Boeing 737 - Non-Normal Configuration Landing Distance

737 Operations Manual
Performance Inflight -
Advisory Information
737-500/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE PI.32.3
ADVISORY INFORMATION
Advi sory In formati on
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.
LANDING CONFIGURATION
APPROACH
SPEED
ONE ENGINE
INOPERATIVE
VREF15 3950 130 / -120 190
ANTI-SKID INOPERATIVE VREF40 4720 150/-150 125
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 4570 150 / -140 230
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 4380 140/-140 180
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 4210 130/-140 180
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 3920 120 / -110 180
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 4870 130 / -150 220
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 4070 130 / -120 200
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 4580 130 / -120 220
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 4260 120 / -120 190
FLAPS UP VREF40+55 5160 140 / -140 270
JAMMED STABILIZER VREF15 3760 120 / -110 170
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.
June 07, 2002