Boeing 737 - Non-Normal Configuration Landing Distance

737 Operations Manual
Performance Inflight -
Advisory Information
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE PI.12.3
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 / -120 170
ANTI-SKID INOPERATIVE VREF40 4810 170/-150 110
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 4550 150 / -140 210
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 4460 150/-150 180
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 4260 160/-150 180
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 3920 120 / -120 170
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 4950 170 / -150 230
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 4050 130 / -120 190
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 4540 140 / -130 210
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 4200 130 / -120 190
FLAPS UP VREF40+55 5080 160 / -140 240
JAMMED STABILIZER VREF15 3750 120 / -110 150
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