Boeing 737 - Non-Normal Configuration Landing Distance

737 Operations Manual
Performance Inflight -
Advisory Information
737-400/CFM56-3_23.5K
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE PI.22.3
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 4100 140 / -130 210
ANTI-SKID INOPERATIVE VREF40 4810 160/-150 125
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 15)
VREF15 4830 170 / -160 250
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 30)
VREF30 4460 150/-150 180
HYDRAULIC SYSTEM A
INOPERATIVE
(FLAPS 40)
VREF40 4270 140/-130 180
HYDRAULIC SYSTEM B
INOPERATIVE
(FLAPS 15)
VREF15 4050 140 / -120 200
HYDRAULIC SYSTEMS
A & B INOPERATIVE
(MANUAL REVERSION)
VREF15 5200 190 / -170 260
LEADING EDGE
ASYMMETRY OR
FAILURE
VREF15+5 4200 140 / -130 220
TRAILING EDGE
FAILURE
(FLAPS LESS THAN 1)
VREF40+40 4550 130 / -120 250
TRAILING EDGE
FAILURE
(FLAPS GREATER THAN 1
AND LESS THAN 15)
VREF40+30 4200 120 / -120 220
FLAPS UP VREF40+55 5100 150 / -140 320
JAMMED STABILIZER VREF15 3880 130 / -120 180
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