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.
PI.32.4 D6-27370-400E-TBCE
ADVISORY INFORMATION
Advi sory In formati on
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.
LANDING CONFIGURATION
APPROACH
SPEED
ONE ENGINE
INOPERATIVE
VREF15 5470 200 / -190 270
ANTI-SKID INOPERATIVE VREF40 5770 200/-190 175
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 5960 230 / -210 310
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 5610 200/-200 240
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 5310 180/-190 230
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 5210 180 / -170 240
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 6350 200 / -220 290
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 5370 190 / -180 270
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 6100 200 / -190 300
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 5670 190 / -180 260
FLAPS UP VREF40+55 6900 230 / -220 370
JAMMED STABILIZER VREF15 4950 180 / -170 220
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