL FLAPS UP VREF40+55 3930 300 / -140 230 -160 590
ANTI-SKID INOPERATIVE VREF40 3920 120 / -110 80 -175 610
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 40)
VREF40 3180 100 / -90 130 -120 400
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 30)
VREF30 3280 90 / -100 130 -120 410
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 15)
VREF15 3250 110 / -90 150 -120 390
HYDRAULICSLOSS
OF SYSTEM B
(FLAPS 15)
VREF15 3050 170 / -90 150 -120 420
HYDRAULICSLOSS
OF SYSTEMS A & B
(MANUAL REVERSION)
VREF15 4900 170 / -160 230 -210 700
JAMMED STABILIZER VREF15 2730 150 / -70 130 -100 350
LEADING EDGE
FLAPS TRANSIT VREF15+5 2900 170 / -70 150 -110 360
ONE ENGINE
INOPERATIVE VREF15 2770 160 / -80 140 -110 360
TRAILING EDGE
FLAP ASYMMETRY
(30≤ FLAPS <40)
VREF30 2590 130 / -60 50 -90 330
TRAILING EDGE
FLAP ASYMMETRY
(15≤ FLAPS <30)
VREF15 2750 160 / -70 60 -90 340
TRAILING EDGE
FLAP ASYMMETRY
(1≤ FLAPS <15)
VREF40+30 3200 210 / -100 180 -120 430
TRAILING EDGE
FLAP DISAGREE
(30≤ FLAPS <40)
VREF30 2590 130 / -60 50 -90 330
TRAILING EDGE
FLAP DISAGREE
(15≤ FLAPS <30)
VREF15 2750 160 / -70 60 -90 340
TRAILING EDGE
FLAP DISAGREE
(FLAPS <15)
VREF15 2750 160 / -70 60 -90 340
TRAILING EDGE
FLAPS UP
(FLAPS < 1)
VREF40+40 3450 250 / -110 190 -130 510
Actual (unfactored) distances are shown
Includes distances from 50 ft above threshold (1000 ft of air distance)
Assumes maximum manual braking and maximum reverse thrust when available on operating engines.
December 3, 2004
737 Flight Crew Operations Manual
Performance Inflight -
Advisory Information
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
 PI.22.5
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Good Reported Braking Action
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
ABOVE S.L.
WIND
CORRECT
PER 10 KTS
HEAD
WIND
WIND
CORRECT
PER 10 KTS
TAIL
WIND
LANDING
CONFIGURATION VREF
ALL FLAPS UP VREF40+55 5070 160 / -140 240 -200 670
ANTI-SKID INOPERATIVE VREF40 4810 170 / -150 110 -245 900
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 40)
VREF40 4260 160 / -150 180 -190 660
HYDRAULICS_
LOSS OF SYSTEM A
(FLAPS 30)
VREF30 4460 150 / -150 180 -200 670
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 15)
VREF15 4550 160 / -140 210 -200 670
HYDRAULICSLOSS
OF SYSTEM B
(FLAPS 15)
VREF15 3900 120 / -120 170 -170 590
HYDRAULICSLOSS
OF SYSTEMS A & B
(MANUAL REVERSION)
VREF15 4950 170 / -160 230 -210 710
JAMMED STABILIZER VREF15 3750 120 / -110 150 -170 570
LEADING EDGE
FLAPS TRANSIT VREF15+5 4070 130 / -120 190 -180 610
ONE ENGINE
INOPERATIVE VREF15 3950 130 / -120 170 -180 610
TRAILING EDGE
FLAP ASYMMETRY
(30≤ FLAPS <40)
VREF30 3550 120 / -100 90 -150 570
TRAILING EDGE
FLAP ASYMMETRY
(15≤ FLAPS <30)
VREF15 3800 130 / -110 100 -160 590
TRAILING EDGE
FLAP ASYMMETRY
(1≤ FLAPS <15)
VREF40+30 4200 140 / -120 190 -180 600
　
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