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TRAILING EDGE
FLAP DISAGREE
(30≤ FLAPS <40)
VREF30 3550 120 / -100 90 -150 570
TRAILING EDGE
FLAP DISAGREE
(15≤ FLAPS <30)
VREF15 3800 130 / -110 100 -160 590
TRAILING EDGE
FLAP DISAGREE
(FLAPS <15)
VREF15 3800 130 / -110 100 -160 590
TRAILING EDGE
FLAPS UP
(FLAPS < 1)
VREF40+40 4530 140 / -130 210 -180 630
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.22.6
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Medium 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 6850 250 / -230 330 -310 1060
ANTI-SKID INOPERATIVE VREF40 5870 220 / -200 145 -350 1350
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 40)
VREF40 5370 220 / -200 230 -290 1000
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 30)
VREF30 5690 210 / -220 240 -300 1030
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 15)
VREF15 5980 230 / -220 280 -300 1040
HYDRAULICSLOSS
OF SYSTEM B
(FLAPS 15)
VREF15 5230 190 / -180 230 -270 960
HYDRAULICSLOSS
OF SYSTEMS A & B
(MANUAL REVERSION)
VREF15 6460 250 / -230 310 -320 1100
JAMMED STABILIZER VREF15 4950 180 / -170 210 -260 920
LEADING EDGE
FLAPS TRANSIT VREF15+5 5420 200 / -190 260 -270 970
ONE ENGINE
INOPERATIVE VREF15 5510 200 / -190 250 -290 1030
TRAILING EDGE
FLAP ASYMMETRY
(30≤ FLAPS <40)
VREF30 4690 170 / -160 130 -240 920
TRAILING EDGE
FLAP ASYMMETRY
(15≤ FLAPS <30
VREF15 5070 200 / -180 150 -250 950
TRAILING EDGE
FLAP ASYMMETRY
(1≤ FLAPS <15)
VREF40+30 5630 210 / -190 260 -280 980
TRAILING EDGE
FLAP DISAGREE
(30≤ FLAPS <40)
VREF30 4690 170 / -160 130 -240 920
TRAILING EDGE
FLAP DISAGREE
(15≤ FLAPS <30)
VREF15 5070 200 / -180 150 -250 950
TRAILING EDGE
FLAP DISAGREE
(FLAPS <15)
VREF15 5070 200 / -180 150 -250 950
TRAILING EDGE
FLAPS UP
(FLAPS < 1)
VREF40+40 6050 220 / -200 280 -290 1000
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.22.7
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Poor 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 8570 340 / -310 420 -440 1580
ANTI-SKID INOPERATIVE VREF40 7410 290 / -280 200 -550 2345
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 40)
VREF40 6490 280 / -260 280 -400 1470
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 30)
VREF30 6900 270 / -280 290 -420 1520
HYDRAULICSLOSS
OF SYSTEM A
(FLAPS 15)
VREF15 7380 310 / -280 360 -430 1550
HYDRAULICSLOSS
OF SYSTEM B
(FLAPS 15)
VREF15 6600 270 / -240 300 -390 1450
HYDRAULICSLOSS
OF SYSTEM A & B
(MANUAL REVERSION)
VREF15 7920 330 / -300 380 -450 1610
JAMMED STABILIZER VREF15 6240 250 / -230 270 -380 1400
LEADING EDGE
FLAPS TRANSIT VREF15+5 6800 280 / -260 330 -400 1460
ONE ENGINE
INOPERATIVE VREF15 7330 300 / -280 330 -450 1640
TRAILING EDGE
FLAP ASYMMETRY
　
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